Open Access
Issue
Sci. Tech. Energ. Transition
Volume 80, 2025
Article Number 49
Number of page(s) 14
DOI https://doi.org/10.2516/stet/2025029
Published online 17 September 2025

© The Author(s), published by EDP Sciences, 2025

Licence Creative CommonsThis is an Open Access article distributed under the terms of the Creative Commons Attribution License (https://creativecommons.org/licenses/by/4.0), which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

1 Introduction

Global warming is one of the major concerns since the beginning of this century. Climate change is primarily caused by human activity, and in particular by the transport sector, which emits large amounts of greenhouse gases. Electric cars are currently designed for emission-free modes of transport. However, electricity cannot be stored in great quantities, and its direct use through battery-powered vehicles has some limitations in terms of autonomy and recharging times. Hydrogen appears to be a viable solution for producing electricity in cars by using fuel cells. Among the different available technologies, the Proton Exchange Membrane Fuel Cell (PEMFC) seems to be the best solution for automotive applications due to its excellent dynamics, high power density, and good efficiency (>0.5). PEMFC converts hydrogen into electrical energy when the hydrogen reacts with the oxygen in the air to produce water and energy (electricity, but also heat). Although promising, PEMFC faces challenges for their large-scale commercialisation. Their durability appears to be the main issue to be solved. Degradations, which can be irreversible, are the origin of the limited lifespan of PEMFC. These degradations occur notably during an imperfect management of water and heat.

Due to their importance in PEMFC models, the balance equations of mass, momentum, and energy are derived in order to compare these equations with the models currently used in PEMFC simulations. We are concerned with two-phase multicomponent flows in porous media. The liquid water is a single component, but the gas phase mixture includes at least hydrogen, oxygen, nitrogen, and water vapour. The porous media involved in a PEMFC are the gas diffusion layer (GDL), the microporous layer (MPL), and the catalyst layer (CL). Sometimes, the bipolar plates (BPs) containing the gas distribution and water evacuation channels are also considered as porous media since these BPs contain a large number of small channels. After a brief literature survey (Sect. 2), Sections 35 give a complete derivation of the equations governing two-phase multicomponent flows in porous media. Section 3 presents the mathematical tools used in the paper as well as the local instantaneous balance equations. In Section 4, a volume averaging operator is applied to the balance equations derived in Section 3 in order to obtain their averaged counterparts. In Section 5, we give more usable forms of these equations, and Section 6 presents simplifications currently used in PEMFC models.

2 Brief literature survey on the models of flows in general porous media

When studying two-phase flows in porous media, a volume averaging is generally done on a representative elementary volume (REV) containing the three phases (gas, liquid, and the solid medium) (Fig. 1). In Figure 1, Agl denotes the gas-liquid interface, Ags denotes the gas-solid interface, and Als denotes the liquid-solid interface, respectively.

thumbnail Figure 1

Scheme of a typical REV containing the three phases.

Gray et al. [1] give the proof of general theorems relating spatial averages of derivatives to the derivatives of spatial averages for a two-phase medium (e.g., a porous structure embedded in a fluid). Slattery [2] considers simplified averaged mass and momentum equations for flows of viscoelastic fluids in porous media. Whitaker [3] studied the diffusion of a passive species concentration c in a porous medium. He shows that the average of the species concentration balance equation: c t + · ( v ̲ c ) = · ( D c ) $$ \frac{{\partial c}}{{\partial t}}+\nabla \cdot \left(\underline{v}c\right)=\nabla \cdot \left(D\nabla c\right) $$(1)where v ̲ $ \underline{v}$ is the fluid velocity and D is the molecular diffusion coefficient, is given by the following equation: c ̅ t + · ( v ̅ ̲ c ̅ + ψ ̲ ) = · ( D ( c ̅ + R τ ̲ ) ) $$ \frac{\partial \bar{c}}{{\partial t}}+\nabla \cdot \left(\underline{\bar{v}}\bar{c}+\underline{\psi }\right)=\nabla \cdot \left(D\left(\nabla \bar{c}+R\underline{\tau }\right)\right) $$(2)where the overbar denotes the spatial averaging operator, and the new terms ψ ̲ $ \underline{\psi }$ and R τ ̲ $ R\underline{\tau }$ are defined through the following equations. The vector ψ ̲ $ \underline{\psi }$ is due to the covariance between the velocity and concentration fluctuations: ψ ̲ v ' ̅ ̲ c ' ̅ $$ \underline{\psi} \stackrel{\operatorname{def}}{=} \overline{v^{\prime} c^{\prime}} $$(3)where the primed quantities represent fluctuations. R denotes the volumetric interfacial area of the porous medium and the vector τ ̲ $ \underline{\tau }$ is linked to the medium tortuosity. The last term in equation (2) is a reduction of the concentration diffusion if the porous medium is tortuous (i.e., the links between the pores are not rectilinear). They are defined by: R A i V   τ ̲ A ̃ i [ c ] n ̲   d a $$ R{\scriptscriptstyle\mathrm{def}}{=}\frac{{A}_i}{V}\enspace \underline{\tau }\stackrel{\scriptscriptstyle\mathrm{def}}{=}{\int }_{{\tilde{A}}_i}^{}[c]\underline{n}\enspace \mathrm{d}a $$(4)where the non-dimensional area element da = dA/Ai and [c] is the jump of c between the fluid and solid phases at the fluid-solid interface. Other equations are written by the author for other quantities like the fluctuations c′ and v ̲ ' $ {\underline{v}}^{\prime}$. The remainder of his paper is a tentative model for the modelling of these unknown terms.

Abriola et al. [4] write several mass balance equations for a four-phase two-component medium (insertion of a pollutant in a soil containing also water and air). Except for the mass balance equations, these authors use a very simplified form of the momentum equations, which is a generalized Darcy’s law for multiphase flows: v ̲ α = - K K ε s α μ α ( P α - ρ α g ̲ ) $$ {\underline{v}}^{\alpha }=-\frac{K{K}_{{r\alpha }}}{\epsilon {s}_{\alpha }{\mu }_{\alpha }}\left(\nabla {P}^{\alpha }-{\rho }^{\alpha }\underline{g}\right) $$(5)which gives the velocity of the α-phase v ̲ α $ {\underline{v}}^{\alpha }$ as a function of the medium permeability K, the relative permeability K, the porosity ε, the saturation sα (which is the volumetric fraction of this phase), the viscosity μα, the pressure gradient ∇P α , and the gravitational acceleration vector g ̲ $ \underline{g}$. The relative permeability is often modelled as a function of the phase saturation.

In their book about convection in porous media, Nield and Bejan [5] synthesize the following mass and momentum equations for a single-phase flow in a porous medium: ε ρ f t +   · ( ρ f v ̲ ) = 0 $$ \epsilon \frac{\partial {\rho }_f}{{\partial t}}+\nabla \enspace \cdot \left({\rho }_f\underline{v}\right)=0 $$(6)for the mass balance equation, where ε is the porosity (ratio of the fluid volume divided by the total volume), ρf is the fluid density and v ̲ $ \underline{v}$ is the seepage velocity, also known as the superficial velocity. It is not the real velocity but the product of it by the porosity: v ̲ = ε v ̲ f . $$ \underline{v}=\epsilon {\underline{v}}_f. $$(7)

The general momentum equation reads: ρ f [ 1 ε v ̲ t + 1 ε · ( v ̲ v ̲ ε ) ] = - p - μ v ̲ K - c F ρ f K | v ̲ | v ̲ + μ ε 2 v ̲ . $$ {\rho }_f\left[\frac{1}{\epsilon }\frac{\partial \underline{v}}{{\partial t}}+\frac{1}{\epsilon }\nabla \cdot \left(\frac{\underline{v}\underline{v}}{\epsilon }\right)\right]=-\nabla p-\frac{\mu \underline{v}}{K}-{c}_F\frac{{\rho }_f}{\sqrt{K}}\left|\underline{v}\right|\underline{v}+\frac{\mu }{\epsilon }{\nabla }^2\underline{v}. $$(8)

The LHS (Left Hand Side) of equation (8) is the inertial terms, and the terms on the RHS (Right Hand Side) are the pressure gradient, the friction term due to Darcy, an additional quadratic friction term due to Forchheimer, and a diffusion term due to Brinkman. equation (8) is rarely used entirely, but parts of it are supposed to balance, the other terms being neglected. We can therefore retrieve the original Darcy equation, or the Brinkman or Forchheimer equations from (8) by neglecting the appropriate terms.

Nield and Bejan [5] also introduce two thermal equations for the fluid and solid phases of the porous medium. This model is sometimes called the Local Thermal Non-Equilibrium (LTNE) since each phase is characterized by its own temperature equation, therefore taking the thermal imbalance between phases into account. The equations given by [5] read: ( 1 - ε ) ( ρ c ) s T s t = ( 1 - ε ) · ( k s T s ) + ( 1 - ε ) q ''' s + h a ( T f - T s ) $$ \left(1-\epsilon \right){\left({\rho c}\right)}_s\frac{\partial {T}_s}{{\partial t}}=\left(1-\epsilon \right)\nabla \cdot \left({k}_s\nabla {T}_s\right)+\left(1-\epsilon \right){{q}^{{\prime\prime\prime}}_s+ha\left({T}_f-{T}_s\right) $$(9) ε ( ρ c p ) f T f t + ( ρ c p ) f v ̲ · T f = ε · ( k f T f ) + ε q ''' f + h a ( T s - T f ) . $$ \epsilon {\left(\rho {c}_p\right)}_f\frac{\partial {T}_f}{{\partial t}}+{\left(\rho {c}_p\right)}_f\underline{v}\cdot \nabla {T}_f=\epsilon \nabla \cdot \left({k}_f\nabla {T}_f\right)+\epsilon {{q}^{{\prime\prime\prime}}_f+ha\left({T}_s-{T}_f\right). $$(10)

In these equations, Ts and Tf denote the average solid and fluid temperatures, respectively. The quantities q′′′s and q′′′f denote volumetric source terms in each phase and h and a denote a heat exchange coefficient and the volumetric contact area between phases, respectively. If we assume that these two temperatures are equal: T s =   T f = T   thermal   equilibrium   assumption $$ {T}_s=\enspace {T}_f={T}\enspace \mathrm{thermal}\enspace \mathrm{equilibrium}\enspace \mathrm{assumption} $$(11)we can deduce a single equation for the mean temperature T by adding together the two equations (9) and (10). We thus obtain: ( ρ c ) m T t + ( ρ c p ) f v ̲ · T = · ( k m T ) + q ''' m $$ {\left({\rho c}\right)}_m\frac{{\partial T}}{{\partial t}}+{\left(\rho {c}_p\right)}_f\underline{v}\cdot \nabla T=\nabla \cdot \left({k}_m\nabla T\right)+{{q}^{{\prime\prime\prime}}_m $$(12)where (ρc)m, km, and q′′′m are the physical properties of the medium and the volumetric source term in the medium, which are defined by the following equations: ( ρ c ) m = ( 1 - ε ) ( ρ c ) s + ε ( ρ c p ) f $$ {\left({\rho c}\right)}_m=\left(1-\epsilon \right){\left({\rho c}\right)}_s+\epsilon {\left(\rho {c}_p\right)}_f $$(13) k m = ( 1 - ε ) k s + ε k f $$ {k}_m=\left(1-\epsilon \right){k}_s+\epsilon {k}_f $$(14) q ''' m = ( 1 - ε ) q ''' s + ε q ''' f . $$ {{q}^{{\prime\prime\prime}}_m=\left(1-\epsilon \right){{q}^{{\prime\prime\prime}}_s+\epsilon {{q}^{{\prime\prime\prime}}_f. $$(15)

We insist on the fact that the equations (12)(15) are only valid under the thermal equilibrium assumption (11) and that the porosity ε should be constant in space, otherwise it cannot be excluded from the divergences as in equations (9) and (10) as we will show later.

References [69] derived complete set of equations for two-phase flow modelling. Their equations are very detailed, unfortunately they do not deal with porous media.

Sha et al. [10] started from a result demonstrated by [1]: · φ ̲ k = 1 V A e φ ̲ k · n ̲ k d a $$ \nabla \cdot \left\langle {\underline{\phi }}_k\right\rangle=\frac{1}{V}{\int }_{{A}_e}^{}{\underline{\phi }}_k\cdot {\underline{n}}_k\mathrm{d}a $$(16)where φ ̲ k $ {\underline{\phi }}_k$ is an arbitrary vector characterizing the k phase, φ ̲ k $ \left\langle {\underline{\phi }}_k\right\rangle$ is its average over the REV (Fig. 1) denoted by V and Ae is the part of A (the boundary surface of V) available to the fluid passage (i.e., the portion of A not contained in the solid parts of the medium). The relation demonstrated by [10] reads: · φ ̲ k = x ( γ Ax α k φ kx kx ) + y ( γ Ay α k φ ky ky ) + z ( γ Az α k φ kz kz ) $$ \nabla \cdot \left\langle {\underline{\phi }}_k\right\rangle=\frac{\partial }{{\partial x}}\left({\gamma }_{{Ax}}{\alpha }_k\left\langle {\phi }_{{kx}}\right\rangle_{{kx}}\right)+\frac{\partial }{{\partial y}}\left({\gamma }_{{Ay}}{\alpha }_k\left\langle {\phi }_{{ky}}\right\rangle_{{ky}}\right)+\frac{\partial }{{\partial z}}\left({\gamma }_{{Az}}{\alpha }_k\left\langle {\phi }_{{kz}}\right\rangle_{{kz}}\right) $$(17)where αkVk/Vm, Vk being the instantaneous volume of phase k contained in the volume V and Vm is the fluid mixture volume contained in the volume V. The three quantities γAx, γAy, and γAz are the surface porosities contained in each of the planes yz, xz, and xy, respectively, the volume V assumed by [10] being a rectangular parallelepiped. The quantities γAx, γAy, and γAz being directional porosities, the quantities 〈φkxkx, 〈φkyky, and 〈φkzkz represent the phase-averaged vector components through the surfaces normal to x, y, and z occupied by phase k. The demonstration of the relation (17) assumes that the size of the REV is not arbitrary: it should be large in comparison to the pores, size and small in comparison to the global scale of the flow [11]. According to [11], if conditions of both stability and regularity are satisfied, then the volume-averaged and surface-averaged values coincide at every point, hence there is no need to make the distinction between the surface porosities γAx, γAy, and γAz and the volumetric one given by ε. Similarly, there is no need to make the distinction between 〈φkxkx and 〈φkxk which is the phase-average of the vector component φkx. According to these assertions, the relation (17) simplifies to: · φ ̲ k = · ( ε α k φ ̲ k k ) $$ \nabla \cdot \left\langle {\underline{\phi }}_k\right\rangle=\nabla \cdot \left(\epsilon {\alpha }_k\left\langle {\underline{\phi }}_k\right\rangle_k\right) $$(18)which is simply a consequence of the chosen notations: φ ̲ k ε α k φ ̲ k k $ \left\langle {\underline{\phi }}_k\right\rangle\stackrel{\scriptscriptstyle\mathrm{def}}{=}\epsilon {\alpha }_k\left\langle {\underline{\phi }}_k\right\rangle_k$ (see later in the article). The proof of what we just said is also given by [12].

3 Two-phase flow equations in porous media

3.1 Definitions and mathematical tools

We consider a two-phase flow in a porous medium. In this porous medium, we isolate a REV containing the three phases: gas, liquid, and solid (Fig. 1). This REV, denoted by V, will be the control volume for averaging. It must be large enough in comparison to the size of the pores and links between them, and small enough in comparison to the global scales of the flow. This double condition on the size of the REV is necessary for the averaged quantities to be stable and regular [11]. It should be remarked that it is not always possible in particular applications, and this condition must be kept in mind when applying the average model to a particular situation, like PEMFC modelling. The porous media in PEMFC (gas diffusion layers, microporous layers, and catalytic layers) contain two fluid phases (water and gas) and several chemical components (oxygen, hydrogen, nitrogen, and water vapour at least), so we develop a multi-constituent two-phase model for porous media. Indexing by k the general phase, by s the solid phase, and by m the liquid-gas mixture in the pores, the porosity is defined by the following relation: ε k s V k V = V m V $$ \epsilon \stackrel{\scriptscriptstyle\mathrm{def}}{=}\frac{\sum_{k\ne s}^{}{V}_k}{V}=\frac{{V}_m}{V} $$(19)where Vk denotes the instantaneous volume occupied by phase k (inside the REV) and Vm denotes the fluid volume in the REV, which does not depend on time since the REV is assumed to be fixed and the porous medium is assumed to be undeformable. The phase k volume fraction, sometimes called the saturation in the porous literature, is defined by the following relation: α k = V k k s V k = V k ε V . $$ {\alpha }_k=\frac{{V}_k}{\sum_{k\ne s}^{}{V}_k}=\frac{{V}_k}{{\epsilon V}}. $$(20)

From equation (20), we can deduce: k s α k = 1 . $$ \sum_{k\ne s}^{}{\alpha }_k=1. $$(21)

Let us define the Phase Indicator Function (PIF) by the following relation: X k ( x ̲ , t ) { 1   if   the   point   x ̲   pertains   to   phase   k   at   time   t 0   otherwise } . $$ {X}_k\left(\underline{x},t\right)\stackrel{\scriptscriptstyle\mathrm{def}}{=}\left\{\begin{array}{c}1\enspace \mathrm{if}\enspace \mathrm{the}\enspace \mathrm{point}\enspace \underline{x}\enspace \mathrm{pertains}\enspace \mathrm{to}\enspace \mathrm{phase}\enspace k\enspace \mathrm{at}\enspace \mathrm{time}\enspace t\\ 0\enspace \mathrm{otherwise}\end{array}\right\}. $$(22)

It can be shown by means of the generalized function theory (e.g., [1, 9]): X k = - n ̲ k δ I $$ \nabla {X}_k=-{\underline{n}}_k{\delta }_I $$(23)where n ̲ k $ {\underline{n}}_k$ is the unit vector normal to the interfaces with the other phases and pointing outwardly from phase k. The quantity δI is a Dirac delta function having different interfaces as its support. δI is also called the local instantaneous interfacial area concentration by [13].

