Numerical methods and HPC
Open Access
Issue
Oil Gas Sci. Technol. – Rev. IFP Energies nouvelles
Volume 74, 2019
Numerical methods and HPC
Article Number 24
Number of page(s) 20
DOI https://doi.org/10.2516/ogst/2018071
Published online 11 March 2019

© V. Girault et al., published by IFP Energies nouvelles, 2019

Licence Creative CommonsThis is an Open Access article distributed under the terms of the Creative Commons Attribution License (http://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

Starting from the pioneering work of von Terzaghi [1] and Biot [2, 3], a growing demand for assessing fluid structure interactions has driven the development of numerical models coupling flow and geomechanics. Here important applications include subsidence events, carbon sequestration, ground water remediation, hydrocarbon production and hydraulic fracturing, enhanced geothermal systems, solid waste disposal, and biomedical heart modeling. In this paper we consider the Biot model that consists of a geomechanics equation coupled to a flow model with the displacement, pressure, and flow velocity as unknowns. In contrast to solving the Biot system fully implicitly, we focus on iterative schemes that allow the decoupling of the flow and mechanics equations and offer several attractive features (such as use of existing flow and mechanics codes, use of appropriate pre-conditioners and solvers for the two models, and ease of implementation). The design of iterative schemes however is an important consideration for an efficient, convergent, and robust algorithm.

Four main iterative coupling schemes for coupling flow with mechanics were introduced by Settari and Mourits [4, 5] and implemented and studied by Gai et al. [6, 7], Gai [8], Dean et al. [9], Girault et al. [10], Almani et al. [1114]. They are known as the fixed-stress split, fixed-strain split, undrained-split, and drained split schemes (Mikelić and Wheeler [15], Mikelić et al. [16] and Kim et al. [17, 18]). In the fixed-stress and fixed-strain split schemes, the flow problem is solved first, followed by the mechanics problem, and a constant mean total stress or constant strain is assumed during the flow solve respectively. In contrast, in the drained and undrained split coupling schemes, the mechanics problem is solved first, followed by the flow problem, and a constant fluid pressure and a constant fluid mass (i.e., fluid content of the medium) is assumed during the mechanics solve respectively. Both the fixed-stress split and undrained split schemes are shown to be contractive (Mikelić and Wheeler [15], Mikelić et al. [16]]), whereas the fixed-strain split and drained split schemes are only conditionally stable (Kim et al. [17, 18]). In addition, we note here that these iterative coupling schemes can be interpreted as pre-conditioner techniques for solving the fully coupled system. For instance, the work of Gai et al. [7, 19] involves interpreting the fixed-stress split scheme as a physics-based preconditioning strategy applied to a Richardson fixed point iteration. The same preconditioning technique was applied to the fully coupled system in the work of Castelletto et al. [20, 21].

Extensions of the fixed-stress split and undrained split iterative schemes to the multirate case, in which flow takes multiple fine time steps within one coarse mechanics time step, can be found in the work of Almani et al. [11] and Kumar et al. [22]. In addition, extensions to a nonlinear case can be found in the work of White et al. [23], Borregales et al. [24], and da Silva et al. [25], and a multiscale extension of the fixed-stress split scheme is illustrated in the work of Dana et al. [26]. Moreover, the work of Bause et al. [27] and Borregales et al. [28] explored space-time methods of the corresponding iterative coupling schemes, and work of Rodrigo et al. [29] considered the stability analysis of the discretization schemes.

Here we restrict our attention to fixed-stress iterative coupling, analyze both Galerkin and mixed finite element for flow and Galerkin for elasticity. We derive a contraction mapping, stability estimates and a priori error estimates for the discretized problem that incorporates convergence of the iteration at each time step. This result appears to be the first that treats the entire spatial-time system. A priori optimal rates of convergence are obtained when convergence of the iteration is achieved at each time step. Due to preference of mass conservation for flow, mixed finite elements are chosen for implementation. Galerkin approximation can be modified by either post processing, see Odsaeter et al. [30], or selecting Enriched Galerkin, see Lee et al. [31], to obtain mass conservation.

While the results presented here apply to the poro-elastic system, a novel feature of this work involves the discretized poro-elastic–elastic system. Such systems arise in coupled flow and poromechanics phenomena representing hydrocarbon production or CO2 sequestration in deep subsurface reservoirs. Here the spatial domain in which fluid flow occurs is generally much smaller than the spatial domain over which significant deformation occurs. The typical approach is to either impose an overburden pressure directly on the reservoir thus treating it as a coupled problem domain or to model flow on a huge domain with zero permeability cells to mimic the no flow boundary condition on the interface of the reservoir and the surrounding rock. The former approach precludes a study of land subsidence or uplift and further does not mimic the true effect of the overburden on stress sensitive reservoirs whereas the latter approach has huge computational costs. A field example that has motivated this work on poro-elastic–elastic sytems is the In Salah Gas Joint Venture in Algeria, a CO2 storage project operational from 2004 to 2011, see Iding and Ringrose [32]. The Krechba field was part of the In Salah gas field development and was the largest onshore CO2 storage site in the world. At Krechba, CO2 from several gas fields was removed from the production stream and injected into the deep saline carboniferous formation away from the producers. The large volume of injected CO2 caused ground upheaval. Surface deflection was recorded using remote sensing sensors on board of an INSAR (Interferometric Synthetic Aperture Radar) satellite. Here applying a compositional flow and geomechanics simulator up to the surface is extremely computationally costly due to the depth of the aquifer.