The volume average of an arbitrary quantity ψ is defined by the following relation: ψ 1 V V ψ d v . $$ \left\langle \psi \right\rangle\stackrel{\scriptscriptstyle\mathrm{def}}{=}\frac{1}{V}{\int }_V^{}\psi \mathrm{d}{v}. $$(24)

The phase-averaged of an arbitrary quantity ψk pertaining to phase k is defined on the phase volume: ψ k k 1 V k V k ψ k d v . $$ \left\langle {\psi }_k\right\rangle_k\stackrel{\scriptscriptstyle\mathrm{def}}{=}\frac{1}{{V}_k}{\int }_{{V}_k}^{}{\psi }_k\mathrm{d}{v}. $$(25)

Because of the PIF definition, it is easily shown that: X k 1 V V X k d v = V k V = ε α k . $$ \left\langle {X}_k\right\rangle\stackrel{\scriptscriptstyle\mathrm{def}}{=}\frac{1}{V}{\int }_V^{}{X}_k\mathrm{d}v=\frac{{V}_k}{V}=\epsilon {\alpha }_k. $$(26)

The mathematical link between the volume average (24) and the phase average (25) is: X k ψ k 1 V V k ψ k d v = V k V 1 V k V k ψ k d v = ε α k ψ k k . $$ \left\langle {X}_k{\psi }_k\right\rangle\stackrel{\scriptscriptstyle\mathrm{def}}{=}\frac{1}{V}{\int }_{{V}_k}^{}{\psi }_k\mathrm{d}v=\frac{{V}_k}{V}\frac{1}{{V}_k}{\int }_{{V}_k}^{}{\psi }_k\mathrm{d}v=\epsilon {\alpha }_k\left\langle {\psi }_k\right\rangle_k. $$(27)

Two theorems must be introduced at this stage, which allow the averaging operator to permute with the time and space derivatives. These theorems are sometimes called the limiting forms of the Leibniz and Gauss theorem [68]. Here we give the version of these two theorems as derived by Gray and Lee [1]. Multiplying the gradient of an arbitrary quantity by the PIF and volume averaging, we can write: X k ψ k = X k ψ k - ψ k X k = X k ψ k + ψ k n ̲ k δ I $$ \left\langle {X}_k\nabla {\psi }_k\right\rangle=\nabla \left\langle {X}_k{\psi }_k\right\rangle-\left\langle {\psi }_k\nabla {X}_k\right\rangle=\nabla \left\langle {X}_k{\psi }_k\right\rangle+\left\langle {\psi }_k{\underline{n}}_k{\delta }_I\right\rangle$$(28)where the last term ψ k n ̲ k δ I $ \left\langle {\psi }_k{\underline{n}}_k{\delta }_I\right\rangle$ represents the contributions of the interfaces between phase k and the other phases. For example, if phase k is the liquid phase, the Dirac distribution δI peaks to the interface with the gas on one hand, and to the interface with the solid part on the other hand. The equation (28) relates the average of a gradient to the gradient of the average. Adding a dot (scalar product) in (28), the corresponding equation for the divergence can be easily obtained. Another writing for the last term in (28) is [14]: ψ k n ̲ k δ I = 1 V A I , k ψ k n ̲ k d a = 1 V A kf ψ k n ̲ k d a + 1 V A ks ψ k n ̲ k d a $$ \left\langle {\psi }_k{\underline{n}}_k{\delta }_I\right\rangle=\frac{1}{V}{\int }_{{A}_{I,k}}^{}{\psi }_k{\underline{n}}_k\mathrm{d}a=\frac{1}{V}{\int }_{{A}_{{kf}}}^{}{\psi }_k{\underline{n}}_k\mathrm{d}a+\frac{1}{V}{\int }_{{A}_{{ks}}}^{}{\psi }_k{\underline{n}}_k\mathrm{d}a $$(29)where the integral on the surface area AI,k has been decomposed into the sum of two integrals: one on the interface between phase k and the other fluid phase f Akf and another on the interface between phase k and the solid parts Aks. AI,k = Akf ∪ Aks is the total interfacial area in the volume V seen by the phase k. Putting ψk = 1 into the equation (28), we obtain a relation giving the gradient of the product between the porosity and the phase saturation: ( ε α k ) = - 1 V A I , k n ̲ k d a = - 1 V A kf n ̲ k d a - 1 V A ks n ̲ k d a . $$ \nabla \left(\epsilon {\alpha }_k\right)=-\frac{1}{V}{\int }_{{A}_{I,k}}^{}{\underline{n}}_k\mathrm{d}a=-\frac{1}{V}{\int }_{{A}_{{kf}}}^{}{\underline{n}}_k\mathrm{d}a-\frac{1}{V}{\int }_{{A}_{{ks}}}^{}{\underline{n}}_k\mathrm{d}{a}. $$(30)

The PIF verifies the following transport equation [9]: X k t + v ̲ I · X k = 0 $$ \frac{\partial {X}_k}{{\partial t}}+{\underline{v}}_I\cdot \nabla {X}_k=0 $$(31)where v ̲ I $ {\underline{v}}_I$ is the local instantaneous interface velocity field. Using equations (23) and (31), we can write: X k ψ k t = t X k ψ k - ψ k X k t = t X k ψ k - ψ k v I · n k δ I $$ \left\langle {X}_k\frac{\partial {\psi }_k}{{\partial t}}\right\rangle=\frac{\partial }{{\partial t}}\left\langle {X}_k{\psi }_k\right\rangle-\left\langle {\psi }_k\frac{\partial {X}_k}{{\partial t}}\right\rangle=\frac{\partial }{{\partial t}}\left\langle {X}_k{\psi }_k\right\rangle-\left\langle {\psi }_k{v}_I\cdot {n}_k{\delta }_I\right\rangle$$(32)which is the second theorem giving the link between the average of a time derivative and the time derivative of the average. The equation (32) can equivalently be written as: X k ψ k t = t ( ε α k ψ k k ) - 1 V A kf ψ k v I · n k d a . $$ \left\langle {X}_k\frac{\partial {\psi }_k}{{\partial t}}\right\rangle=\frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_k\left\langle {\psi }_k\right\rangle_k\right)-\frac{1}{V}{\int }_{{A}_{{kf}}}^{}{\psi }_k{v}_I\cdot {n}_k\mathrm{d}{a}. $$(33)

Here, there is no contribution from the interface with the solid because the solid parts are assumed to be immobile. Putting ψk = 1 into (33), the time derivative of the phase volumetric fraction is obtained: t ( ε α k ) = 1 V A kf v I · n k d a . $$ \frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_k\right)=\frac{1}{V}{\int }_{{A}_{{kf}}}^{}{v}_I\cdot {n}_k\mathrm{d}a. $$(34)

3.2 Local instantaneous balance equations for two-phase flows

A general balance equation for two-phase flows before the averaging operation can be written as [68]: ρ k ψ k t + · ( ρ k ψ k v ̲ k ) = - · J ̲ k + ϕ k $$ \frac{\partial {\rho }_k{\psi }_k}{{\partial t}}+\nabla \cdot \left({\rho }_k{\psi }_k{\underline{v}}_k\right)=-\nabla \cdot {\underline{J}}_k+{\phi }_k $$(35)where ρk is the phase density, v ̲ k $ {\underline{v}}_k$ is the phase velocity, ψk is an arbitrary quantity per unit mass of phase k, J ̲ k $ {\underline{J}}_k$ is a diffusional flux and ϕk is a general source term. The equation (35) is valid inside the phase k only. The corresponding equation valid through the interfaces between two phases (sometimes called the jump condition) reads: k ( m ̇ k ψ k - J ̲ k . n ̲ k ) = ϕ I $$ \sum_k^{}\left({\dot{m}}_k{\psi }_k-{\underline{J}}_k.{\underline{n}}_k\right)={\phi }_I $$(36)

The quantity m ̇ k $ {\dot{m}}_k$ is the mass gain for phase k, per unit surface and unit time, due to phase change (vaporisation and condensation). It is defined by the following equation: m ̇ k ρ k ( v ̲ I - v ̲ k ) · n ̲ k . $$ {\dot{m}}_k\stackrel{\scriptscriptstyle\mathrm{def}}{=}{\rho }_k\left({\underline{v}}_I-{\underline{v}}_k\right)\cdot {\underline{n}}_k. $$(37)

The quantity ϕI is a general source term defined on the interfaces. Table 1 gives the values of ψk, Jk, ϕk and ϕI for the different balance equations of interest: mass, species mass, momentum, and the different forms of energy.

Table 1

Notations for the generalised balance equations (35) and (36).

Substituting these values into the balance equations (35) and (36), we thus obtain the detailed balance equations for phase k. The mass balances read: ρ k t + · ( ρ k v ̲ k ) = r k   and   k m ̇ k = 0 $$ \frac{\partial {\rho }_k}{{\partial t}}+\nabla \cdot \left({\rho }_k{\underline{v}}_k\right)={r}_k\enspace \mathrm{and}\enspace \sum_k^{}{\dot{m}}_k=0 $$(38)where ρk is the density of phase k and the symbol Σk means the summation on the two phases separated by the interface (the second Eq. (38)), as all the jump conditions, is valid on an interface only). The symbol rk is used for the source term due to chemical reactions. The species balance equations for species i in phase k read: ρ k Y ik t + · ( ρ k Y ik v ̲ k ) = - · j ̲ ik + r ik   and   k ( m ̇ k Y ik - j ̲ ik · n ̲ k ) = r is $$ \frac{\partial {\rho }_k{Y}_{{ik}}}{{\partial t}}+\nabla \cdot \left({\rho }_k{Y}_{{ik}}{\underline{v}}_k\right)=-\nabla \cdot {\underline{j}}_{{ik}}+{r}_{{ik}}\enspace \mathrm{and}\enspace \sum_k^{}\left({\dot{m}}_k{Y}_{{ik}}-{\underline{j}}_{{ik}}\cdot {\underline{n}}_k\right)={r}_{{is}} $$(39)where Yik is the mass fraction of species i in phase k, j ik is the diffusive flux and rik is a source term due to homogeneous chemical reactions. The term ris is the rate at which species i is produced by heterogeneous chemical reactions.

The momentum balance equation in phase k reads: ρ k v ̲ k t + · ( ρ k v ̲ k v ̲ k ) = - p k + · τ ̲ ̲ k + ρ k g ̲   + r k v k r . $$ \frac{\partial {\rho }_k{\underline{v}}_k}{{\partial t}}+\nabla \cdot \left({\rho }_k{\underline{v}}_k{\underline{v}}_k\right)=-\nabla {p}_k+\nabla \cdot {\underline{\underline{\tau }}}_k+{\rho }_k\underline{g}\enspace +{r}_k{v}_k^r. $$(40)

The term r k v k r $ {r}_k{v}_k^r$ was introduced by [14] and corresponds to a supply of momentum due to chemical reactions, pk is the pressure for phase k and τ ̲ ̲ k $ {\underline{\underline{\tau }}}_k$ is the viscous stress tensor. The momentum jump condition reads [9, 15]: k ( m ̇ k v ̲ k + σ ̲ ̲ k · n ̲ k ) = F ̲ I s σ + 2 H k σ n ̲ k . $$ \sum_k^{}\left({\dot{m}}_k{\underline{v}}_k+{\underline{\underline{\sigma }}}_k\cdot {\underline{n}}_k\right)={\underline{F}}_I\cong {\nabla }_s\sigma +2{H}_k\sigma {\underline{n}}_k. $$(41)

The vector g ̲ $ \underline{g}$ is the gravity acceleration, σ ̲ ̲ k $ {\underline{\underline{\sigma }}}_k$ is the total stress tensor (grouping the pressure and the viscous ones) and F ̲ I $ {\underline{F}}_I$ is the surface tension force per unit area. In (41) σ is the surface tension coefficient and H k - ( · n ̲ k ) / 2 $ {H}_k\stackrel{\scriptscriptstyle\mathrm{def}}{=}-\left(\nabla \cdot {\underline{n}}_k\right)/2$ is the local mean curvature of the interface seen by phase k. The first term ∇sσ is the surface gradient of the surface tension, which is called the Marangoni effect in the literature.

The total energy balance equation in phase k reads: ρ k ( e k + v k 2 2 ) t + · ( ρ k ( e k + v k 2 2 ) v ̲ k ) = - · ( q ̲ k - σ ̲ ̲ k · v ̲ k ) + ρ k g ̲ · v ̲ k $$ \frac{\partial {\rho }_k\left({e}_k+\frac{{{v}_k}^2}{2}\right)}{{\partial t}}+\nabla \cdot \left({\rho }_k\left({e}_k+\frac{{{v}_k}^2}{2}\right){\underline{v}}_k\right)=-\nabla \cdot \left({\underline{q}}_k-{\underline{\underline{\sigma }}}_k\cdot {\underline{v}}_k\right)+{\rho }_k\underline{g}\cdot {\underline{v}}_k $$(42)and the total energy jump condition reads: k ( m ̇ k ( e k + v k 2 2 ) - ( q ̲ k - σ ̲ ̲ k · v ̲ k ) · n ̲ k ) = E I $$ \sum_k^{}\left({\dot{m}}_k\left({e}_k+\frac{{{v}_k}^2}{2}\right)-\left({\underline{q}}_k-{\underline{\underline{\sigma }}}_k\cdot {\underline{v}}_k\right)\cdot {\underline{n}}_k\right)={E}_I $$(43)where ek is the internal energy per unit mass, q ̲ k $ {\underline{q}}_k$ is the heat flux density and EI is a possible interfacial energy source. References [16, 17] give the exact expression for the interfacial source term EI: E I = ρ I D I ( e I + v I 2 / 2 ) Dt + m ̇ I ( e I + v I 2 / 2 ) - ρ I v ̲ I · g ̲ + s · q ̲ I - s · ( σ v ̲ It ) . $$ {E}_I={\rho }_I\frac{{D}_I\left({e}_I+{{v}_I}^2/2\right)}{{Dt}}+{\dot{m}}_I\left({e}_I+{{v}_I}^2/2\right)-{\rho }_I{\underline{v}}_I\cdot \underline{g}+{\nabla }_s\cdot {\underline{q}}_I-{\nabla }_s\cdot \left({\sigma \underline{v}}_{{It}}\right). $$(44)

In this equation, ρI is the interface density per unit surface, eI is the interfacial internal energy per unit mass and v ̲ I $ {\underline{v}}_I$ is the interface velocity, σ v ̲ It $ {\sigma \underline{v}}_{{It}}$ is the product of the surface tension coefficient and the tangential interfacial velocity vector. The interfacial mass source term m ̇ I $ {\dot{m}}_I$ is defined by: m ̇ I D I ρ I Dt + ρ I s · v ̲ I . $$ {\dot{m}}_I\stackrel{\scriptscriptstyle\mathrm{def}}{=}\frac{{D}_I{\rho }_I}{{Dt}}+{\rho }_I{\nabla }_s\cdot {\underline{v}}_I. $$(45)

In this study, we neglect the interface properties except the surface tension and latent heat, therefore the approximate form of equation (44) is: ρ I = q ̲ I = 0 E I - s · ( σ v ̲ It ) . $$ {\rho }_I={\underline{q}}_I=0\to {E}_I\cong -{\nabla }_s\cdot \left({\sigma \underline{v}}_{{It}}\right). $$(46)

The advantage of the generic balance equation (35) is that we can apply the averaging operator and theorems once to it to obtain the corresponding generic averaged balance equation. After this is done, the detailed averaged balance equations will be deduced from the generic one by employing the values given in Table 1.

The enthalpy balance equation reads: ρ k h k t + · ( ρ k h k v ̲ k ) = - · q ̲ k + D k p k Dt + τ ̲ ̲ k : v ̲ k   + r k h k r $$ \frac{\partial {\rho }_k{h}_k}{{\partial t}}+\nabla \cdot \left({\rho }_k{h}_k{\underline{v}}_k\right)=-\nabla \cdot {\underline{q}}_k+\frac{{D}_k{p}_k}{{Dt}}+{\underline{\underline{\tau }}}_k:\nabla {\underline{v}}_k\enspace +{r}_k{h}_k^r $$(47)where h k r $ {h}_k^r$ is a reaction enthalpy and D k p k Dt $ \frac{{D}_k{p}_k}{{Dt}}$ is the material derivative of the pressure: D k p k Dt p k t + v ̲ k · p k . $$ \frac{{D}_k{p}_k}{{Dt}}\stackrel{\scriptscriptstyle\mathrm{def}}{=}\frac{\partial {p}_k}{{\partial t}}+{\underline{v}}_k\cdot \nabla {p}_k. $$(48)

The term τ ̲ ̲ k : v ̲ k $ {\underline{\underline{\tau }}}_k:\nabla {\underline{v}}_k$ is the dissipation of mechanical energy into heat due to internal friction. The interfacial enthalpy balance reads: k ( m ̇ k h k - q ̲ k · n ̲ k ) = H I . $$ \sum_k^{}\left({\dot{m}}_k{h}_k-{\underline{q}}_k\cdot {\underline{n}}_k\right)={H}_I. $$(49)

References [16, 17] derive the following expression for the interfacial balance of enthalpy: k ( m ̇ k ( h k + v k 2 2 - v ̲ k · v ̲ I ) - q ̲ k · n ̲ k + τ ̲ ̲ k · n ̲ k · ( v ̲ k - v ̲ I ) ) = - ρ I D I h I Dt - D I σ Dt - m ̇ I ( h I - v I 2 2 ) - s · q ̲ I . $$ \sum_k^{}\left({\dot{m}}_k\left({h}_k+\frac{{{v}_k}^2}{2}-{\underline{v}}_k\cdot {\underline{v}}_I\right)-{\underline{q}}_k\cdot {\underline{n}}_k+{\underline{\underline{\tau }}}_k\cdot {\underline{n}}_k\cdot \left({\underline{v}}_k-{\underline{v}}_I\right)\right)=-{\rho }_I\frac{{D}_I{h}_I}{{Dt}}-\frac{{D}_I\sigma }{{Dt}}-{\dot{m}}_I\left({h}_I-\frac{{{v}_I}^2}{2}\right)-{\nabla }_s\cdot {\underline{q}}_I. $$(50)

The comparison of (49) and (50) allows us to find the exact expression of the term HI. Neglecting the interfacial properties as we have done in (46) and neglecting the mechanical effects in comparison to the thermal effects in the LHS of (50), we obtain the following approximate expression for HI: H I - D I σ Dt = - σ t - v ̲ I · s σ . $$ {H}_I\cong -\frac{{D}_I\sigma }{{Dt}}=-\frac{{\partial \sigma }}{{\partial t}}-{\underline{v}}_I\cdot {\nabla }_s{\sigma }. $$(51)

The internal energy balance equation reads: ρ k e k t + · ( ρ k e k v ̲ k ) = - · q ̲ k - p k · v ̲ k + τ ̲ ̲ k : v ̲ k + r k h k r $$ \frac{\partial {\rho }_k{e}_k}{{\partial t}}+\nabla \cdot \left({\rho }_k{e}_k{\underline{v}}_k\right)=-\nabla \cdot {\underline{q}}_k{-p}_k\nabla \cdot {\underline{v}}_k+{\underline{\underline{\tau }}}_k:\nabla {\underline{v}}_k+{r}_k{h}_k^r $$(52)where the source term due to homogeneous chemical reactions is proportional to the reaction enthalpy h k r $ {h}_k^r$ [14]. This can be easily verified by comparing (52) and (47). The interfacial balance equation (36) reads: k ( m ̇ k e k - q ̲ k · n ̲ k ) = ϵ I . $$ \sum_k^{}\left({\dot{m}}_k{e}_k-{\underline{q}}_k\cdot {\underline{n}}_k\right)={\epsilon }_I. $$(53)

References [16, 17] derive the following expression for the interfacial balance of internal energy: k ( m ̇ k ( e k + v k 2 2 - v ̲ k · v ̲ I ) - q ̲ k · n ̲ k + σ ̲ ̲ k · n ̲ k · ( v ̲ k - v ̲ I ) ) = - ρ I D I e I Dt - m ̇ I ( e I - v I 2 2 ) - s · q ̲ I + σ s · v ̲ It . $$ \sum_k^{}\left({\dot{m}}_k\left({e}_k+\frac{{{v}_k}^2}{2}-{\underline{v}}_k\cdot {\underline{v}}_I\right)-{\underline{q}}_k\cdot {\underline{n}}_k+{\underline{\underline{\sigma }}}_k\cdot {\underline{n}}_k\cdot \left({\underline{v}}_k-{\underline{v}}_I\right)\right)=-{\rho }_I\frac{{D}_I{e}_I}{{Dt}}-{\dot{m}}_I\left({e}_I-\frac{{{v}_I}^2}{2}\right)-{\nabla }_s\cdot {\underline{q}}_I+\sigma {\nabla }_s\cdot {\underline{v}}_{{It}}. $$(54)

The comparison of (53) and (54) allows to find the exact expression of the term ϵI. Neglecting the interfacial properties as we have done before and neglecting the mechanical effects in comparison to the thermal effects in the LHS of (54), we obtain the following approximate expression for ϵI: ϵ I σ s · v ̲ It . $$ {\epsilon }_I\cong \sigma {\nabla }_s\cdot {\underline{v}}_{{It}}. $$(55)

The entropy balance equation reads: ρ k s k t + · ( ρ k s k v ̲ k ) = - · ( q ̲ k T k ) + k + r k s k r . $$ \frac{\partial {\rho }_k{s}_k}{{\partial t}}+\nabla \cdot \left({\rho }_k{s}_k{\underline{v}}_k\right)=-\nabla \cdot \left(\frac{{\underline{q}}_k}{{T}_k}\right)+{\Delta }_k+{r}_k{s}_k^r. $$(56)where ∆k is the entropy source term, which is given by: k τ ̲ ̲ k : v ̲ k T k + q ̲ k · ( 1 T k ) 0 . $$ {\Delta }_k\stackrel{\scriptscriptstyle\mathrm{def}}{=}\frac{{\underline{\underline{\tau }}}_k:\nabla {\underline{v}}_k}{{T}_k}+{\underline{q}}_k\cdot \nabla \left(\frac{1}{{T}_k}\right)\ge 0. $$(57)

The fact that ∆k ≥ 0 is the expression of the second law of thermodynamics for phase k.

References [16, 17] give the following expression of the second law of thermodynamics at the interface: k ( m ̇ k s k - q ̲ k T k · n ̲ k ) + ρ I D I s I Dt + m ̇ I s I + s · ( q ̲ I T I ) 0 . $$ \sum_k^{}\left({\dot{m}}_k{s}_k-\frac{{\underline{q}}_k}{{T}_k}\cdot {\underline{n}}_k\right)+{\rho }_I\frac{{D}_I{s}_I}{{Dt}}+{\dot{m}}_I{s}_I+{\nabla }_s\cdot \left(\frac{{\underline{q}}_I}{{T}_I}\right)\ge 0. $$(58)

Equation (36) gives for the particular case of entropy (see Table 1): k ( m ̇ k s k - q ̲ k T k · n ̲ k ) = I . $$ \sum_k^{}\left({\dot{m}}_k{s}_k-\frac{{\underline{q}}_k}{{T}_k}\cdot {\underline{n}}_k\right)={\Delta }_I. $$(59)

Comparing these two expressions and neglecting the interfacial properties as we have done before, the interfacial entropy source is equal to zero: I 0 . $$ {\Delta }_I\cong 0. $$(60)

One important consequence of (60) is that the local temperatures are equal at the interface [7, 8]: T L = T G = T I . $$ {T}_L={T}_G={T}_I. $$(61)

Equation (47), (52), and (56) are equivalent to the primary total energy equation (42). The choice of the energy equation is just a question of convenience.

4 Two-phase volume-averaged equations

Multiplying the phase general equation (35) by Xk, taking the volume average of the resulting equation and using the theorems and definitions of the previous section, the following averaged general balance equation is easily obtained: t ( ε α k ρ k ψ k k ) + · ( ε α k ρ k ψ k v ̲ k k ) = 1 V A Ik ( m ̇ k ψ k - J ̲ k · n ̲ k ) d a - · ( ε α k J ̲ k k ) + ε α k ϕ k k . $$ \frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_k\left\langle {\rho }_k{\psi }_k\right\rangle_k\right)+\nabla \cdot \left(\epsilon {\alpha }_k\left\langle {\rho }_k{\psi }_k{\underline{v}}_k\right\rangle_k\right)=\frac{1}{V}{\int }_{{A}_{{Ik}}}^{}\left({\dot{m}}_k{\psi }_k-{\underline{J}}_k\cdot {\underline{n}}_k\right)\mathrm{d}a-\nabla \cdot \left(\epsilon {\alpha }_k\left\langle {\underline{J}}_k\right\rangle_k\right)+\epsilon {\alpha }_k\left\langle {\phi }_k\right\rangle_k. $$(62)

In the same manner, the interfacial average of equation (36) gives: k 1 V A I ( m ̇ k ψ k - J ̲ k · n ̲ k ) d a = 1 V A I ϕ I d a . $$ \sum_k^{}\frac{1}{V}{\int }_{{A}_I}^{}\left({\dot{m}}_k{\psi }_k-{\underline{J}}_k\cdot {\underline{n}}_k\right)\mathrm{d}a=\frac{1}{V}{\int }_{{A}_I}^{}{\phi }_I\mathrm{d}a. $$(63)

4.1 Mass balance equation

Putting ψ k = 1 ,   J ̲ k = 0 ,   ϕ k = r k $ {\psi }_k=1,\enspace {\underline{J}}_k=0,\enspace {\phi }_k={r}_k$ in the equation (62), the following phase k mass balance equation is obtained: t ( ε α k ρ k k ) + · ( ε α k ρ k v ̲ k k ) = ε α k r k k + 1 V A Ik m ̇ k d a . $$ \frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_k\left\langle {\rho }_k\right\rangle_k\right)+\nabla \cdot \left(\epsilon {\alpha }_k\left\langle {\rho }_k{\underline{v}}_k\right\rangle_k\right)=\epsilon {\alpha }_k\left\langle {r}_k\right\rangle_k+\frac{1}{V}{\int }_{{A}_{{Ik}}}^{}{\dot{m}}_k\mathrm{d}a. $$(64)

Now, two different notations will be introduced. First, the phase average of the product between the density and velocity will be rewritten as: ρ k v ̲ k k ρ k k v ̲ k ̿ k $$ \left\langle {\rho }_k{\underline{v}}_k\right\rangle_k\stackrel{\scriptscriptstyle\mathrm{def}}{=}\left\langle {\rho }_k\right\rangle_k{\stackrel{\text{=}{{\underline{v}}_k}}^k $$(65)which defines the Favre averaged velocity v ̲ k ̿ k $ {\stackrel{\text{=}{{\underline{v}}_k}}^k$. The Favre average has been introduced in the compressible flow theories in order to avoid the appearance of double correlations between density fluctuations and velocity fluctuations. The mean velocity v ̲ k ̿ k $ {\stackrel{\text{=}{{\underline{v}}_k}}^k$ is the center-of-mass velocity of the k phase included in the REV. The last term in the RHS of equation (64) corresponds to the phase k volumetric production rate due to phase change, and we introduce the following special notation for it: Γ k 1 V A Ik m ̇ k d a . $$ {\mathrm{\Gamma }}_k\stackrel{\scriptscriptstyle\mathrm{def}}{=}\frac{1}{V}{\int }_{{A}_{{Ik}}}^{}{\dot{m}}_k\mathrm{d}{a}. $$(66)

Multiplying the last equation (38) by δI followed by volume averaging, we obtain: k Γ k = 0 $$ \sum_k^{}{\mathrm{\Gamma }}_k=0 $$(67)showing that there is no mass accumulation on the interfaces.

4.2 Species mass balance equation

Putting ψ k = Y ik ,   J ̲ k = j ̲ ik ,   ϕ k = r ik $ {\psi }_k={Y}_{{ik}},\enspace {\underline{J}}_k={\underline{j}}_{{ik}},\enspace {\phi }_k={r}_{{ik}}$ in the equation (62), the averaged species mass balance equation is obtained: t ( ε α k ρ k Y ik k ) + · ( ε α k ρ k Y ik v ̲ k k ) = 1 V A Ik ( m ̇ k Y ik - j ̲ ik · n ̲ k ) d a - · ( ε α k j ̲ ik k ) + ε α k r ik k . $$ \frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_k\left\langle {\rho }_k{Y}_{{ik}}\right\rangle_k\right)+\nabla \cdot \left(\epsilon {\alpha }_k\left\langle {\rho }_k{Y}_{{ik}}{\underline{v}}_k\right\rangle_k\right)=\frac{1}{V}{\int }_{{A}_{{Ik}}}^{}\left({\dot{m}}_k{Y}_{{ik}}-{\underline{j}}_{{ik}}\cdot {\underline{n}}_k\right)\mathrm{d}a-\nabla \cdot \left(\epsilon {\alpha }_k\left\langle {\underline{j}}_{{ik}}\right\rangle_k\right)+\epsilon {\alpha }_k\left\langle {r}_{{ik}}\right\rangle_k. $$(68)

Multiplying the second equation (39) by δI followed by volume averaging, the following averaged jump condition is obtained: k ( Γ k Y ik ̅ ̅ I - a Ik j ̲ ik · n ̲ k I ) = 1 V A Ik r is d a . $$ \sum_k^{}\left({\mathrm{\Gamma }}_k{\overline{\overline{{Y}_{{ik}}}}}^I-{a}_{{Ik}}\left\langle {\underline{j}}_{{ik}}\cdot {\underline{n}}_k\right\rangle_I\right)=\frac{1}{V}{\int }_{{A}_{{Ik}}}^{}{r}_{{is}}\mathrm{d}{a}. $$(69)where the following averages are defined: j ̲ ik · n ̲ k δ I a Ik j ̲ ik · n ̲ k I $$ \left\langle {\underline{j}}_{{ik}}\cdot {\underline{n}}_k{\delta }_I\right\rangle\stackrel{\scriptscriptstyle\mathrm{def}}{=}{a}_{{Ik}}\left\langle {\underline{j}}_{{ik}}\cdot {\underline{n}}_k\right\rangle_I $$(70) m ̇ k Y ik δ I = Γ k Y ik ̅ ̅ I $$ \left\langle {\dot{m}}_k{Y}_{{ik}}{\delta }_I\right\rangle={\mathrm{\Gamma }}_k{\overline{\overline{{Y}_{{ik}}}}}^I $$(71)where aIk = 〈δI〉 is the interfacial area concentration seen by phase k (including the wall interface), j ̲ ik · n ̲ k I $ \left\langle {\underline{j}}_{{ik}}\cdot {\underline{n}}_k\right\rangle_I$ is an interfacial average of the normal diffusive flux and Y ik ̅ ̅ I $ {\overline{\overline{{Y}_{{ik}}}}}^I$ is the interfacial average of the mass fraction weighted by phase change.

4.3 Momentum balance equation

Putting ψ k = v ̲ k ,   J ̲ k = - σ ̲ ̲ k ,   ϕ k = ρ k g ̲ + r k v ̲ k r $ {\psi }_k={\underline{v}}_k,\enspace {\underline{J}}_k=-{\underline{\underline{\sigma }}}_k,\enspace {\phi }_k={\rho }_k\underline{g}+{r}_k{\underline{v}}_k^r$ in the equation (62), the averaged momentum balance equation is obtained: t ( ε α k ρ k v ̲ k k ) + · ( ε α k ρ k v ̲ k v ̲ k k ) = 1 V A Ik ( m ̇ k v ̲ k + σ ̲ ̲ k · n ̲ k ) d a + · ( ε α k σ ̲ ̲ k k ) + ε α k ρ k k g ̲ + ε α k r k v ̲ k r k . $$ \frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_k\left\langle {\rho }_k{\underline{v}}_k\right\rangle_k\right)+\nabla \cdot \left(\epsilon {\alpha }_k\left\langle {\rho }_k{\underline{v}}_k{\underline{v}}_k\right\rangle_k\right)=\frac{1}{V}{\int }_{{A}_{{Ik}}}^{}\left({\dot{m}}_k{\underline{v}}_k+{\underline{\underline{\sigma }}}_k\cdot {\underline{n}}_k\right)\mathrm{d}a+\nabla \cdot \left(\epsilon {\alpha }_k\left\langle {\underline{\underline{\sigma }}}_k\right\rangle_k\right)+\epsilon {\alpha }_k\left\langle {\rho }_k\right\rangle_k\underline{g}+\epsilon {\alpha }_k\left\langle {r}_k{\underline{v}}_k^r\right\rangle_k. $$(72)

We will introduce a new notation for the set of momentum interfacial terms: M ̲ k ( m ̇ k v ̲ k + σ ̲ ̲ k · n ̲ k ) δ I = 1 V A Ik ( m ̇ k v ̲ k + σ ̲ ̲ k · n ̲ k ) d a . $$ {\underline{M}}_k\stackrel{\scriptscriptstyle\mathrm{def}}{=}\left\langle \left({\dot{m}}_k{\underline{v}}_k+{\underline{\underline{\sigma }}}_k\cdot {\underline{n}}_k\right){\delta }_I\right\rangle=\frac{1}{V}{\int }_{{A}_{{Ik}}}^{}\left({\dot{m}}_k{\underline{v}}_k+{\underline{\underline{\sigma }}}_k\cdot {\underline{n}}_k\right)\mathrm{d}{a}. $$(73)

Multiplying the jump condition (41) by δI and averaging, the following averaged jump condition is obtained: k M ̲ k = M ̲ I F ̲ I δ I $$ \sum_k^{}{\underline{M}}_k={\underline{M}}_I\stackrel{\scriptscriptstyle\mathrm{def}}{=}\left\langle {\underline{F}}_I{\delta }_I\right\rangle$$(74)where M ̲ I $ {\underline{M}}_I$ is the interfacial momentum source due to the surface tension.