To address flow and mechanics modeling in deep subsurface reservoirs, a rigorous derivation of the interface conditions between a poro-elastic medium (the pay-zone) and an elastic body (the non-pay zone) was derived in Mikelić & Wheeler [33]. Here effective equations represent a two-scale system for three displacements and two pressures, coupled through the interface conditions with the Navier equations for the elastic displacement in the non-pay zone. The following appropriate interface conditions at the interface between an elastic and a poro-elastic medium were determined: (i) the displacement continuity, (ii) the effective normal stress continuity and (iii) the normal Darcy velocity zero from the poro-elastic side. This theoretically supports our computational approach for treating the poro-elasticity–elasticity domains in this paper.

This work is organized as follows. In the subsection below we establish notation. In Section 2, a continuous time model involving the decoupling of the model into elastic and poro-elastic domains with interface conditions is formulated both in primal and mixed form. The primal formulation, complete with the fixed-stress splitting algorithm, is fully discretized in Section 3. Convergence of the algorithm, which invokes stability of the scheme, is also established in Section 3. The a priori error equalities, inequalities, and error estimates are derived in Section 4. Section 5 is devoted to the discretization of the mixed formulation and a short survey of its convergence and numerical analysis. Computational results for the mixed scheme that confirm these error bounds are presented in Section 6.

1.1 Notation

In the sequel, we shall use the following functional notation; for the sake of simplicity, we define the spaces in three dimensions. In a region Ω, C 0 ( Ω ̅ ) Mathematical equation: $ {\mathcal{C}}^0\left(\overline{\mathrm{\Omega }}\right)$ denotes the space of continuous functions in Ω ̅ Mathematical equation: $ \overline{\mathrm{\Omega }}$. The scalar product of L2(Ω) is denoted by ( · , · ) Ω Mathematical equation: $ (\middot,\middot {)}_{\mathrm{\Omega }}$ f , g L 2 ( Ω ) ,   ( f , g ) Ω = Ω f ( x ) g ( x ) d x , Mathematical equation: $$ \forall f,g\in {L}^2(\mathrm{\Omega }),\enspace (f,g{)}_{\mathrm{\Omega }}={\int }_{\mathrm{\Omega }} f\left({x}\right)g\left({x}\right)\mathrm{d}{x}, $$and if the domain of integration is clear from the context, we suppress the index Ω Mathematical equation: $ \mathrm{\Omega }$. Let (k 1, k 2, k 3) denote a triple of non-negative integers, set |k| = k 1 + k 2 + k 3 and define the partial derivative k by k v = | k | v x 1 k 1 x 2 k 2 x 3 k 3 · Mathematical equation: $$ {\mathrm{\partial }}^kv=\frac{{\mathrm{\partial }}^{|k|}v}{\mathrm{\partial }{x}_1^{{k}_1}\mathrm{\partial }{x}_2^{{k}_2}\mathrm{\partial }{x}_3^{{k}_3}}\middot $$Then, for any non-negative integer m, recall the classical Sobolev space (cf. Adams [34] or Nečas [35]) H m ( Ω ) = { v L 2 ( Ω ) ;   k v L 2 ( Ω )   | k | m } , Mathematical equation: $$ {H}^m\left(\mathrm{\Omega }\right)=\left\{v\in {L}^2\left(\mathrm{\Omega }\right);\enspace {\mathrm{\partial }}^kv\in {L}^2\left(\mathrm{\Omega }\right)\hspace{1em}\forall \enspace \left|k\right|\le m\right\}, $$equipped with the following seminorm and norm (for which it is a Hilbert space) | v | H m ( Ω ) = [ | k | = m Ω | k v ( x ) | 2   d x ] 1 2 ,   | | v | | H m ( Ω ) = [ 0 | k | m | v | H k ( Ω ) 2 ] 1 2 . Mathematical equation: $$ |v{|}_{{H}^m\left(\mathrm{\Omega }\right)}={\left[\sum_{\left|k\right|=m} {\int }_{\mathrm{\Omega }} |{\mathrm{\partial }}^kv({x}){|}^2\enspace \mathrm{d}{x}\right]}^{\frac{1}{2}},\enspace {|\left|v\right||}_{{H}^m\left(\mathrm{\Omega }\right)}={\left[\sum_{0\le |k|\le m} |v{|}_{{H}^k(\mathrm{\Omega })}^2\right]}^{\frac{1}{2}}. $$This definition is extended to any real number s = m + s' for an integer m ≥ 0 and 0<s'<1 by defining in dimension d Mathematical equation: $ d$ the fractional semi-norm and norm: | v | H s ( Ω ) = ( | k | = m Ω Ω | k v ( x ) - k v ( y ) | 2 | x - y | d + 2   s '   d x d y ) 1 2 ,   | | v | | H s ( Ω ) = ( | | v | | H m ( Ω ) 2 + | v | H s ( Ω ) 2 ) 1 2 . Mathematical equation: $$ {|v{|}_{{H}^s(\mathrm{\Omega })}=\left(\sum_{|k|=m} {\int }_{\mathrm{\Omega }} {\int }_{\mathrm{\Omega }} \frac{|{\mathrm{\partial }}^kv({x})-{\mathrm{\partial }}^kv({y}){|}^2}{|{x}-{y}{|}^{d+2\enspace {s}^{\prime}}\enspace \mathrm{d}{x}\mathrm{d}{y}\right)}^{\frac{1}{2}},\enspace {|\left|v\right||}_{{H}^s\left(\mathrm{\Omega }\right)}={\left({||v||}_{{H}^m(\mathrm{\Omega })}^2+|v{|}_{{H}^s(\mathrm{\Omega })}^2\right)}^{\frac{1}{2}}. $$The reader can refer to Lions and Magenes [36] and Grisvard [37] for properties of these spaces. In particular, we have the following trace property in a domain Ω with Lipschitz continuous boundary Ω: If v belongs to H s (Ω) for some s ] 1 2 , 1 ] Mathematical equation: $ s\in ]\frac{1}{2},1]$, then its trace on Ω belongs to H s - 1 2 ( Ω ) Mathematical equation: $ {H}^{s-\frac{1}{2}}(\mathrm{\partial \Omega })$ and there exists a constant C such that v H s ( Ω ) ,   | | v | | H s - 1 2 ( Ω ) C | | v | | H s ( Ω ) . Mathematical equation: $$ \forall v\in {H}^s\left(\mathrm{\Omega }\right),\enspace {|\left|v\right||}_{{H}^{s-\frac{1}{2}}\left(\mathrm{\partial \Omega }\right)}\le C{|\left|v\right||}_{{H}^s\left(\mathrm{\Omega }\right)}. $$Finally, if Γ is a subset of Ω with positive measure, |Γ| > 0, we say that a function g in H 1 2 ( Γ ) Mathematical equation: $ {H}^{\frac{1}{2}}(\mathrm{\Gamma })$ belongs to H 00 1 2 ( Γ ) Mathematical equation: $ {H}_{00}^{\frac{1}{2}}(\mathrm{\Gamma })$ if its extension by zero to Ω Mathematical equation: $ \mathrm{\partial \Omega }$ belongs to H 1 2 ( Ω ) Mathematical equation: $ {H}^{\frac{1}{2}}(\mathrm{\partial \Omega })$. It is a proper subspace of H 1 2 ( Γ ) Mathematical equation: $ {H}^{\frac{1}{2}}(\mathrm{\Gamma })$, and is normed by | | v | | H 00 1 2 ( Γ ) = ( | v | H 1 2 ( Γ ) 2 + Γ | v ( x ) | 2   d x d ( x , Γ ) ) 1 2 , Mathematical equation: $$ {|\left|v\right||}_{{H}_{00}^{\frac{1}{2}}\left(\mathrm{\Gamma }\right)}={\left(|v{|}_{{H}^{\frac{1}{2}}\left(\mathrm{\Gamma }\right)}^2+{\int }_{\mathrm{\Gamma }} |v({x}){|}^2\enspace \frac{\mathrm{d}{x}}{\mathrm{d}\left({x},\mathrm{\Gamma }\right)}\right)}^{\frac{1}{2}}, $$(1)where | v | H 1 2 ( Γ ) = ( Γ Γ | v ( x ) - v ( y ) | 2 | x - y | d d x   d y ) 1 2 , Mathematical equation: $$ |v{|}_{{H}^{\frac{1}{2}}(\mathrm{\Gamma })}={\left({\int }_{\mathrm{\Gamma }} {\int }_{\mathrm{\Gamma }} \frac{|v({x})-v({y}){|}^2}{|{x}-{y}{|}^d}\mathrm{d}{x}\enspace \mathrm{d}{y}\right)}^{\frac{1}{2}}, $$and d( x , Γ) denotes the distance to Γ.