4.4 Total energy balance equation

Putting ψ k = e k + v k 2 2 ,   J ̲ k = q ̲ k - σ ̲ ̲ k · v ̲ k ,   ϕ k = ρ k g ̲ · v ̲ k $ {\psi }_k={e}_k+\frac{{{v}_k}^2}{2},\enspace {\underline{J}}_k={\underline{q}}_k-{\underline{\underline{\sigma }}}_k\cdot {\underline{v}}_k,\enspace {\phi }_k={\rho }_k\underline{g}\cdot {\underline{v}}_k$ in the equation (62), the averaged total energy balance equation is obtained: t ( ε α k ρ k ( e k + v k 2 2 ) k ) + · ( ε α k ρ k ( e k + v k 2 2 ) v ̲ k k ) = 1 V A Ik ( m ̇ k ( e k + v k 2 2 ) - ( q ̲ k - σ ̲ ̲ k · v ̲ k ) · n ̲ k ) d a - · ( ε α k q ̲ k - σ ̲ ̲ k · v ̲ k k ) + ε α k ρ k v ̲ k k · g ̲ . $$ \frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_k\left\langle {\rho }_k\left({e}_k+\frac{{{v}_k}^2}{2}\right)\right\rangle_k\right)+\nabla \cdot \left(\epsilon {\alpha }_k\left\langle {\rho }_k\left({e}_k+\frac{{{v}_k}^2}{2}\right){\underline{v}}_k\right\rangle_k\right)=\frac{1}{V}{\int }_{{A}_{{Ik}}}^{}\left({\dot{m}}_k\left({e}_k+\frac{{{v}_k}^2}{2}\right)-\left({\underline{q}}_k-{\underline{\underline{\sigma }}}_k\cdot {\underline{v}}_k\right)\cdot {\underline{n}}_k\right)\mathrm{d}a-\nabla \cdot \left(\epsilon {\alpha }_k\left\langle {\underline{q}}_k-{\underline{\underline{\sigma }}}_k\cdot {\underline{v}}_k\right\rangle_k\right)+\epsilon {\alpha }_k\left\langle {\rho }_k{\underline{v}}_k\right\rangle_k\cdot \underline{g}. $$(75)

Now, we can define: Q k 1 V A Ik ( m ̇ k ( e k + v k 2 2 ) - ( q ̲ k - σ ̲ ̲ k · v ̲ k ) · n ̲ k ) d a . $$ {Q}_k\stackrel{\scriptscriptstyle\mathrm{def}}{=}\frac{1}{V}{\int }_{{A}_{{Ik}}}^{}\left({\dot{m}}_k\left({e}_k+\frac{{{v}_k}^2}{2}\right)-\left({\underline{q}}_k-{\underline{\underline{\sigma }}}_k\cdot {\underline{v}}_k\right)\cdot {\underline{n}}_k\right)\mathrm{d}a. $$(76)

Multiplying the jump condition (43) by δI and averaging the resulting equation, the averaged form of the total energy jump condition is obtained: k Q k = Q I E I δ I . $$ \sum_k^{}{Q}_k={Q}_I\stackrel{\scriptscriptstyle\mathrm{def}}{=}\left\langle {E}_I{\delta }_I\rangle. $$(77)

4.5 Enthalpy balance equation

Putting ψ k = h k ,   J ̲ k = q ̲ k ,   ϕ k = D k p k Dt + τ ̲ ̲ k : v ̲ k + r k h k r $ {\psi }_k={h}_k,\enspace {\underline{J}}_k={\underline{q}}_k,\enspace {\phi }_k=\frac{{D}_k{p}_k}{{Dt}}+{\underline{\underline{\tau }}}_k:\nabla {\underline{v}}_k+{r}_k{h}_k^r$ in the equation (62), the averaged enthalpy balance equation is obtained: t ( ε α k ρ k h k k ) + · ( ε α k ρ k h k v ̲ k k ) = 1 V A Ik ( m ̇ k h k - q ̲ k · n ̲ k ) da - · ( ε α k q ̲ k k ) + ε α k D k p k Dt + τ ̲ ̲ k : v ̲ k + r k h k r k . $$ \frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_k\left\langle {\rho }_k{h}_k\right\rangle_k\right)+\nabla \cdot \left(\epsilon {\alpha }_k\left\langle {\rho }_k{h}_k{\underline{v}}_k\right\rangle_k\right)=\frac{1}{V}{\int }_{{A}_{{Ik}}}^{}\left({\dot{m}}_k{h}_k-{\underline{q}}_k\cdot {\underline{n}}_k\right){da}-\nabla \cdot \left(\epsilon {\alpha }_k\left\langle {\underline{q}}_k\right\rangle_k\right)+\epsilon {\alpha }_k\left\langle \frac{{D}_k{p}_k}{{Dt}}+{\underline{\underline{\tau }}}_k:\nabla {\underline{v}}_k+{r}_k{h}_k^r\right\rangle_k. $$(78)

And the enthalpy mean jump condition reads (Eq. (49)): k 1 V A I ( m ̇ k h k - q ̲ k · n ̲ k ) d a = 1 V A I H I d a 0 $$ \sum_k^{}\frac{1}{V}{\int }_{{A}_I}^{}\left({\dot{m}}_k{h}_k-{\underline{q}}_k\cdot {\underline{n}}_k\right)\mathrm{d}a=\frac{1}{V}{\int }_{{A}_I}^{}{H}_I\mathrm{d}a\cong 0 $$(79)where the term involving HI can be neglected according to [15].

4.6 Internal energy balance equation

Putting ψ k = e k ,   J ̲ k = q ̲ k ,   ϕ k = - p k · v ̲ k + τ ̲ ̲ k : v ̲ k + r k h k r $ {\psi }_k={e}_k,\enspace {\underline{J}}_k={\underline{q}}_k,\enspace {\phi }_k={-p}_k\nabla \cdot {\underline{v}}_k+{\underline{\underline{\tau }}}_k:\nabla {\underline{v}}_k+{r}_k{h}_k^r$ in the equation (62), the averaged internal energy balance equation is obtained: t ( ε α k ρ k e k k ) + · ( ε α k ρ k e k v ̲ k k ) = 1 V A Ik ( m ̇ k e k - q ̲ k · n ̲ k ) d a - · ( ε α k q ̲ k k ) + ε α k τ ̲ ̲ k : v ̲ k - p k · v ̲ k + r k e k r k . $$ \frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_k\left\langle {\rho }_k{e}_k\right\rangle_k\right)+\nabla \cdot \left(\epsilon {\alpha }_k\left\langle {\rho }_k{e}_k{\underline{v}}_k\right\rangle_k\right)=\frac{1}{V}{\int }_{{A}_{{Ik}}}^{}\left({\dot{m}}_k{e}_k-{\underline{q}}_k\cdot {\underline{n}}_k\right)\mathrm{d}a-\nabla \cdot \left(\epsilon {\alpha }_k\left\langle {\underline{q}}_k\right\rangle_k\right)+\epsilon {\alpha }_k\left\langle {\underline{\underline{\tau }}}_k:\nabla {\underline{v}}_k{-p}_k\nabla \cdot {\underline{v}}_k+{r}_k{e}_k^r\right\rangle_k. $$(80)

And the averaged internal energy jump condition reads: k 1 V A I ( m ̇ k e k - q ̲ k · n ̲ k ) d a = 1 V A I ϵ I d a 0 $$ \sum_k^{}\frac{1}{V}{\int }_{{A}_I}^{}\left({\dot{m}}_k{e}_k-{\underline{q}}_k\cdot {\underline{n}}_k\right)\mathrm{d}a=\frac{1}{V}{\int }_{{A}_I}^{}{\epsilon }_I\mathrm{d}a\cong 0 $$(81)where the term involving ϵI can be neglected according to [15].

4.7 Entropy balance equation

Putting ψ k = s k ,   J ̲ k = q ̲ k / T k ,   ϕ k = τ ̲ ̲ k : v ̲ k T k + q ̲ k · ( 1 / T k ) + r k s k r $ {\psi }_k={s}_k,\enspace {\underline{J}}_k={\underline{q}}_k/{T}_k,\enspace {\phi }_k=\frac{{\underline{\underline{\tau }}}_k:\nabla {\underline{v}}_k}{{T}_k}+{\underline{q}}_k\cdot \nabla \left(1/{T}_k\right)+{r}_k{s}_k^r$ in the equation (62), the averaged entropy balance equation is obtained: t ( ε α k ρ k s k k ) + · ( ε α k ρ k s k v ̲ k k ) = 1 V A Ik ( m ̇ k s k - q ̲ k T k · n ̲ k ) d a - · ( ε α k q ̲ k T k k ) + ε α k τ ̲ ̲ k : v ̲ k T k + q ̲ k · ( 1 / T k ) + r k s k r k . $$ \frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_k\left\langle {\rho }_k{s}_k\right\rangle_k\right)+\nabla \cdot \left(\epsilon {\alpha }_k\left\langle {\rho }_k{s}_k{\underline{v}}_k\right\rangle_k\right)=\frac{1}{V}{\int }_{{A}_{{Ik}}}^{}\left({\dot{m}}_k{s}_k-\frac{{\underline{q}}_k}{{T}_k}\cdot {\underline{n}}_k\right)\mathrm{d}a-\nabla \cdot \left(\epsilon {\alpha }_k\left\langle \frac{{\underline{q}}_k}{{T}_k}\right\rangle_k\right)+\epsilon {\alpha }_k\left\langle \frac{{\underline{\underline{\tau }}}_k:\nabla {\underline{v}}_k}{{T}_k}+{\underline{q}}_k\cdot \nabla \left(1/{T}_k\right)+{r}_k{s}_k^r\right\rangle_k. $$(82)

The averaged entropy jump condition is obtained from (59): k 1 V A I ( m ̇ k s k - q ̲ k T k · n ̲ k ) d a 0 . $$ \sum_k^{}\frac{1}{V}{\int }_{{A}_I}^{}\left({\dot{m}}_k{s}_k-\frac{{\underline{q}}_k}{{T}_k}\cdot {\underline{n}}_k\right)\mathrm{d}a\cong 0. $$(83)where (60) has been taken into account.

Up to now, the mass, momentum, and energy averaged balance equations have been derived in their exact form. Nevertheless, these equations cannot be used directly since they are expressed in terms of averages of products of local quantities and integral terms. Instead, we must express all these unknown terms by closure relations. This will be done in the next sections.

5 The two-fluid model in porous medium

5.1 Useful form of the mass balance equation

Denoting by Sk the source term due to chemical reactions: S k ε α k r k k $$ {S}_k\stackrel{\scriptscriptstyle\mathrm{def}}{=}\epsilon {\alpha }_k\left\langle {r}_k\right\rangle_k $$(84)and using the definitions (65) and (66), the mass balance equation for phase k becomes: t ( ε α k ρ k k ) + · ( ε α k ρ k k v ̲ k ̿ k ) = S k + Γ k $$ \frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_k\left\langle {\rho }_k\right\rangle_k\right)+\nabla \cdot \left(\epsilon {\alpha }_k\left\langle {\rho }_k\right\rangle_k{\stackrel{\text{=}{{\underline{v}}_k}}^k\right)={S}_k+{\mathrm{\Gamma }}_k $$(85)where there are two source terms in the RHS: one due to chemical reactions and the other due to phase change. These two terms must be modelled by appropriate closure laws.

5.2 Useful form of the species mass balance equation

In what follows, we will denote the partial density of species i in phase k as: ρ ik ρ k Y ik . $$ {\rho }_{{ik}}\stackrel{\scriptscriptstyle\mathrm{def}}{=}{\rho }_k{Y}_{{ik}}. $$(86)

We will also assume that the diffusion flux j ̲ ik $ {\underline{j}}_{{ik}}$ is modelled by Fick’s law: j ̲ ik = - D ik ρ ik . $$ {\underline{j}}_{{ik}}=-{D}_{{ik}}\nabla {\rho }_{{ik}}. $$(87)

Substituting these two relations as well as (70) and (71) in (68), the following equation is obtained: t ( ε α k ρ ik k ) + · ( ε α k ρ ik k v ̲ k ̿ k ) = Γ k Y ik ̅ ̅ I + a Ik D ik ρ ik · n ̲ k I + · ( ε α k D ik ρ ik k ) + S ik $$ \frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_k\left\langle {\rho }_{{ik}}\right\rangle_k\right)+\nabla \cdot \left(\epsilon {\alpha }_k\left\langle {\rho }_{{ik}}\right\rangle_k{\stackrel{\text{=}{{\underline{v}}_k}}^k\right)={\mathrm{\Gamma }}_k{\overline{\overline{{Y}_{{ik}}}}}^I+{a}_{{Ik}}\left\langle {D}_{{ik}}\nabla {\rho }_{{ik}}\cdot {\underline{n}}_k\right\rangle_I+\nabla \cdot \left(\epsilon {\alpha }_k\left\langle {D}_{{ik}}\nabla {\rho }_{{ik}}\right\rangle_k\right)+{S}_{{ik}} $$(88)where the last term is due to chemical reactions: S ik ε α k r ik k . $$ {S}_{{ik}}\stackrel{\scriptscriptstyle\mathrm{def}}{=}\epsilon {\alpha }_k\left\langle {r}_{{ik}}\right\rangle_k. $$(89)

Assuming that the diffusivity of the species i in phase k is constant at the scale of the averaging volume, the diffusive term can be rewritten as: · ( ε α k D ik ρ ik k ) = · ( D ik X k ρ ik ) = · ( D ik ( ( ε α k ρ ik k ) + ρ ik n ̲ k δ I ) ) $$ \nabla \cdot \left(\epsilon {\alpha }_k\left\langle {D}_{{ik}}\nabla {\rho }_{{ik}}\right\rangle_k\right)=\nabla \cdot \left({D}_{{ik}}\left\langle {X}_k\nabla {\rho }_{{ik}}\right\rangle\right)=\nabla \cdot \left({D}_{{ik}}\left(\nabla \left(\epsilon {\alpha }_k\left\langle {\rho }_{{ik}}\right\rangle_k\right)+\left\langle {\rho }_{{ik}}{\underline{n}}_k{\delta }_I\right\rangle\right)\right) $$(90)where the theorem relating the average of a gradient to the gradient of the average has been used.