All the above definitions are directly extended to vector functions, with the same notation. The space H(div, Ω) is the Hilbert space H ( div , Ω ) = { v L 2 ( Ω ) d ;   div   v L 2 ( Ω ) } , Mathematical equation: $$ H(\mathrm{div},\mathrm{\Omega })=\{{v}\in {L}^2(\mathrm{\Omega }{)}^d;\enspace \mathrm{div}\enspace {v}\in {L}^2\left(\mathrm{\Omega }\right)\}, $$(2)equipped with the graph norm. The normal trace v ·  n of a function v of H(div, Ω) on Ω belongs to H - 1 2 ( Ω ) Mathematical equation: $ {H}^{-\frac{1}{2}}(\mathrm{\partial \Omega })$, the dual space of H 1 2 ( Ω ) Mathematical equation: $ {H}^{\frac{1}{2}}(\mathrm{\partial \Omega })$, see for instance Girault and Raviart [38]. The same result holds when Γ is a part of Ω and is a closed surface. But if Γ is not a closed surface, then v ·  n belongs to the dual of H 00 1 2 ( Γ ) Mathematical equation: $ {H}_{00}^{\frac{1}{2}}(\mathrm{\Gamma })$. We also recall Korn’s inequality, valid for all functions v in H 1 ( Ω ) d Mathematical equation: $ {H}^1(\mathrm{\Omega }{)}^d$ that vanish on Γ, | v | H 1 ( Ω ) C 1 ( Ω , Γ ) | | ε ( v ) | | L 2 ( Ω ) , Mathematical equation: $$ |{v}{|}_{{H}^1\left(\mathrm{\Omega }\right)}\le {C}_1\left(\mathrm{\Omega },\mathrm{\Gamma }\right){||{\epsilon }\left({v}\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}, $$(3)for a constant C 1(Ω, Γ) depending only on Ω and Γ. Here ε ( v ) denotes the strain tensor. When combined with Poincaré’s inequality, also valid for all functions v in H1(Ω) that vanish on Γ, with another constant C 2(Ω, Γ) depending only on Ω and Γ, | | v | | L 2 ( Ω ) C 2 ( Ω , Γ ) | v | H 1 ( Ω ) , Mathematical equation: $$ {||v||}_{{L}^2\left(\mathrm{\Omega }\right)}\le {C}_2(\mathrm{\Omega },\mathrm{\Gamma })|v{|}_{{H}^1\left(\mathrm{\Omega }\right)}, $$(4)we recover the full H1 norm in the left-hand side of (3): | | v | | H 1 ( Ω ) C 1 ( Ω , Γ ) ( 1 + C 2 2 ( Ω , Γ ) ) 1 2 | | ε ( v ) | | L 2 ( Ω ) . Mathematical equation: $$ {||{v}||}_{{H}^1\left(\mathrm{\Omega }\right)}\le {C}_1(\mathrm{\Omega },\mathrm{\Gamma })(1+{C}_2^2\left(\mathrm{\Omega },\mathrm{\Gamma }\right){)}^{\frac{1}{2}}{\left|\left|{\epsilon }\left({v}\right)\right|\right|}_{{L}^2\left(\mathrm{\Omega }\right)}. $$(5)

We also have the interpolation inequality v H 1 ( Ω ) ,   | | v | | L 2 ( Γ ) C ( Ω ) | | v | | L 2 ( Ω ) 1 2 | | v | | H 1 ( Ω ) 1 2 . Mathematical equation: $$ \forall v\in {H}^1(\mathrm{\Omega }),\enspace {||v||}_{{L}^2(\mathrm{\Gamma })}\le C(\mathrm{\Omega }){||v||}_{{L}^2(\mathrm{\Omega })}^{\frac{1}{2}}{||v||}_{{H}^1(\mathrm{\Omega })}^{\frac{1}{2}}. $$Thus by combining this with (4), (3), and (5), we derive the trace inequality for all functions v in H1(Ω) d that vanish on Γ v L 2 ( Γ ) C ( Ω ) C 1 ( Ω , Γ ) C 2 ( Ω , Γ ) 1 2 ( 1 + C 2 2 ( Ω , Γ ) ) 1 4 | | ε ( v ) | | L 2 ( Ω ) . Mathematical equation: $$ {\Vert {v}\Vert }_{{L}^2\left(\mathrm{\Gamma }\right)}\le C(\mathrm{\Omega }){C}_1(\mathrm{\Omega },\mathrm{\Gamma }){C}_2(\mathrm{\Omega },\mathrm{\Gamma }{)}^{\frac{1}{2}}(1+{C}_2^2(\mathrm{\Omega },\mathrm{\Gamma }){)}^{\frac{1}{4}}{||{\epsilon }({v})||}_{{L}^2\left(\mathrm{\Omega }\right)}. $$(6)

As usual, for handling time-dependent problems, it is convenient to consider measurable functions defined on a time interval]a, b[with values in a functional space, say X (cf. [36]). More precisely, let ||·|| X denote the norm of X Mathematical equation: $ X$; then for any number r, 1 ≤ r ≤ ∞, we define L r ( a , b ; X ) = { f   measurable   in   ] a , b [ ;   a b | | f ( t ) | | X r d t < } , Mathematical equation: $$ {L}^r(a,b;X)=\{f\enspace \mathrm{measurable}\enspace \mathrm{in}\enspace ]a,b[;\enspace {\int }_a^b {||f(t)||}_X^r\mathrm{d}t<\infty \}, $$equipped with the norm | | f | | L r ( a , b ; X ) = ( a b | | f ( t ) | | X r d t ) 1 r , Mathematical equation: $$ {||f||}_{{L}^r(a,b;X)}={\left({\int }_a^b {||f(t)||}_X^r\mathrm{d}t\right)}^{\frac{1}{r}}, $$with the usual modification if r = ∞. It is a Banach space if X is a Banach space, and for r = 2, it is a Hilbert space if X is a Hilbert space. We denote derivatives with respect to time by t and we define for instance H 1 ( a , b ; X ) = { f L 2 ( a , b ; X ) ;   t   f L 2 ( a , b ; X ) } . Mathematical equation: $$ {H}^1(a,b;X)=\{f\in {L}^2(a,b;X);\enspace {\mathrm{\partial }}_t\enspace f\in {L}^2(a,b;X)\}. $$Similarly, C 0 ( [ a , b ] ; X ) Mathematical equation: $ {\mathcal{C}}^0([a,b];X)$ is the space of continuous functions in [a, b] with values in X and | | f | | C 0 ( [ a , b ] ; X ) = sup t [ a , b ] | | f ( t ) | | X . Mathematical equation: $$ {||f||}_{{\mathcal{C}}^0([a,\hspace{0.5em}b];X)}=\underset{t\in \left[a,b\right]}{\mathrm{sup}}{|\left|f(t)\right||}_X. $$