Substituting (86) and (90) into (88), the following equation is obtained: t ( ε α k ρ k Y ik k ) + · ( ε α k ρ k Y ik v ̲ k k ) = Γ k Y ik ̅ ̅ I + a Ik D ik ρ ik · n ̲ k I + · ( D ik ( ( ε α k ρ ik k ) + ρ ik n ̲ k δ I ) ) + S ik . $$ \frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_k\left\langle {\rho }_k{Y}_{{ik}}\right\rangle_k\right)+\nabla \cdot \left(\epsilon {\alpha }_k\left\langle {\rho }_k{Y}_{{ik}}{\underline{v}}_k\right\rangle_k\right)={\mathrm{\Gamma }}_k{\overline{\overline{{Y}_{{ik}}}}}^I+{a}_{{Ik}}\left\langle {D}_{{ik}}\nabla {\rho }_{{ik}}\cdot {\underline{n}}_k\right\rangle_I+\nabla \cdot \left({D}_{{ik}}\left(\nabla \left(\epsilon {\alpha }_k\left\langle {\rho }_{{ik}}\right\rangle_k\right)+\left\langle {\rho }_{{ik}}{\underline{n}}_k{\delta }_I\right\rangle\right)\right)+{S}_{{ik}}. $$(91)

Following [18], the term ρ ik n ̲ k δ I $ \left\langle {\rho }_{{ik}}{\underline{n}}_k{\delta }_I\right\rangle$ is neglected and the term a Ik D ik ρ ik · n ̲ k I $ {a}_{{Ik}}\left\langle {D}_{{ik}}\nabla {\rho }_{{ik}}\cdot {\underline{n}}_k\right\rangle_I$ is attributed to the adsorption/desorption phenomena: Σ ik a Ik D ik ρ ik · n ̲ k I $$ {\mathrm{\Sigma }}_{{ik}}\stackrel{\scriptscriptstyle\mathrm{def}}{=}{a}_{{Ik}}\left\langle {D}_{{ik}}\nabla {\rho }_{{ik}}\cdot {\underline{n}}_k\right\rangle_I $$(92)

The final form of the equation (91) reads: t ( ε α k ρ k k Y ik ̿ k ) + · ( ε α k ρ k k Y ik v ̲ k ̿ k ) = · ( D ik ( ε α k ρ k k Y ik ̿ k ) ) + Γ k Y ik Γ + Σ ik + S ik . $$ \frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_k\left\langle {\rho }_k\right\rangle_k{\stackrel{\text{=}{{Y}_{{ik}}}}^k\right)+\nabla \cdot \left(\epsilon {\alpha }_k\left\langle {\rho }_k\right\rangle_k{\stackrel{\text{=}{{Y}_{{ik}}{\underline{v}}_k}}^k\right)=\nabla \cdot \left({D}_{{ik}}\nabla \left(\epsilon {\alpha }_k\left\langle {\rho }_k\right\rangle_k{\stackrel{\text{=}{{Y}_{{ik}}}}^k\right)\right)+{\mathrm{\Gamma }}_k{Y}_{{ik}}^{\mathrm{\Gamma }}+{\mathrm{\Sigma }}_{{ik}}+{S}_{{ik}}. $$(93)

5.3 Useful form of the momentum balance equation

Introducing the Favre average and the definition (73), the momentum balance equation (72) becomes: t ( ε α k ρ k k v ̲ k ̿ k ) + · ( ε α k ρ k k v ̲ k v ̲ k ̅ ̅ k ) = 1 V A kf ( m ̇ k v ̲ k + ( τ ̲ ̲ k - p k I ̲ ̲ ) . n ̲ k ) d a + 1 V A ks ( m ̇ k v ̲ k + ( τ ̲ ̲ k - p k I ̲ ̲ ) . n ̲ k ) d a - ( ε α k p k k ) + . ( ε α k τ ̲ ̲ k k ) + ε α k ρ k k g ̲   + ε α k r k v ̲ k r k . $$ \frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_k\left\langle {\rho }_k\right\rangle_k{\stackrel{\text{=}{{\underline{v}}_k}}^k\right)+\nabla \cdot \left(\epsilon {\alpha }_k\left\langle {\rho }_k\right\rangle_k{\overline{\overline{{\underline{v}}_k{\underline{v}}_k}}}^k\right)=\frac{1}{V}{\int }_{{A}_{{kf}}}^{}\left({\dot{m}}_k{\underline{v}}_k+\left({\underline{\underline{\tau }}}_k-{p}_k\underline{\underline{I}}\right).{\underline{n}}_k\right)\mathrm{d}a+\frac{1}{V}{\int }_{{A}_{{ks}}}^{}\left({\dot{m}}_k{\underline{v}}_k+\left({\underline{\underline{\tau }}}_k-{p}_k\underline{\underline{I}}\right).{\underline{n}}_k\right)\mathrm{d}a-\nabla \left(\epsilon {\alpha }_k\left\langle {p}_k\right\rangle_k\right)+\nabla.\left(\epsilon {\alpha }_k\left\langle {\underline{\underline{\tau }}}_k\right\rangle_k\right)+\epsilon {\alpha }_k\left\langle {\rho }_k\right\rangle_k\underline{g}\enspace +\epsilon {\alpha }_k\left\langle {r}_k{\underline{v}}_k^r\right\rangle_k. $$(94)

In this equation, the total stress tensor has been decomposed into a pressure term and a viscous stress tensor (Table 1). The interfacial term has been split into two integrals: the first integral concerns the gas-liquid interface Akf and the second one concerns the wall surface Aks. In the LHS of (94), we have the Favre average of the tensorial product of the velocity by itself v ̲ k v ̲ k ̅ ̅ k $ {\overline{\overline{{\underline{v}}_k{\underline{v}}_k}}}^k$. In order to make the dispersion tensor appear, the local velocity is decomposed into its mean value and a fluctuating component: v ̲ k v ̲ k ̿ k + v ̲ k ' . $$ {\underline{v}}_k\stackrel{\scriptscriptstyle\mathrm{def}}{=}{\stackrel{\text{=}{{\underline{v}}_k}}^k+{\underline{v}}_k^{\prime}. $$(95)

The Favre average of the equation (95) shows that v ' ̲ k ̿ k = 0 $ {\stackrel{\text{=}{{\underline{{v}^{\prime}}_k}}^k=0$, i.e., the average of a fluctuation is zero, and we deduce immediately that the average of a product is equal to the product of the averages, in addition to the average of the product of fluctuations: v ̲ k v ̲ k ̅ ̅ k = v ̲ k ̿ k v ̲ k ̿ k + v ̲ k ' v ̲ k ' ̅ ̅ k . $$ {\overline{\overline{{\underline{v}}_k{\underline{v}}_k}}}^k={\stackrel{\text{=}{{\underline{v}}_k}}^k{\stackrel{\text{=}{{\underline{v}}_k}}^k+{\overline{\overline{{\underline{v}}_k\prime{\underline{v}}_k\prime}}^k. $$(96)

Substituting (96) into (94) and introducing the following notation for the dispersion tensor: τ ̲ ̲ k T - ρ k k v ̲ k v ̲ k ̅ ̅ k . $$ {\underline{\underline{\tau }}}_k^T\stackrel{\scriptscriptstyle\mathrm{def}}{=}-\left\langle {\rho }_k\right\rangle_k{\overline{\overline{{\underline{v}}_k\mathrm{\prime}{\underline{v}}_k\mathrm{\prime}}}^k. $$(97)

The tensor τ ̲ ̲ k T $ {\underline{\underline{\tau }}}_k^T$ is called the Reynolds stress tensor in the turbulence community when a time or ensemble average is used. Here, we prefer to call it the dispersion tensor since a spatial average is used. Substituting (96) and (97) into (94), the momentum equation becomes: t ( ε α k ρ k k v ̲ k ̿ k ) + · ( ε α k ρ k k v ̲ k ̿ k v ̲ k ̿ k ) = 1 V A Ik ( m ̇ k v ̲ k + ( τ ̲ ̲ k - p k I ̲ ̲ ) · n ̲ k ) d a + 1 V A wk ( m ̇ k v ̲ k + ( τ ̲ ̲ k - p k I ̲ ̲ ) · n ̲ k ) d a - ( ε α k p k k ) + · ( ε α k ( τ ̲ ̲ k k + τ ̲ ̲ k T ) ) + ε α k ρ k k g ̲   + ε α k r k v ̲ k r k . $$ \frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_k\left\langle {\rho }_k\right\rangle_k{\stackrel{\text{=}{{\underline{v}}_k}}^k\right)+\nabla \cdot \left(\epsilon {\alpha }_k\left\langle {\rho }_k\right\rangle_k{\stackrel{\text{=}{{\underline{v}}_k}}^k{\stackrel{\text{=}{{\underline{v}}_k}}^k\right)=\frac{1}{V}{\int }_{{A}_{{Ik}}}^{}\left({\dot{m}}_k{\underline{v}}_k+\left({\underline{\underline{\tau }}}_k-{p}_k\underline{\underline{I}}\right)\cdot {\underline{n}}_k\right)\mathrm{d}a+\frac{1}{V}{\int }_{{A}_{{wk}}}^{}\left({\dot{m}}_k{\underline{v}}_k+\left({\underline{\underline{\tau }}}_k-{p}_k\underline{\underline{I}}\right)\cdot {\underline{n}}_k\right)\mathrm{d}a-\nabla \left(\epsilon {\alpha }_k\left\langle {p}_k\right\rangle_k\right)+\nabla \cdot \left(\epsilon {\alpha }_k\left(\left\langle {\underline{\underline{\tau }}}_k\right\rangle_k+{\underline{\underline{\tau }}}_k^T\right)\right)+\epsilon {\alpha }_k\left\langle {\rho }_k\right\rangle_k\underline{g}\enspace +\epsilon {\alpha }_k\left\langle {r}_k{\underline{v}}_k^r\right\rangle_k. $$(98)

Following [19], we can use the momentum jump condition (74) in order to introduce the surface tension, for example, in the liquid phase: 1 V A Ik ( m ̇ L v ̲ L + ( τ ̲ ̲ L - p L I ̲ ̲ ) · n ̲ L ) d a = - 1 V A Ik ( m ̇ G v ̲ G + ( τ ̲ ̲ G - p G I ̲ ̲ ) · n ̲ G - s σ + 2 H L σ n ̲ L ) d a . $$ \frac{1}{V}{\int }_{{A}_{{Ik}}}^{}\left({\dot{m}}_L{\underline{v}}_L+\left({\underline{\underline{\tau }}}_L-{p}_L\underline{\underline{I}}\right)\cdot {\underline{n}}_L\right)\mathrm{d}a=-\frac{1}{V}{\int }_{{A}_{{Ik}}}^{}\left({\dot{m}}_G{\underline{v}}_G+\left({\underline{\underline{\tau }}}_G-{p}_G\underline{\underline{I}}\right)\cdot {\underline{n}}_G-{\nabla }_s\sigma +2{H}_L\sigma {\underline{n}}_L\right)\mathrm{d}a. $$(99)

The first term, due to phase change, is sometimes called the recoil force, and we can use the interfacial average weighted by phase change as in (71) to express it: 1 V A Ik m ̇ k v ̲ k d a = Γ k v ̲ k ̅ ̅ I Γ k V ̲ Γ . $$ \frac{1}{V}{\int }_{{A}_{{Ik}}}^{}{\dot{m}}_k{\underline{v}}_k\mathrm{d}a={\mathrm{\Gamma }}_k{\overline{\overline{{\underline{v}}_k}}}^I\stackrel{\scriptscriptstyle\mathrm{def}}{=}{\mathrm{\Gamma }}_k{\underline{V}}_{\mathrm{\Gamma }}. $$(100)

In the last definition, it is not useful to put a k index on the mean velocity weighted by phase change V ̲ Γ $ {\underline{V}}_{\mathrm{\Gamma }}$ since this mean velocity should not depends on the phase considered [20, 21].

Substituting (99) into (98) written for the liquid phase: t ( ε α L ρ L L v ̲ L ̿ L ) + · ( ε α L ρ L L v ̲ L ̿ L v ̲ L ̿ L ) = = - 1 V A I ( m ̇ G v ̲ G - ( τ ̲ ̲ G - p G I ̲ ̲ ) · n ̲ L - s σ + 2 H L σ n ̲ L ) d a + 1 V A wL ( m ̇ L v ̲ L + ( τ ̲ ̲ L - p L I ̲ ̲ ) · n ̲ L ) d a - ( ε α L p L L ) + · ( ε α L ( τ ̲ ̲ L L + τ ̲ ̲ L T ) ) + ε α L ρ L L g ̲   + ε α L r L v ̲ L r L $$ \frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_L\left\langle {\rho }_L\right\rangle_L{\stackrel{\text{=}{{\underline{v}}_L}}^L\right)+\nabla \cdot \left(\epsilon {\alpha }_L\left\langle {\rho }_L\right\rangle_L{\stackrel{\text{=}{{\underline{v}}_L}}^L{\stackrel{\text{=}{{\underline{v}}_L}}^L\right)==-\frac{1}{V}{\int }_{{A}_I}^{}\left({\dot{m}}_G{\underline{v}}_G-\left({\underline{\underline{\tau }}}_G-{p}_G\underline{\underline{I}}\right)\cdot {\underline{n}}_L-{\nabla }_s\sigma +2{H}_L\sigma {\underline{n}}_L\right)\mathrm{d}a+\frac{1}{V}{\int }_{{A}_{{wL}}}^{}\left({\dot{m}}_L{\underline{v}}_L+\left({\underline{\underline{\tau }}}_L-{p}_L\underline{\underline{I}}\right)\cdot {\underline{n}}_L\right)\mathrm{d}a-\nabla \left(\epsilon {\alpha }_L\left\langle {p}_L\right\rangle_L\right)+\nabla \cdot \left(\epsilon {\alpha }_L\left(\left\langle {\underline{\underline{\tau }}}_L\right\rangle_L+{\underline{\underline{\tau }}}_L^T\right)\right)+\epsilon {\alpha }_L\left\langle {\rho }_L\right\rangle_L\underline{g}\enspace +\epsilon {\alpha }_L\left\langle {r}_L{\underline{v}}_L^r\right\rangle_L $$(101)

Decomposing pL and pG into their mean and fluctuating components, the previous equation becomes: t ( ε α L ρ L L v ̲ L ̿ L ) + · ( ε α L ρ L L v ̲ L ̿ L v ̲ L ̿ L ) = - p G G V A I n ̲ L d a - 1 V A I ( m ̇ G v ̲ G - ( τ ̲ ̲ G - p G I ̲ ̲ ) · n ̲ L - s σ + 2 H L σ n ̲ L ) d a - p L L V A wL n ̲ L d a + 1 V A wL ( m ̇ L v ̲ L + ( τ ̲ ̲ L - p L I ̲ ̲ ) · n ̲ L ) d a - ( ε α L p L L ) + · ( ε α L ( τ ̲ ̲ L L + τ ̲ ̲ L T ) ) + ε α L ρ L L g ̲   + ε α L r L v ̲ L r L . $$ \frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_L\left\langle {\rho }_L\right\rangle_L{\stackrel{\text{=}{{\underline{v}}_L}}^L\right)+\nabla \cdot \left(\epsilon {\alpha }_L\left\langle {\rho }_L\right\rangle_L{\stackrel{\text{=}{{\underline{v}}_L}}^L{\stackrel{\text{=}{{\underline{v}}_L}}^L\right)=-\frac{\left\langle {p}_G\right\rangle_G}{V}{\int }_{{A}_I}^{}{\underline{n}}_L\mathrm{d}a-\frac{1}{V}{\int }_{{A}_I}^{}\left({\dot{m}}_G{\underline{v}}_G-\left({\underline{\underline{\tau }}}_G-{p\mathrm{\prime}_G\underline{\underline{I}}\right)\cdot {\underline{n}}_L-{\nabla }_s\sigma +2{H}_L\sigma {\underline{n}}_L\right)\mathrm{d}a-\frac{\left\langle {p}_L\right\rangle_L}{V}{\int }_{{A}_{{wL}}}^{}{\underline{n}}_L\mathrm{d}a+\frac{1}{V}{\int }_{{A}_{{wL}}}^{}\left({\dot{m}}_L{\underline{v}}_L+\left({\underline{\underline{\tau }}}_L-{p\mathrm{\prime}_L\underline{\underline{I}}\right)\cdot {\underline{n}}_L\right)\mathrm{d}a-\nabla \left(\epsilon {\alpha }_L\left\langle {p}_L\right\rangle_L\right)+\nabla \cdot \left(\epsilon {\alpha }_L\left(\left\langle {\underline{\underline{\tau }}}_L\right\rangle_L+{\underline{\underline{\tau }}}_L^T\right)\right)+\epsilon {\alpha }_L\left\langle {\rho }_L\right\rangle_L\underline{g}\enspace +\epsilon {\alpha }_L\left\langle {r}_L{\underline{v}}_L^r\right\rangle_L. $$(102)

AI,k being decomposed into the interfacial area AI and the wall area in contact to the liquid AwL, the first and third terms in the RHS of (102) can be transformed into: - p G G V A I n ̲ L d a - p L L V A wL n ̲ L d a = p G G ( ε α L ) + ( p G G - p L L ) 1 V A wL n ̲ L d a . $$ -\frac{\left\langle {p}_G\right\rangle_G}{V}{\int }_{{A}_I}^{}{\underline{n}}_L\mathrm{d}a-\frac{\left\langle {p}_L\right\rangle_L}{V}{\int }_{{A}_{{wL}}}^{}{\underline{n}}_L\mathrm{d}a=\left\langle {p}_G\right\rangle_G\nabla \left(\epsilon {\alpha }_L\right)+\left(\left\langle {p}_G\right\rangle_G-\left\langle {p}_L\right\rangle_L\right)\frac{1}{V}{\int }_{{A}_{{wL}}}^{}{\underline{n}}_L\mathrm{d}a. $$(103)

Assuming that the mean curvature HL and the surface tension σ do not fluctuate, the surface tension terms in (102) can be rewritten as: - 1 V A I ( 2 H L σ n ̲ L - s σ ) d a = 2 H L σ ( ( ε α L ) + 1 V A wL n ̲ L d a ) + 1 V A I s σ d a . $$ -\frac{1}{V}{\int }_{{A}_I}^{}\left(2{H}_L\sigma {\underline{n}}_L-{\nabla }_s\sigma \right)\mathrm{d}a=2{H}_L\sigma \left(\nabla \left(\epsilon {\alpha }_L\right)+\frac{1}{V}{\int }_{{A}_{{wL}}}^{}{\underline{n}}_L\mathrm{d}a\right)+\frac{1}{V}{\int }_{{A}_I}^{}{\nabla }_s\sigma \mathrm{d}a. $$(104)