2 Domain and model formulations

Let Ω be a bounded, connected, Lipschitz domain in R d Mathematical equation: $ {\mathbb{R}}^d$, d = 2, 3, and let Ω1 be a connected proper subset of Ω with a Lipschitz boundary that does not intersect the boundary of Ω, as in Figure 1. We set Ω 2 = Ω \ Ω ̅ 1 . Mathematical equation: $$ {\mathrm{\Omega }}_2=\mathrm{\Omega }\backslash {\overline{\mathrm{\Omega }}}_1. $$We are interested in the situation where a poro-elastic model holds in Ω1 (the pay-zone) while an elastic model holds in Ω2 (the non-pay zone) which is a non-porous region, see Figure 1. This work extends readily to more general configurations, but for simplicity, we focus on this situation. In reference [33], the model was derived from first principles:

  1. In Ω1, the quasi-static Biot’s system from consolidation theory.

  2. On the boundary of Ω1, the interface conditions between a poro-elastic medium and an elastic medium, i.e., the boundary conditions at a closed outer boundary for the quasi-static Biot system.

  3. In Ω2, the elasticity equations.

Thumbnail: Fig. 1 Refer to the following caption and surrounding text. Fig. 1

Pay-zone with surrounding rock.

Let Γ12 denote the boundary of Ω1 and let n 12 be the unit normal on Γ12 exterior to Ω1. Let the boundary of Ω Mathematical equation: $ \mathrm{\Omega }$, Ω Mathematical equation: $ \mathrm{\partial \Omega }$ be partitioned into two disjoint open regions, not necessarily connected, but with a finite number of connected components, Ω ̅ = Γ D ̅ Γ N ̅ ; Mathematical equation: $$ \overline{\mathrm{\partial \Omega }}=\overline{{\mathrm{\Gamma }}_D}\cup \overline{{\mathrm{\Gamma }}_N}; $$when d = 3, we suppose that the boundaries of Γ D and Γ N are both Lipschitz-continuous. We denote by n Ω the unit outward normal vector to Ω. To simplify, we assume that the measure of Γ D is positive: |Γ D | > 0. For the sake of brevity, we present the problem in the three-dimensional case. Let f be the body force in Ω. In the non-pay zone Ω2, the governing equations are those of linear elasticity. Recalling the Cauchy stress tensor for linear elasticity, σ ( u ) = λ ( · u ) I + 2 G ε ( u ) , Mathematical equation: $$ {\sigma }\left({u}\right)=\lambda \left(\nabla \middot {u}\right){I}+2G{\epsilon }\left({u}\right), $$(7)we have a.e. in Ω2 × ]0, T[ - · ( λ ( · u ) I + 2 G ε ( u ) ) = f . Mathematical equation: $$ -\nabla \middot \left(\lambda \left(\nabla \middot {u}\right){I}+2G{\epsilon }\left({u}\right)\right)={f}. $$(8)

In the pay-zone Ω1, we use Biot’s consolidation model for a linear elastic, homogeneous, isotropic, porous solid saturated with a slightly compressible fluid. The unknowns are the solid’s displacement u and the fluid’s pressure p. This model is based on a quasi-static assumption, namely it assumes that the material deformation is much slower than the flow rate, and hence the second time derivative of the displacement (i.e., the acceleration) is zero. We refer to [39] for the full derivation of the system of equations, but as an example, let us make precise the fluid’s density. The fluid’s density ρ f is related to the pressure by ρ f = ρ f , r ( 1 + c f ( p - p r ) ) , Mathematical equation: $$ {\rho }_f={\rho }_{f,r}(1+{c}_f(p-{p}_r)), $$where p r is a reference pressure, ρ f,r  > 0 a constant reference density relative to p r , and c f the fluid compressibility. But the fluid compressibility c f is assumed to be small (e.g. of the order of 10−8 or 10−9), and c f (p − p r ) is also small. Therefore this term is neglected and we replace ρ f by the constant ρ f,r . With this simplification, similar linearization, and arguing as in [39], we obtain the following system of equations a.e. in Ω1 × ]0, T[ t ( 1 M p + α   · u ) - 1 μ f · ( K ( p - ρ f , r ) ) = q , Mathematical equation: $$ {\mathrm{\partial }}_t\left(\frac{1}{M}p+\alpha \enspace \nabla \middot {u}\right)-\frac{1}{{\mu }_f}\nabla \middot \left({K}\nabla \left(p-{\rho }_{f,r}{g\eta }\right)\right)=q, $$(9) - · ( λ ( · u ) I + 2 G ε ( u ) - α p I ) = f . Mathematical equation: $$ -\nabla \middot \left(\lambda \left(\nabla \middot {u}\right){I}+2G{\epsilon }\left({u}\right)-{\alpha p}{I}\right)={f}. $$(10)

This system is complemented by an initial condition p ( 0 ) = p 0   in   Ω 1 . Mathematical equation: $$ p(0)={p}_0\enspace \mathrm{in}\enspace {\mathrm{\Omega }}_1. $$(11)Here λ > 0 and G > 0 are the Lamé coefficients, which for simplicity are assumed to be constant, α > 0 is the Biot-Willis constant, which is usually around one, μ f is the fluid’s viscosity assumed to be constant, φ 0 is the initial porosity, M > 0 is the Biot modulus satisfying, see Coussy [40], 1 M = ( α - φ 0 ) ( 1 - α ) K b + c f φ 0 , Mathematical equation: $$ \frac{1}{M}=\frac{(\alpha -{\phi }_0)(1-\alpha )}{{K}_b}+{c}_f{\phi }_0, $$where K b is the drained bulk modulus, g is the gravitation constant, η is the signed distance in the vertical direction, q is a volumetric fluid source term, and K is the permeability tensor, assumed to be symmetric, uniformly bounded, and uniformly positive definite, i.e., each eigenvalue λ i of K is real and there exist two constants λ min > 0 and λ max > 0 such that a.e . x Ω 1 ,   λ min λ i ( x ) λ max . Mathematical equation: $$ \mathrm{a.e}.\hspace{0.5em}{x}\in {\mathrm{\Omega }}_1,\enspace {\lambda }_{\mathrm{min}}\le {\lambda }_i\left({x}\right)\le {\lambda }_{\mathrm{max}}. $$(12)Strictly speaking, the initial condition should be given as ( 1 M p + α   · u ) ( t = 0 ) = 1 M p 0 + α   · u 0 . Mathematical equation: $$ \left(\frac{1}{M}p+\alpha \enspace \nabla \middot {u}\right)(t=0)=\frac{1}{M}{p}_0+\alpha \enspace \nabla \middot {{u}}_0. $$However, in practice, the pressure is either measured or computed through a hydrostatic assumption and the initial displacement is computed satisfying (10). When the data are sufficiently smooth, as stated below, initializing the pressure is sufficient to determine the solution.

As the boundary of Ω1 is reduced to Γ12, that is entirely contained in Ω, the only boundary conditions on Γ12 are in fact transmission conditions between the two regions. The equations themselves are steady, but the unknowns depend on time through the transmission conditions that are proposed below. On the boundary Ω, we prescribe mixed boundary conditions: u = 0   on   Γ D ,   σ ( u ) n Ω = t N   on   Γ N . Mathematical equation: $$ {u}=0\enspace \mathrm{on}\enspace {\mathrm{\Gamma }}_D,\enspace {\sigma }\left({u}\right){{n}}_{\mathrm{\Omega }}={{t}}_N\enspace \mathrm{on}\enspace {\mathrm{\Gamma }}_N. $$(13)

For the transmission conditions on the interface, we recall the definition of jump through Γ12 in the direction of the normal, for any smooth enough function v, [ v ] = ( v | Ω 1 - v | Ω 2 ) | Γ 12 . Mathematical equation: $$ [v]=(v{|}_{{\mathrm{\Omega }}_1}-v{|}_{{\mathrm{\Omega }}_2}){|}_{{\mathrm{\Gamma }}_{12}}. $$(14)Then, we prescribe the following transmission conditions, see [33, 41]: the   medium   is   continuous   [ u ] = 0 , Mathematical equation: $$ \mathrm{the}\enspace \mathrm{medium}\enspace \mathrm{is}\enspace \mathrm{continuous}\enspace \left[{u}\right]=0, $$(15) the   normal   stresses   are   continuous   [ σ ( u ) ] n 12 = α   p   n 12 , Mathematical equation: $$ \mathrm{the}\enspace \mathrm{normal}\enspace \mathrm{stresses}\enspace \mathrm{are}\enspace \mathrm{continuous}\enspace \left[{\sigma }\left({u}\right)\right]{{n}}_{12}=\alpha \enspace p\enspace {{n}}_{12}, $$(16) there   is   no   flow   at   the   interface   - 1 μ f ( K ( p - ρ f , r ) ) · n 12 = 0 . Mathematical equation: $$ \mathrm{there}\enspace \mathrm{is}\enspace \mathrm{no}\enspace \mathrm{flow}\enspace \mathrm{at}\enspace \mathrm{the}\enspace \mathrm{interface}\enspace -\frac{1}{{\mu }_f}\left({K}\nabla \left(p-{\rho }_{f,r}{g\eta }\right)\right)\middot {{n}}_{12}=0. $$(17)Concerning data regularity, we assume that f belongs to H1(0, T; L2(Ω) d ), q belongs to L21 × ]0, T[), t N is in H1(0, T; L2 N ) d ), and p 0 belongs to H1(Ω). These are not the most general data assumptions, but they are a convenient simplification for the applications we have in mind. Note that both f and t N are continuous in time and therefore f (0) and t N (0) are well-defined.