Grouping the mean pressure terms and the surface tension terms appearing in (102), we obtain: - ( ε α L p L L ) - p G G V A I n ̲ L d a - p L L V A wL n ̲ L d a - 1 V A I ( 2 H L σ n ̲ L - s σ ) d a = - ε α L p L L + ( p G G - p L L + 2 H L σ ) ( ( ε α L ) + 1 V A wL n ̲ L d a ) + 1 V A I s σ d a . $$ -\nabla \left(\epsilon {\alpha }_L\left\langle {p}_L\right\rangle_L\right)-\frac{\left\langle {p}_G\right\rangle_G}{V}{\int }_{{A}_I}^{}{\underline{n}}_L\mathrm{d}a-\frac{\left\langle {p}_L\right\rangle_L}{V}{\int }_{{A}_{{wL}}}^{}{\underline{n}}_L\mathrm{d}a-\frac{1}{V}{\int }_{{A}_I}^{}\left(2{H}_L\sigma {\underline{n}}_L-{\nabla }_s\sigma \right)\mathrm{d}a=-\epsilon {\alpha }_L\nabla \left\langle {p}_L\right\rangle_L+\left(\left\langle {p}_G\right\rangle_G-\left\langle {p}_L\right\rangle_L+2{H}_L\sigma \right)\left(\nabla \left(\epsilon {\alpha }_L\right)+\frac{1}{V}{\int }_{{A}_{{wL}}}^{}{\underline{n}}_L\mathrm{d}a\right)+\frac{1}{V}{\int }_{{A}_I}^{}{\nabla }_s\sigma \mathrm{d}a. $$(105)

The recoil force is modelled by (100) [20, 21]. Grouping all these results, the momentum equation for the liquid phase (102) becomes: t ( ε α L ρ L L v ̲ L ̿ L ) + · ( ε α L ρ L L v ̲ L ̿ L v ̲ L ̿ L ) = Γ LI V ̲ Γ I + Γ Lw V ̲ Γ w - ε α L p L L + ( p G G - p L L + 2 H L σ ) ( ( ε α L ) + 1 V A wL n ̲ L d a ) + 1 V A I s σ d a + 1 V A I ( τ ̲ ̲ G - p G I ̲ ̲ ) · n ̲ L d a + 1 V A wL ( τ ̲ ̲ L - p L I ̲ ̲ ) · n ̲ L d a + · ( ε α L ( τ ̲ ̲ L L + τ ̲ ̲ L T ) ) + ε α L ρ L L g ̲   + ε α L r L v ̲ L r L . $$ \frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_L\left\langle {\rho }_L\right\rangle_L{\stackrel{\text{=}{{\underline{v}}_L}}^L\right)+\nabla \cdot \left(\epsilon {\alpha }_L\left\langle {\rho }_L\right\rangle_L{\stackrel{\text{=}{{\underline{v}}_L}}^L{\stackrel{\text{=}{{\underline{v}}_L}}^L\right)={\mathrm{\Gamma }}_{{LI}}{\underline{V}}_{\mathrm{\Gamma I}}+{\mathrm{\Gamma }}_{{Lw}}{\underline{V}}_{\mathrm{\Gamma w}}-\epsilon {\alpha }_L\nabla \left\langle {p}_L\right\rangle_L+\left(\left\langle {p}_G\right\rangle_G-\left\langle {p}_L\right\rangle_L+2{H}_L\sigma \right)\left(\nabla \left(\epsilon {\alpha }_L\right)+\frac{1}{V}{\int }_{{A}_{{wL}}}^{}{\underline{n}}_L\mathrm{d}a\right)+\frac{1}{V}{\int }_{{A}_I}^{}{\nabla }_s\sigma \mathrm{d}a+\frac{1}{V}{\int }_{{A}_I}^{}\left({\underline{\underline{\tau }}}_G-{p\mathrm{\prime}_G\underline{\underline{I}}\right)\cdot {\underline{n}}_L\mathrm{d}a+\frac{1}{V}{\int }_{{A}_{{wL}}}^{}\left({\underline{\underline{\tau }}}_L-{p\mathrm{\prime}_L\underline{\underline{I}}\right)\cdot {\underline{n}}_L\mathrm{d}a+\nabla \cdot \left(\epsilon {\alpha }_L\left(\left\langle {\underline{\underline{\tau }}}_L\right\rangle_L+{\underline{\underline{\tau }}}_L^T\right)\right)+\epsilon {\alpha }_L\left\langle {\rho }_L\right\rangle_L\underline{g}\enspace +\epsilon {\alpha }_L\left\langle {r}_L{\underline{v}}_L^r\right\rangle_L. $$(106)

For the gas phase, we will conserve the primitive form without using the momentum jump condition. As a consequence, the equation (98) becomes for the gas phase: t ( ε α G ρ G G v ̲ G ̿ G ) + · ( ε α G ρ G G v ̲ G ̿ G v ̲ G ̿ G ) = - Γ LI V ̲ Γ I - Γ Lw V ̲ L w - ε α G p G G + 1 V A I ( τ ̲ ̲ G - p G I ̲ ̲ ) · n ̲ G d a + 1 V A wG ( τ ̲ ̲ G - p G I ̲ ̲ ) · n ̲ G d a + · ( ε α G ( τ ̲ ̲ G G + τ ̲ ̲ G T ) ) + ε α G ρ G G g ̲   + ε α G r G v ̲ G r G $$ \frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_G\left\langle {\rho }_G\right\rangle_G{\stackrel{\text{=}{{\underline{v}}_G}}^G\right)+\nabla \cdot \left(\epsilon {\alpha }_G\left\langle {\rho }_G\right\rangle_G{\stackrel{\text{=}{{\underline{v}}_G}}^G{\stackrel{\text{=}{{\underline{v}}_G}}^G\right)={-\mathrm{\Gamma }}_{{LI}}{\underline{V}}_{\mathrm{\Gamma I}}-{\mathrm{\Gamma }}_{{Lw}}{\underline{V}}_{L\mathrm{w}}-\epsilon {\alpha }_G\nabla \left\langle {p}_G\right\rangle_G+\frac{1}{V}{\int }_{{A}_I}^{}\left({\underline{\underline{\tau }}}_G-{p\mathrm{\prime}_G\underline{\underline{I}}\right)\cdot {\underline{n}}_G\mathrm{d}a+\frac{1}{V}{\int }_{{A}_{{wG}}}^{}\left({\underline{\underline{\tau }}}_G-{p\mathrm{\prime}_G\underline{\underline{I}}\right)\cdot {\underline{n}}_G\mathrm{d}a+\nabla \cdot \left(\epsilon {\alpha }_G\left(\left\langle {\underline{\underline{\tau }}}_G\right\rangle_G+{\underline{\underline{\tau }}}_G^T\right)\right)+\epsilon {\alpha }_G\left\langle {\rho }_G\right\rangle_G\underline{g}\enspace +\epsilon {\alpha }_G\left\langle {r}_G{\underline{v}}_G^r\right\rangle_G $$(107)

5.4 Useful forms of the energy equation

Here we follow the development of [14] and choose the enthalpy balance equation (78) as the departure point. First of all, the dissipative term is assumed to be negligible: τ ̲ ̲ k : v ̲ k k 0 . $$ \left\langle {\underline{\underline{\tau }}}_k:\nabla {\underline{v}}_k\right\rangle_k\cong 0. $$(108)

This term is really important for very viscous fluids, such as liquid polymers. Here we deal with water and air, which are weakly viscous; therefore the assumption (108) is not too strong. Now we must examine the average of the pressure material derivative: D k p k Dt = p k t + v ̲ k · p k . $$ \frac{{D}_k{p}_k}{{Dt}}=\frac{\partial {p}_k}{{\partial t}}+{\underline{v}}_k\cdot \nabla {p}_k. $$(109)

For the time derivative, the relations (29) and (32) can be used: ε α k p k t k = X k p k t = t ( ε α k p k k ) - 1 V A kf p k v ̲ I · n ̲ k d a - 1 V A ks p k v ̲ I · n ̲ k d a . $$ \epsilon {\alpha }_k\left\langle \frac{\partial {p}_k}{{\partial t}}\right\rangle_k=\left\langle {X}_k\frac{\partial {p}_k}{{\partial t}}\right\rangle=\frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_k\left\langle {p}_k\right\rangle_k\right)-\frac{1}{V}{\int }_{{A}_{{kf}}}^{}{p}_k{\underline{v}}_I\cdot {\underline{n}}_k\mathrm{d}a-\frac{1}{V}{\int }_{{A}_{{ks}}}^{}{p}_k{\underline{v}}_I\cdot {\underline{n}}_k\mathrm{d}a. $$(110)

The term v ̲ k · p k $ {\underline{v}}_k\cdot \nabla {p}_k$ in (109) is more complicated since it is non-linear. Faust and Mercer [14] assume that the phase velocity and the pressure gradient are weakly correlated to obtain the following approximation: X k v ̲ k · p k   v ̲ k ̿ k · X k p k   = v ̲ k ̿ k · [ X k p k + p k n ̲ k δ I   ] = v ̲ k ̿ k · [ ( ε α k p k k ) + 1 V A kf p k n ̲ k d a + 1 V A ks p k n ̲ k d a   ] $$ \left\langle {X}_k{\underline{v}}_k\cdot \nabla {p}_k\enspace \right\rangle\cong {\stackrel{\text{=}{{\underline{v}}_k}}^k\cdot \left\langle {X}_k\nabla {p}_k\enspace \right\rangle={\stackrel{\text{=}{{\underline{v}}_k}}^k\cdot \left[\nabla \left\langle {X}_k{p}_k\right\rangle+\left\langle {p}_k{\underline{n}}_k{\delta }_I\right\rangle\enspace \right]={\stackrel{\text{=}{{\underline{v}}_k}}^k\cdot \left[\nabla \left(\epsilon {\alpha }_k\left\langle {p}_k\right\rangle_k\right)+\frac{1}{V}{\int }_{{A}_{{kf}}}^{}{p}_k{\underline{n}}_k\mathrm{d}a+\frac{1}{V}{\int }_{{A}_{{ks}}}^{}{p}_k{\underline{n}}_k\mathrm{d}a\enspace \right] $$(111)where (28) and (29) have been used. Decomposing the pressure into phase-average and fluctuating parts: p k = p k k + p' k $$ {p}_k=\left\langle {p}_k\right\rangle_k+{{p\prime}_k $$(112)then the equation (111) can be rewritten into the following equivalent form: X k v ̲ k · p k   v ̲ k ̿ k · [ ε α k p k k + 1 V A kf p' k n ̲ k d a + 1 V A ks p' k n ̲ k d a ] $$ \left\langle {X}_k{\underline{v}}_k\cdot \nabla {p}_k\enspace \right\rangle\cong {\stackrel{\text{=}{{\underline{v}}_k}}^k\cdot \left[\epsilon {\alpha }_k\nabla \left\langle {p}_k\right\rangle_k+\frac{1}{V}{\int }_{{A}_{{kf}}}^{}{{p\prime}_k{\underline{n}}_k\mathrm{d}a+\frac{1}{V}{\int }_{{A}_{{ks}}}^{}{{p\prime}_k{\underline{n}}_k\mathrm{d}a\right] $$(113)by using the relation (30). Substituting (108), (109), and (113) into (78) gives: t ( ε α k ρ k h k k ) + · ( ε α k ρ k h k v ̲ k k ) = 1 V A kf ( m ̇ k h k - q ̲ k · n ̲ k ) d a + 1 V A ks ( m ̇ k h k - q ̲ k · n ̲ k ) d a - · ( ε α k q ̲ k k ) + ε α k r k h k r k + t ( ε α k p k k ) - 1 V A kf p k v ̲ I · n ̲ k d a - 1 V A ks p k v ̲ I · n ̲ k d a + v ̲ k ̿ k · [ ε α k p k k + 1 V A kf p' k n ̲ k d a + 1 V A ks p' k n ̲ k d a ] . $$ \frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_k\left\langle {\rho }_k{h}_k\right\rangle_k\right)+\nabla \cdot \left(\epsilon {\alpha }_k\left\langle {\rho }_k{h}_k{\underline{v}}_k\right\rangle_k\right)=\frac{1}{V}{\int }_{{A}_{{kf}}}^{}\left({\dot{m}}_k{h}_k-{\underline{q}}_k\cdot {\underline{n}}_k\right)\mathrm{d}a+\frac{1}{V}{\int }_{{A}_{{ks}}}^{}\left({\dot{m}}_k{h}_k-{\underline{q}}_k\cdot {\underline{n}}_k\right)\mathrm{d}a-\nabla \cdot \left(\epsilon {\alpha }_k\left\langle {\underline{q}}_k\right\rangle_k\right)+\epsilon {\alpha }_k\left\langle {r}_k{h}_k^r\right\rangle_k+\frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_k\left\langle {p}_k\right\rangle_k\right)-\frac{1}{V}{\int }_{{A}_{{kf}}}^{}{p}_k{\underline{v}}_I\cdot {\underline{n}}_k\mathrm{d}a-\frac{1}{V}{\int }_{{A}_{{ks}}}^{}{p}_k{\underline{v}}_I\cdot {\underline{n}}_k\mathrm{d}a+{\stackrel{\text{=}{{\underline{v}}_k}}^k\cdot \left[\epsilon {\alpha }_k\nabla \left\langle {p}_k\right\rangle_k+\frac{1}{V}{\int }_{{A}_{{kf}}}^{}{{p\prime}_k{\underline{n}}_k\mathrm{d}a+\frac{1}{V}{\int }_{{A}_{{ks}}}^{}{{p\prime}_k{\underline{n}}_k\mathrm{d}a\right]. $$(114)

It is assumed that there is no phase change between a fluid phase and the solid phase, hence the phase change term m ̇ k h k $ {\dot{m}}_k{h}_k$ gives no contribution on the solid surface Aks. Let us introduce some new notations for the integral terms: Γ k h k Γ 1 V A kf m ̇ k h k d a + 1 V A ks m ̇ k h k d a = 1 V A kf m ̇ k h k d a . $$ {\mathrm{\Gamma }}_k{h}_k^{\mathrm{\Gamma }}\stackrel{\scriptscriptstyle\mathrm{def}}{=}\frac{1}{V}{\int }_{{A}_{{kf}}}^{}{\dot{m}}_k{h}_k\mathrm{d}a+\frac{1}{V}{\int }_{{A}_{{ks}}}^{}{\dot{m}}_k{h}_k\mathrm{d}a=\frac{1}{V}{\int }_{{A}_{{kf}}}^{}{\dot{m}}_k{h}_k\mathrm{d}{a}. $$(115) q kf = - 1 V A kf q ̲ k · n ̲ k d a   q ks = - 1 V A ks q ̲ k · n ̲ k d a $$ {q}_{{kf}}=-\frac{1}{V}{\int }_{{A}_{{kf}}}^{}{\underline{q}}_k\cdot {\underline{n}}_k\mathrm{d}a\enspace {q}_{{ks}}=-\frac{1}{V}{\int }_{{A}_{{ks}}}^{}{\underline{q}}_k\cdot {\underline{n}}_k\mathrm{d}a $$(116) q kf v ̲ k ̿ k · 1 V A kf p k n ̲ k d a   q   ks v ̲ k ̿ k · 1 V A ks p k n ̲ k d a . $$ {{q}^{\prime\prime }}_{{kf}}\stackrel{\scriptscriptstyle\mathrm{def}}{=}{\stackrel{\text{=}{{\underline{v}}_k}}^k\cdot \frac{1}{V}{\int }_{{A}_{{kf}}}^{}{{p}^\mathrm{\prime}}_k{\underline{n}}_k\mathrm{d}a\enspace {{q}^{\prime\prime }\enspace }_{{ks}}\stackrel{\scriptscriptstyle\mathrm{def}}{=}{\stackrel{\text{=}{{\underline{v}}_k}}^k\cdot \frac{1}{V}{\int }_{{A}_{{ks}}}^{}{{p}^\mathrm{\prime}}_k{\underline{n}}_k\mathrm{d}{a}. $$(117)

Strangely, the two terms - 1 V A kf p k v ̲ I · n ̲ k d a - 1 V A ks p k v ̲ I · n ̲ k d a $ -\frac{1}{V}{\int }_{{A}_{{kf}}}^{}{p}_k{\underline{v}}_I\cdot {\underline{n}}_k\mathrm{d}a-\frac{1}{V}{\int }_{{A}_{{ks}}}^{}{p}_k{\underline{v}}_I\cdot {\underline{n}}_k\mathrm{d}a$ are included in the term Γ k h k Γ $ {\mathrm{\Gamma }}_k{h}_k^{\mathrm{\Gamma }}$ by [14]. Making the same choice, equation (114) begins: t ( ε α k ρ k h k k ) + · ( ε α k ρ k h k v ̲ k k ) = Γ k h k Γ + q kf + q ks - · ( ε α k q ̲ k k ) + ε α k r k h k r k + t ( ε α k p k k ) + ε α k v ̲ k ̿ k · p k k + q kf + q ks . $$ \frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_k\left\langle {\rho }_k{h}_k\right\rangle_k\right)+\nabla \cdot \left(\epsilon {\alpha }_k\left\langle {\rho }_k{h}_k{\underline{v}}_k\right\rangle_k\right)={\mathrm{\Gamma }}_k{h}_k^{\mathrm{\Gamma }}+{q}_{{kf}}+{q}_{{ks}}-\nabla \cdot \left(\epsilon {\alpha }_k\left\langle {\underline{q}}_k\right\rangle_k\right)+\epsilon {\alpha }_k\left\langle {r}_k{h}_k^r\right\rangle_k+\frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_k\left\langle {p}_k\right\rangle_k\right)+\epsilon {\alpha }_k{\stackrel{\text{=}{{\underline{v}}_k}}^k\cdot \nabla \left\langle {p}_k\right\rangle_k+{{q}^{\prime\prime }}_{{kf}}+{{q}^{\prime\prime }}_{{ks}}. $$(118)