Finally, the mean stress σ ¯ Mathematical equation: $ \overline{\sigma }$ which will be used in the algorithm is defined by σ ¯ = λ · u - α p . Mathematical equation: $$ \overline{\sigma }=\lambda \nabla \middot {u}-{\alpha p}. $$(18)It is the hydrostatic stress borne by the composite. More precisely, the product of λ and the divergence of the displacement is borne by the skeletal solid, and the product of the Biot-Willis constant and the pore pressure is borne by the pore fluid. The negative sign in front of the pore pressure is due to the sign convention where tensile stresses are considered positive.

2.1 Primal variational formulation

Let us introduce the space H 0 D 1 ( Ω ) = { v H 1 ( Ω ) ;   v | Γ D = 0 } ,   V = H 0 D 1 ( Ω ) d . Mathematical equation: $$ {H}_{0D}^1(\mathrm{\Omega })=\{v\in {H}^1(\mathrm{\Omega });\enspace v{|}_{{\mathrm{\Gamma }}_D}=0\},\enspace {V}={H}_{0D}^1(\mathrm{\Omega }{)}^d. $$(19)As shown in reference [42], problem (9)(13), (15)(17) has the equivalent variational formulation: Find u in L(0, T; V ) and p in L(0,T; L21)) ∩ L2(0, T; H11)) solving v V ,   2 G ( ε ( u ) , ε ( v ) ) Ω + λ ( · u , · v ) Ω - α ( p , · v ) Ω 1 = ( f , v ) Ω + ( t N , v ) Γ N , Mathematical equation: $$ \forall {v}\in {V},\enspace 2G({\epsilon }({u}),{\epsilon }({v}){)}_{\mathrm{\Omega }}+\lambda (\nabla \middot {u},\nabla \middot {v}{)}_{\mathrm{\Omega }}-\alpha (p,\nabla \middot {v}{)}_{{\mathrm{\Omega }}_1}=({f},{v}{)}_{\mathrm{\Omega }}+({{t}}_N,{v}{)}_{{\mathrm{\Gamma }}_N}, $$(20) θ H 1 ( Ω 1 ) ,   ( t ( 1 M p + α · u ) , θ ) Ω 1 + 1 μ f ( K   ( p - ρ f , r ) ,   θ ) Ω 1 = ( q , θ ) Ω 1 , Mathematical equation: $$ \forall \theta \in {H}^1({\mathrm{\Omega }}_1),\enspace {\left({\mathrm{\partial }}_t\left(\frac{1}{M}p+\alpha \nabla \middot {u}\right),\theta \right)}_{{\mathrm{\Omega }}_1}+\frac{1}{{\mu }_f}({K}\enspace \nabla (p-{\rho }_{f,r}{g\eta }),\nabla \enspace \theta {)}_{{\mathrm{\Omega }}_1}=(q,\theta {)}_{{\mathrm{\Omega }}_1}, $$(21) p ( 0 ) = p 0   in   Ω 1 . Mathematical equation: $$ p(0)={p}_0\enspace \mathrm{in}\enspace {\mathrm{\Omega }}_1. $$We observe that the transmission conditions are such that no jump appears in the variational formulation.