The term Γ k h k Γ $ {\mathrm{\Gamma }}_k{h}_k^{\mathrm{\Gamma }}$ represents the interfacial transfer of enthalpy associated to the transfer of mass by evaporation or condensation. The terms qkf and qks represent the interfacial conduction terms between the two fluid phases on one hand and between phase k and the solid phase on the other hand. The term r k h k r k $ \left\langle {r}_k{h}_k^r\right\rangle_k$ represents the reaction enthalpy due to chemical reactions. The last two terms qkf and qks are the mechanical powers of the interfacial fluctuating pressure forces in the mean velocity. Introducing a Favre average value for the enthalpy, we can write: ρ k h k k = ρ k k h k ̅ ̅ k $$ \left\langle {\rho }_k{h}_k\right\rangle_k=\left\langle {\rho }_k\right\rangle_k{\overline{\overline{{h}_k}}}^k $$(119) ρ k h k v ̲ k k = ρ k k h k v ̲ k ̅ ̅ k = ρ k k ( h k ̅ ̅ k v ̲ k ̅ ̅ k + h' k v' ̲ k ̅ ̅ k ) $$ \left\langle {\rho }_k{h}_k{\underline{v}}_k\right\rangle_k=\left\langle {\rho }_k\right\rangle_k{\overline{\overline{{h}_k{\underline{v}}_k}}}^k=\left\langle {\rho }_k\right\rangle_k\left({\overline{\overline{{h}_k}}}^k{\overline{\overline{{\underline{v}}_k}}}^k+{\overline{\overline{{{h\prime}_k{\underline{{v\prime}}_k}}}^k\right) $$(120)where h' k v ' ̲ k ̅ ̅ k $ {\overline{\overline{{{h\prime}_k{\underline{v\prime}_k}}}^k$ is a correlation between the fluctuating enthalpy and velocity, we call it the dispersion vector and denote it as follows: q ̲ k d ρ k k h k v ̲ k ̅ ̅ k . $$ {\underline{q}}_k^d\stackrel{\scriptscriptstyle\mathrm{def}}{=}\left\langle {\rho }_k\right\rangle_k{\overline{\overline{{{h}^\mathrm{\prime}}_k{\underline{{v}^\mathrm{\prime}}}_k}}}^k. $$(121)

Substituting (119) and (121) into (118) gives: t ( ε α k ρ k k h k ̅ ̅ k ) + · ( ε α k ρ k k h k ̅ ̅ k v ̲ k ̅ ̅ k ) = Γ k h k Γ + q kf + q ks - · ( ε α k ( q ̲ k k + q ̲ k d ) ) + ε α k r k h k r k + t ( ε α k p k k ) + ε α k v ̲ k ̿ k · p k k + q kf + q ks . $$ \frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_k\left\langle {\rho }_k\right\rangle_k{\overline{\overline{{h}_k}}}^k\right)+\nabla \cdot \left(\epsilon {\alpha }_k\left\langle {\rho }_k\right\rangle_k{\overline{\overline{{h}_k}}}^k{\overline{\overline{{\underline{v}}_k}}}^k\right)={\mathrm{\Gamma }}_k{h}_k^{\mathrm{\Gamma }}+{q}_{{kf}}+{q}_{{ks}}-\nabla \cdot \left(\epsilon {\alpha }_k\left(\left\langle {\underline{q}}_k\right\rangle_k+{\underline{q}}_k^d\right)\right)+\epsilon {\alpha }_k\left\langle {r}_k{h}_k^r\right\rangle_k+\frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_k\left\langle {p}_k\right\rangle_k\right)+\epsilon {\alpha }_k{\stackrel{\text{=}{{\underline{v}}_k}}^k\cdot \nabla \left\langle {p}_k\right\rangle_k+{{q}^{\prime\prime }}_{{kf}}+{{q}^{\prime\prime }}_{{ks}}. $$(122)

The modeling of the average molecular heat flux q ̲ k k $ \left\langle {\underline{q}}_k\right\rangle_k$ uses the Fourier’s law: q ̲ k = - k k T k . $$ {\underline{q}}_k=-{k}_k\nabla {T}_k. $$(123)

Assuming that the conductivity kk does not vary significantly at the scale of the REV: ε α k q ̲ k k = - k k X k T k k = - k k ( ( ε α k T k k ) + 1 V A kf T k n ̲ k d a + 1 V A ks T k n ̲ k d a ) . $$ \epsilon {\alpha }_k\left\langle {\underline{q}}_k\right\rangle_k=-{k}_k\left\langle {X}_k\nabla {T}_k\right\rangle_k=-{k}_k\left(\nabla \left(\epsilon {\alpha }_k\left\langle {T}_k\right\rangle_k\right)+\frac{1}{V}{\int }_{{A}_{{kf}}}^{}{T}_k{\underline{n}}_k\mathrm{d}a+\frac{1}{V}{\int }_{{A}_{{ks}}}^{}{T}_k{\underline{n}}_k\mathrm{d}a\right). $$(124)

As done previously for the pressure, we decompose the temperature Tk into its phase average plus a fluctuation: T k T k k + T ' k . $$ {T}_k\stackrel{\scriptscriptstyle\mathrm{def}}{=}\left\langle {T}_k\right\rangle_k+{{T}^{\prime}_k. $$(125)

Introducing (125) into (124) and using (30), we obtain: ε α k q ̲ k k = - k k ( ε α k T k k + 1 V A kf T ' k n ̲ k d a + 1 V A ks T ' k n ̲ k d a ) $$ \epsilon {\alpha }_k\left\langle {\underline{q}}_k\right\rangle_k=-{k}_k\left(\epsilon {\alpha }_k\nabla \left\langle {T}_k\right\rangle_k+\frac{1}{V}{\int }_{{A}_{{kf}}}^{}{{T}^{\prime}_k{\underline{n}}_k\mathrm{d}a+\frac{1}{V}{\int }_{{A}_{{ks}}}^{}{{T}^{\prime}_k{\underline{n}}_k\mathrm{d}a\right) $$(126)where the two surface integrals represent the decreased conduction rate due to the tortuosity of the medium, we define the tortuosity vector for the heat flux as: ϑ ̲ k 1 V A kf T ' k n ̲ k d a + 1 V A ks T ' k n ̲ k d a . $$ {\underline{\vartheta }}_k\stackrel{\scriptscriptstyle\mathrm{def}}{=}\frac{1}{V}{\int }_{{A}_{{kf}}}^{}{{T}^{\prime}_k{\underline{n}}_k\mathrm{d}a+\frac{1}{V}{\int }_{{A}_{{ks}}}^{}{{T}^{\prime}_k{\underline{n}}_k\mathrm{d}a. $$(127)

Hence, equation (126) becomes: ε α k q ̲ k k = - k k ( ε α k T k k + ϑ ̲ k ) . $$ \epsilon {\alpha }_k\left\langle {\underline{q}}_k\right\rangle_k=-{k}_k\left(\epsilon {\alpha }_k\nabla \left\langle {T}_k\right\rangle_k+{\underline{\vartheta }}_k\right). $$(128)

Assuming that the dispersion vector can be modelled similarly by a diffusion effect, we introduce the dispersion tensor such that: ε α k q ̲ k d = - k ̲ ̲ k d · ( ε α k T k k + ϑ ̲ k ) . $$ \epsilon {\alpha }_k{\underline{q}}_k^d=-{\underline{\underline{k}}}_k^d\cdot \left(\epsilon {\alpha }_k\nabla \left\langle {T}_k\right\rangle_k+{\underline{\vartheta }}_k\right). $$(129)

Substituting (128) and (129) into equation (122), this equation becomes: t ( ε α k ρ k k h k ̅ ̅ k ) + · ( ε α k ρ k k h k ̅ ̅ k v ̲ k ̅ ̅ k ) = Γ k h k Γ + q kf + q ks + · ( ( k k I ̲ ̲ + k ̲ ̲ k d ) · ( ε α k T k k + ϑ ̲ k ) ) + ε α k r k h k r k + t ( ε α k p k k ) + ε α k v ̲ k ̿ k · p k k + q kf + q ks . $$ \frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_k\left\langle {\rho }_k\right\rangle_k{\overline{\overline{{h}_k}}}^k\right)+\nabla \cdot \left(\epsilon {\alpha }_k\left\langle {\rho }_k\right\rangle_k{\overline{\overline{{h}_k}}}^k{\overline{\overline{{\underline{v}}_k}}}^k\right)={\mathrm{\Gamma }}_k{h}_k^{\mathrm{\Gamma }}+{q}_{{kf}}+{q}_{{ks}}+\nabla \cdot \left(\left({k}_k\underline{\underline{I}}+{\underline{\underline{k}}}_k^d\right)\cdot \left(\epsilon {\alpha }_k\nabla \left\langle {T}_k\right\rangle_k+{\underline{\vartheta }}_k\right)\right)+\epsilon {\alpha }_k\left\langle {r}_k{h}_k^r\right\rangle_k+\frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_k\left\langle {p}_k\right\rangle_k\right)+\epsilon {\alpha }_k{\stackrel{\text{=}{{\underline{v}}_k}}^k\cdot \nabla \left\langle {p}_k\right\rangle_k+{{q}^{\mathrm{\prime\prime }}}_{{kf}}+{{q}^{\mathrm{\prime\prime }}}_{{ks}}. $$(130)

For the solid phase, the equation is simpler since there is no velocity (hence no dispersion), no phase change, no chemical reaction… in it, hence we can write the enthalpy equation for the solid phase as: t ( ( 1 - ε ) ρ s s h s ̅ ̅ s ) = q sl + q sg + · ( k s ( ( 1 - ε ) T s s + ϑ ̲ s ) ) . $$ \frac{\partial }{{\partial t}}\left(\left(1-\epsilon \right)\left\langle {\rho }_s\right\rangle_s{\overline{\overline{{h}_s}}}^s\right)={q}_{{sl}}+{q}_{{sg}}+\nabla \cdot \left({k}_s\left(\left(1-\epsilon \right)\nabla \left\langle {T}_s\right\rangle_s+{\underline{\vartheta }}_s\right)\right). $$(131)where qsl and qsg denote the heat exchanges between the solid and the liquid on one hand and between the solid and the gas on the other hand.

6 Simplifications currently adopted in the case of PEMFC

6.1 Simplification of the momentum balance equations

Faust and Mercer [14] made the following simplification of the momentum balance equation for phase k. Starting from our equation (72) and neglecting the inertial terms (including the phase change term and the chemical one, which is justifiable in porous media since viscous and pressure effects are predominant), the remaining equation is: 0 1 V A Ik σ ̲ ̲ k · n ̲ k d a - ε α k p k k + · ( ε α k τ ̲ ̲ k k ) + ε α k ρ k k g ̲ . $$ 0\cong \frac{1}{V}{\int }_{{A}_{{Ik}}}^{}{\underline{\underline{\sigma }}}_k\cdot {\underline{n}}_k\mathrm{d}a-\epsilon {\alpha }_k{\nabla \left\langle {p}_k\right\rangle_k+\nabla \cdot \left(\epsilon {\alpha }_k\left\langle {\underline{\underline{\tau }}}_k\right\rangle_k\right)+\epsilon {\alpha }_k\left\langle {\rho }_k\right\rangle_k\underline{g}. $$(132)

Then [14] introduces the following modeling of the interfacial term plus the phase viscous diffusion: 1 V A Ik σ ̲ ̲ k · n ̲ k d a + · ( ε α k τ ̲ ̲ k k ) = K ̲ ̲ - 1 · ε α k μ k K rk ( v ̲ S - v ̲ k ) . $$ \frac{1}{V}{\int }_{{A}_{{Ik}}}^{}{\underline{\underline{\sigma }}}_k\cdot {\underline{n}}_k\mathrm{d}a+\nabla \cdot \left(\epsilon {\alpha }_k\left\langle {\underline{\underline{\tau }}}_k\right\rangle_k\right)={\underline{\underline{K}}}^{-1}\cdot \frac{\epsilon {\alpha }_k{\mu }_k}{{K}_{{rk}}}\left(\left\langle {\underline{v}}_S\right\rangle-\left\langle {\underline{v}}_k\right\rangle\right). $$(133)where K ̲ ̲ $ \underline{\underline{K}}$ is the local intrinsic permeability tensor, Krk is the dimensionless relative permeability for phase k and μk is phase k’s viscosity. Substituting (133) into (132), we obtain: p k k - ρ k k g ̲ = K ̲ ̲ - 1 · μ k K rk ( v ̲ S - v ̲ k ) . $$ {\nabla \left\langle {p}_k\right\rangle_k-\left\langle {\rho }_k\right\rangle_k\underline{g}={\underline{\underline{K}}}^{-1}\cdot \frac{{\mu }_k}{{K}_{{rk}}}\left(\left\langle {\underline{v}}_S\right\rangle-\left\langle {\underline{v}}_k\right\rangle\right). $$(134)

Here we assume that the solid phase is immobile ( v ̲ S = 0 $ \left\langle {\underline{v}}_S\right\rangle=0$) and v ̲ k $ \left\langle {\underline{v}}_k\right\rangle$ is the filtration velocity, which is defined by [14] as: v ̲ k = ε α k v ̲ k k . $$ \left\langle {\underline{v}}_k\right\rangle=\epsilon {\alpha }_k\left\langle {\underline{v}}_k\right\rangle_k. $$(135)

Hence, we obtain: v ̲ k k = K ̲ ̲ K rk ε α k μ k ( p k k - ρ k k g ̲ ) . $$ \left\langle {\underline{v}}_k\right\rangle_k=\frac{\underline{\underline{K}}{K}_{{rk}}}{\epsilon {\alpha }_k{\mu }_k}\left({\nabla \left\langle {p}_k\right\rangle_k-\left\langle {\rho }_k\right\rangle_k\underline{g}\right). $$(136)

We have retrieved the result (5) given by [4]. The closure relation (136) is used as an approximation for v ̲ k ̅ ̅ k $ {\overline{\overline{{\underline{v}}_k}}}^k$ by [22] in the case of PEMFC.

For the flows in the channels of the bipolar plates, [23] adopted the simplest forms of our equations (106) and (107). Assuming that the flows in the channels remain laminar, they retain the following two-fluid model equations: t ( α L ρ L L v ̲ L ̿ L ) + · ( α L ρ L L v ̲ L ̿ L v ̲ L ̿ L ) = - α L P + F ̲ s - R ̲ LG + · ( α L τ ̲ ̲ L L ) + α L ρ L L g ̲ $$ \frac{\partial }{{\partial t}}\left({\alpha }_L\left\langle {\rho }_L\right\rangle_L{\stackrel{\text{=}{{\underline{v}}_L}}^L\right)+\nabla \cdot \left({\alpha }_L\left\langle {\rho }_L\right\rangle_L{\stackrel{\text{=}{{\underline{v}}_L}}^L{\stackrel{\text{=}{{\underline{v}}_L}}^L\right)=-{\alpha }_L\nabla P+{\underline{F}}_s-{\underline{R}}_{{LG}}+\nabla \cdot \left({\alpha }_L\left\langle {\underline{\underline{\tau }}}_L\right\rangle_L\right)+{\alpha }_L\left\langle {\rho }_L\right\rangle_L\underline{g} $$(137) t ( α G ρ G G v ̲ G ̿ G ) + · ( α G ρ G G v ̲ G ̿ G v ̲ G ̿ G ) = - α G P + F ̲ s + R ̲ LG + · ( α G τ ̲ ̲ G G ) + α G ρ G G g ̲ $$ \frac{\partial }{{\partial t}}\left({\alpha }_G\left\langle {\rho }_G\right\rangle_G{\stackrel{\text{=}{{\underline{v}}_G}}^G\right)+\nabla \cdot \left({\alpha }_G\left\langle {\rho }_G\right\rangle_G{\stackrel{\text{=}{{\underline{v}}_G}}^G{\stackrel{\text{=}{{\underline{v}}_G}}^G\right)=-{\alpha }_G\nabla P+{\underline{F}}_s+{\underline{R}}_{{LG}}+\nabla \cdot \left({\alpha }_G\left\langle {\underline{\underline{\tau }}}_G\right\rangle_G\right)+{\alpha }_G\left\langle {\rho }_G\right\rangle_G\underline{g} $$(138)where the indices L and G denote the liquid and gas phases, R ̲ LG $ {\underline{R}}_{{LG}}$ is the volumetric friction between phases and F ̲ s $ {\underline{F}}_s$ is a surface tension source term.

6.2 Simplification of the species mass balance equation

Tardy [22] starts from the equation (93) and neglects the correlation between the mass fraction and the velocity fluctuations: Y ik v ̲ k ̿ k Y ik ̿ k v ̲ k ̿ k . $$ {\stackrel{\text{=}{{Y}_{{ik}}{\underline{v}}_k}}^k\cong {\stackrel{\text{=}{{Y}_{{ik}}}}^k{\stackrel{\text{=}{{\underline{v}}_k}}^k. $$(139)

Substituting this relation into (93) gives: t ( ε α k ρ k k Y ik ̿ k ) + · ( ε α k ρ k k Y ik ̿ k v ̲ k ̿ k ) = · ( D ik ( ε α k ρ k k Y ik ̿ k ) ) + Γ k Y ik Γ + Σ ik + S ik . $$ \frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_k\left\langle {\rho }_k\right\rangle_k{\stackrel{\text{=}{{Y}_{{ik}}}}^k\right)+\nabla \cdot \left(\epsilon {\alpha }_k\left\langle {\rho }_k\right\rangle_k{\stackrel{\text{=}{{Y}_{{ik}}}}^k{\stackrel{\text{=}{{\underline{v}}_k}}^k\right)=\nabla \cdot \left({D}_{{ik}}\nabla \left(\epsilon {\alpha }_k\left\langle {\rho }_k\right\rangle_k{\stackrel{\text{=}{{Y}_{{ik}}}}^k\right)\right)+{\mathrm{\Gamma }}_k{Y}_{{ik}}^{\mathrm{\Gamma }}+{\mathrm{\Sigma }}_{{ik}}+{S}_{{ik}}. $$(140)

This equation can be compared to the following one derived by [24] rewritten with our notations: t ( ε α k C ik k ) + · ( ε α k ( C ik k v ̲ k k + C' ik v' ̲ k k ) ) = Γ k ρ k k C ik k + · ( D ik [ ( ε α k C ik k ) + ε α k τ ̲ ik ] ) + ε α k K a Ik ( C ik k - C ik k 0 ) + ε α k r ik k . $$ \frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_k\left\langle {C}_{{ik}}\right\rangle_k\right)+\nabla \cdot \left(\epsilon {\alpha }_k\left(\left\langle {C}_{{ik}}\right\rangle_k\left\langle {\underline{v}}_k\right\rangle_k+\left\langle {{C\prime}_{{ik}}{\underline{{v\prime}}_k\right\rangle_k\right)\right)=\frac{{\mathrm{\Gamma }}_k}{\left\langle {\rho }_k\right\rangle_k}\left\langle {C}_{{ik}}\right\rangle_k+\nabla \cdot \left({D}_{{ik}}\left[\nabla \left(\epsilon {\alpha }_k\left\langle {C}_{{ik}}\right\rangle_k\right)+\epsilon {\alpha }_k{\underline{\tau }}_{{ik}}\right]\right)+\epsilon {\alpha }_kK{a}_{{Ik}}\left(\left\langle {C}_{{ik}}\right\rangle_k-\left\langle {C}_{{ik}}\right\rangle_{k0}\right)+\epsilon {\alpha }_k\left\langle {r}_{{ik}}\right\rangle_k. $$(141)

This comparison shows that C ik k = ρ k k Y ik ̿ k $ \left\langle {C}_{{ik}}\right\rangle_k=\left\langle {\rho }_k\right\rangle_k{\stackrel{\text{=}{{Y}_{{ik}}}}^k$ (mass of species i per unit volume of phase k), Sik = εαkrikk and Σik = εαkKaIk(〈Cikk − 〈Cikk0) where aIk is the volumetric interfacial area between phase k and the other phases and K is a mass transfer coefficient. 〈Cikk0 denotes the concentration value at the interface with the other phase. Tardy [22] neglects this term as well as the dispersion term C ' ik v ' ̲ k k $ \left\langle {C\prime}_{{ik}}{\underline{v\prime}_k\right\rangle_k$ and the tortuosity vector for the species τ ̲ ik $ {\underline{\tau }}_{{ik}}$.

6.3 Simplification of the enthalpy balance equation

Zhang and Jiao [25] start from the multiphase model derived from [4] and transform it to a multiphase multicomponent mixture model by summing the equations on the different phases. Their model is used later in the channels of PEMFC by [26]. Here, we present the simplifications made by these authors, starting from our enthalpy balance equations (130) and (131). The enthalpy balance equation for phase k retained by [25] has the following form: t ( ε α k ρ k k h k ̅ ̅ k ) + . ( ρ k k h k ̅ ̅ k v ̲ k ) = . ( α k k k eff T ) + Q k $$ \frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_k\left\langle {\rho }_k\right\rangle_k{\overline{\overline{{h}_k}}}^k\right)+\nabla.\left(\left\langle {\rho }_k\right\rangle_k{\overline{\overline{{h}_k}}}^k\left\langle {\underline{v}}_k\right\rangle\right)=\nabla.\left({\alpha }_k{k}_k^{{eff}}\nabla T\right)+{Q}_k $$(142)where v ̲ k $ \left\langle {\underline{v}}_k\right\rangle$ denotes the filtration velocity defined by (135). The comparison of (142) with our equation (130) shows the simplifying assumptions made by these authors. First of all, they adopt the thermal equilibrium assumption given by (11), hence, the phase-averaged temperatures are all equal to the mean temperature T for the medium. Secondly, all the diffusion and dispersion effects are modelled collectively by introducing an effective conductivity k k eff : $ {k}_k^{{eff}}:$ · ( α k k k eff T ) = · ( ( k k I ̲ ̲ + k ̲ ̲ k d ) · ( ε α k T k k + ϑ ̲ k ) )   by   definition   of   k k eff . $$ \nabla \cdot \left({\alpha }_k{k}_k^{{eff}}\nabla T\right)=\nabla \cdot \left(\left({k}_k\underline{\underline{I}}+{\underline{\underline{k}}}_k^d\right)\cdot \left(\epsilon {\alpha }_k\nabla \left\langle {T}_k\right\rangle_k+{\underline{\vartheta }}_k\right)\right)\enspace \mathrm{by}\enspace \mathrm{definition}\enspace \mathrm{of}\enspace {k}_k^{{eff}}. $$(143)

Thirdly, the term Qk in (142) models, collectively all the remaining terms in our equation (130): Q k = Γ k h k Γ + q kf + q ks + ε α k r k h k r k + t ( ε α k p k k ) + ε α k v ̲ k ̿ k · p k k + q kf + q ks . $$ {Q}_k={\mathrm{\Gamma }}_k{h}_k^{\mathrm{\Gamma }}+{q}_{{kf}}+{q}_{{ks}}+\epsilon {\alpha }_k\left\langle {r}_k{h}_k^r\right\rangle_k+\frac{\partial }{{\partial t}}\left(\epsilon {\alpha }_k\left\langle {p}_k\right\rangle_k\right)+\epsilon {\alpha }_k{\stackrel{\text{=}{{\underline{v}}_k}}^k\cdot \nabla \left\langle {p}_k\right\rangle_k+{{q}^{\mathrm{\prime\prime }}}_{{kf}}+{{q}^{\mathrm{\prime\prime }}}_{{ks}}. $$(144)

Summing the equations (142) on the different phases, including the solid phase s, the following equation is obtained: t ( ( 1 - ε ) ρ s h s + ε k s α k ρ k h k ) + · ( k s ρ k h k v ̲ k ) = . ( k eff T ) + Q $$ \frac{\partial }{{\partial t}}\left(\left(1-\epsilon \right){\rho }_s{h}_s+\epsilon \sum_{k\ne s}^{}{\alpha }_k{\rho }_k{h}_k\right)+\nabla \cdot \left(\sum_{k\ne s}^{}{\rho }_k{h}_k\left\langle {\underline{v}}_k\right\rangle\right)=\nabla.\left({k}_{{eff}}\nabla T\right)+Q $$(145)with: k eff k + s α k k k eff and   Q k + s Q k $$ {k}_{{eff}}\stackrel{\scriptscriptstyle\mathrm{def}}{=}\sum_{k+s}^{}{\alpha }_k{k}_k^{{eff}}\mathrm{and}\enspace Q\stackrel{\scriptscriptstyle\mathrm{def}}{=}\sum_{k+s}^{}{Q}_k $$(146)

Posing: ρ h k s α k ρ k h k   k ρ k h k v ̲ k = λ k h k ρ v ̲ + h k j ̲ k γ h ρ h v ̲ + k h k j ̲ k $$ {\rho h}\stackrel{\scriptscriptstyle\mathrm{def}}{=}\sum_{k\ne s}^{}{\alpha }_k{\rho }_k{h}_k\enspace \sum_k^{}{\rho }_k{h}_k\left\langle {\underline{v}}_k\right\rangle=\sum_{}^{}{\lambda }_k{h}_k\rho \underline{v}+{h}_k{\underline{j}}_k\stackrel{\scriptscriptstyle\mathrm{def}}{=}{\gamma }_h{\rho h}\underline{v}+\sum_k^{}{h}_k{\underline{j}}_k $$(147)where λk is the phase k mobility, j ̲ k $ {\underline{j}}_k$ is a diffusive flux due to the difference between the phases’ velocities and γh is a correction factor for enthalpy convection defined by: λ k K rk ν k ν   ρ k v ̲ k = λ k ρ v ̲ + j ̲ k   γ h ρ k s λ k h k ρ h $$ {\lambda }_k\stackrel{\scriptscriptstyle\mathrm{def}}{=}\frac{{K}_{{rk}}}{{\nu }_k}\nu \enspace {\rho }_k\left\langle {\underline{v}}_k\right\rangle={\lambda }_k\rho \underline{v}+{\underline{j}}_k\enspace {\gamma }_h\stackrel{\scriptscriptstyle\mathrm{def}}{=}\frac{\rho \sum_{k\ne s}^{}{\lambda }_k{h}_k}{{\rho h}} $$(148)where νk and ν denote the kinematic viscosities of the phase k and the mixture respectively. ρ, v ̲ $ \underline{v}$ and h denote the density, center of mass velocity, and enthalpy of the gas-liquid mixture: ρ k α k ρ k   ρ v ̲ k ρ k v ̲ k . $$ \rho \stackrel{\scriptscriptstyle\mathrm{def}}{=}\sum_k^{}{\alpha }_k{\rho }_k\enspace {\rho }\underline{v}\stackrel{\scriptscriptstyle\mathrm{def}}{=}\sum_k^{}{\rho }_k\left\langle {\underline{v}}_k\rangle. $$(149)

Introducing (147) and (149) into (145), the equation for the mixture enthalpy reads: t ( ( 1 - ε ) ρ s h s + ε ρ h ) + · ( γ h ρ h v ̲ ) = · ( k eff T - k h k j ̲ k ) + Q $$ \frac{\partial }{{\partial t}}\left(\left(1-\epsilon \right){\rho }_s{h}_s+{\epsilon \rho h}\right)+\nabla \cdot \left({\gamma }_h{\rho h}\underline{v}\right)=\nabla \cdot \left({k}_{{eff}}\nabla T-\sum_k^{}{h}_k{\underline{j}}_k\right)+Q $$(150)

Zhang et al. [27] as well as Tardy [22] retain only a two-phase version of the mixture temperature: t ( k = L , G ε α k ρ k k C p , k T ) +   · ( k = L , G ε α k ρ k k C p , k T v ̲ k ̿ k ) = Q + · ( ε k eff T ) . $$ \frac{\partial }{{\partial t}}\left(\sum_{k=L,G}^{}\epsilon {\alpha }_k\left\langle {\rho }_k\right\rangle_k{C}_{p,k}T\right)+\nabla \enspace \cdot \left(\sum_{k=L,G}^{}\epsilon {\alpha }_k\left\langle {\rho }_k\right\rangle_k{C}_{p,k}T{\stackrel{\text{=}{{\underline{v}}_k}}^k\right)=Q+\nabla \cdot \left(\epsilon {k}_{{eff}}\nabla T\right). $$(151)

7 Conclusions

This paper gives a complete derivation of the average equations governing the two-phase multicomponent flows in porous media. The targeted application is the proton exchange membrane fuel cells. As we consider the fuel cells working at temperatures below 100 °C (typically 80 °C), water exists in gas and liquid phases in the interior of the PEMFC (porous layers and bipolar plates). All the equations have been derived for liquid and gas masses, species masses, momenta of the two phases, as well as the different forms of energy and entropy. The simplified versions of these equations currently used in PEMFC models are given in the last section.

References

  • Gray W.G., Lee P.C.Y. (1977) On the theorems for local volume averaging of multiphase systems, Int. J. Multiphase Flow 3, 333–340. [Google Scholar]
  • Slattery J.C. (1967) Flow of viscoelastic fluids in porous media, Aiche J. 13, 6, 1066–1071. [Google Scholar]
  • Whitaker S. (1967) Diffusion and dispersion in porous media, Aiche J. 13, 3, 420–427. [Google Scholar]
  • Abriola L.M., Pinder G.F. (1985) A multiphase approach to the modelling of porous media. Contamination by organic compounds, part I: Equations development, Water Resour. Res. 21, 1, 11–18. [Google Scholar]
  • Nield D.A., Bejan A. (2017) Convection in porous media, 5th edn., Springer, USA. [Google Scholar]
  • Delhaye J.M. (2008) Thermohydraulique des réacteurs, EDP Science, France. [Google Scholar]
  • Ishii M. (1975) Thermo-fluid dynamic theory of two-phase flow, Eyrolles, Paris. [Google Scholar]
  • Ishii M., Hibiki T. (2011) Thermo-fluid dynamics of two-phase flows, 2nd edn., Springer, USA. [Google Scholar]
  • Morel C. (2015) Mathematical modelling of disperse two-phase flows. Fluid mechanics and its applications, Springer, USA. [Google Scholar]
  • Sha W.T., Chao B.T., Soo S.L. (1984) Porous media formulation for multiphase flows with heat transfer, Nuclear Eng. Des. 82, 93–106. [Google Scholar]
  • Nigmatulin R.I. (1990) Dynamics of multiphase media, vol. 1, HPC. [Google Scholar]
  • Whitaker S. (1969) Fluid motion in porous media, Ind. Eng. Chem. 61, 12, 14–28. [Google Scholar]
  • Kataoka I. (1986) Local instant formulation of two-phase flow, Int. J. Multiphase Flow 12, 5, 745–758. [Google Scholar]
  • Faust C.R., Mercer J.W. (1977) Theoretical analysis of fluid flow and energy transport in hydrothermal systems, U.S. Geological Survey, Report 77-60. [Google Scholar]
  • Jakobsen H.A. (2008) Chemical reactor modelling, multiphase reacting flows, Springer, Berlin. [Google Scholar]
  • Delhaye J.M. (1974) Conditions d’interface et source d’entropie dans les systèmes diphasiques, CEA-R-4562. [Google Scholar]
  • Delhaye J.M. (1974) Jump conditions and entropy sources in two-phase systems: local instant formulation, Int. J. Multiphase Flow 1, 395–409. [Google Scholar]
  • Kaviany M. (1995) Principles of heat transfer in porous media, 2nd edn, Springer, USA. [Google Scholar]
  • Kolev N.I. (2005) Multiphase flow dynamics 1: fundamentals, 2nd edn., Springer, USA. [Google Scholar]
  • Lhuillier D. (2003) A mean field description of two-phase flow with phase changes, Int. J. Multiphase Flow 29, 511–525. [Google Scholar]
  • Lhuillier D., Theofanous T.G., Liou MS. (2010) Multiphase flows: compressible multi-hydrodynamics, in: Cacuci D.G.(ed.), Handbook of nuclear engineering, Springer, Berlin, pp. 1813–1912. [Google Scholar]
  • Tardy E. (2022) Etude de la distribution d’eau liquide dans les piles à combustible PEM de grande surface à l’aide d’un modèle multiphysique d’écoulement diphasique, Thèse de Doctorat, Université Grenoble Alpes, Saint-Martin-d’Hères, France. [Google Scholar]
  • Zhang G., Jiao K. (2018) Three-dimensional multiphase simulations of PEMFC at high current density using Eulerian-Eulerian model and two-fluid model, Energy Convers. Manag. 176, 409–421. [Google Scholar]
  • Whitaker S. (1973) The transport equations for multiphase systems, Chem. Eng. Sci. 28, 139–147. [Google Scholar]
  • Wang C.Y., Cheng P. (1996) A multiphase mixture model for multiphase, multicomponent transport in capillary porous media: I model development, Int. J. Heat Mass Transfer 39, 17, 3607–3618. [Google Scholar]
  • Wang Y., Basu S., Wang C.Y. (2008) Modelling two-phase flow in PEM fuel cell channels, J. Power Sources 179, 603–617. [Google Scholar]
  • Zhang G., Xie X., Xie B., Du Q., Jiao K. (2019) Large scale multiphase simulation of proton exchange membrane fuel cell, Int. J. Heat Mass Transfer 130, 555–563. [Google Scholar]

All Tables

Table 1

Notations for the generalised balance equations (35) and (36).

All Figures

thumbnail Figure 1

Scheme of a typical REV containing the three phases.

In the text

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