2.2 Mixed variational formulation

We retain the displacement equation but use a mixed formulation for the flow because it leads to locally conservative discrete schemes. Although p Mathematical equation: $ p$ is continuous, the mixed formulation relaxes its regularity and allows us to take p Mathematical equation: $ p$ in L ( 0 ,   T ; L 2 ( Ω 1 ) ) Mathematical equation: $ {L}^{\mathrm{\infty }}(0,\enspace T;{L}^2({\mathrm{\Omega }}_1))$. We associate with the pressure in Ω 1 Mathematical equation: $ {\mathrm{\Omega }}_1$ an auxiliary Darcy velocity z defined by z = - K μ f ( p - ρ f , r ) , Mathematical equation: $$ {z}=-\frac{{K}}{{\mu }_f}\nabla \left(p-{\rho }_{f,r}{g\eta }\right), $$(22)and the space for the reservoir velocity is Z = { q H ( div , Ω 1 ) ;   q · n 12 = 0   on   Γ 12 } = H 0 ( div ; Ω 1 ) , Mathematical equation: $$ {Z}=\left\{{q}\in H\left(\mathrm{div},{\mathrm{\Omega }}_1\right);\enspace {q}\middot {{n}}_{12}=0\enspace \mathrm{on}\enspace {\mathrm{\Gamma }}_{12}\right\}={H}_0\left(\mathrm{div};{\mathrm{\Omega }}_1\right), $$(23)normed by | | q | | Z = | | q | | H ( div , Ω 1 ) . Mathematical equation: $$ {||{q}||}_{{Z}}={|\left|{q}\right||}_{H\left(\mathrm{div},{\mathrm{\Omega }}_1\right)}. $$(24)With the same data regularity, the mixed variational formulation reads: Find u L ( 0 , T ; V ) Mathematical equation: $ {u}\in {L}^{\mathrm{\infty }}(0,T;{V})$, p L ( 0 , T ; L 2 ( Ω 1 ) ) Mathematical equation: $ p\in {L}^{\mathrm{\infty }}(0,T;{L}^2({\mathrm{\Omega }}_1))$, and z L 2 ( 0 , T ; Z ) Mathematical equation: $ {z}\in {L}^2(0,T;{Z})$, such that v V ,   2 G ( ε ( u ) , ε ( v ) ) Ω + λ ( · u , · v ) Ω - α ( p , · v ) Ω 1 = ( f , v ) Ω + ( t N , v ) Γ N , Mathematical equation: $$ \forall {v}\in {V},\enspace 2G({\epsilon }({u}),{\epsilon }({v}){)}_{\mathrm{\Omega }}+\lambda (\nabla \middot {u},\nabla \middot {v}{)}_{\mathrm{\Omega }}-\alpha (p,\nabla \middot {v}{)}_{{\mathrm{\Omega }}_1}=({f},{v}{)}_{\mathrm{\Omega }}+({{t}}_N,{v}{)}_{{\mathrm{\Gamma }}_N}, $$(25) θ L 2 ( Ω ) ,   ( t ( 1 M p + α · u ) , θ ) Ω 1 + ( · z , θ ) Ω 1 = ( q , θ ) Ω 1 , Mathematical equation: $$ \forall \theta \in {L}^2(\mathrm{\Omega }),\enspace {\left({\mathrm{\partial }}_t\left(\frac{1}{M}p+\alpha \nabla \middot {u}\right),\theta \right)}_{{\mathrm{\Omega }}_1}+(\nabla \middot {z},\theta {)}_{{\mathrm{\Omega }}_1}=(q,\theta {)}_{{\mathrm{\Omega }}_1}, $$(26) ζ Z ,   ( μ f K - 1 z , ζ ) Ω 1 = ( p , · ζ ) Ω 1 + ( ( ρ f , r ) , ζ ) Ω 1 , Mathematical equation: $$ \forall {\zeta }\in {Z},\enspace ({\mu }_f{{K}}^{-1}{z},{\zeta }{)}_{{\mathrm{\Omega }}_1}=(p,\nabla \middot {\zeta }{)}_{{\mathrm{\Omega }}_1}+(\nabla ({\rho }_{f,r}{g\eta }),{\zeta }{)}_{{\mathrm{\Omega }}_1}, $$(27)subject to the initial condition (11): p ( 0 ) = p 0   in   Ω 1 . Mathematical equation: $$ p(0)={p}_0\enspace \mathrm{in}\enspace {\mathrm{\Omega }}_1. $$

3 Continuous Galerkin approximation and algorithm

In this and the next sections, the theory is developed for the primal formulation. To simplify the presentation, we describe here the case d = 3 Mathematical equation: $ d=3$, but everything carries over to d = 2 Mathematical equation: $ d=2$. Let P k Mathematical equation: $ {\mathbb{P}}_k$ denote the space of polynomials of total degree less than or equal to k Mathematical equation: $ k$ in d Mathematical equation: $ d$ variables. From now on, we assume that Ω Mathematical equation: $ \mathrm{\Omega }$ is a Lipschitz polyhedron and that the boundaries of Γ D Mathematical equation: $ {\mathrm{\Gamma }}_D$ and Γ N Mathematical equation: $ {\mathrm{\Gamma }}_N$ are polygonal. Let T h Mathematical equation: $ {\mathcal{T}}_h$ be a regular family of conforming triangulations of Ω ̅ Mathematical equation: $ \overline{\mathrm{\Omega }}$ consisting of tetrahedra, E Mathematical equation: $ E$, of maximum diameter h Mathematical equation: $ h$, and such that no element adjacent to Ω Mathematical equation: $ \mathrm{\partial \Omega }$ intersects both Γ D Mathematical equation: $ {\mathrm{\Gamma }}_D$ and Γ N Mathematical equation: $ {\mathrm{\Gamma }}_N$ and the interior of no element intersects Γ 12 Mathematical equation: $ {\mathrm{\Gamma }}_{12}$. We denote by T h , 1 Mathematical equation: $ {\mathcal{T}}_{h,1}$ the restriction of T h Mathematical equation: $ {\mathcal{T}}_h$ to Ω 1 Mathematical equation: $ {\mathrm{\Omega }}_1$. The restriction to simplicial elements is only a matter of convenience; the analysis below extends readily to other shapes such as hexahedra or prisms. As usual, we assume that these triangulations are regular in the sense of Ciarlet [43]: There exists a constant κ > 0 Mathematical equation: $ \kappa >0$, independent of h Mathematical equation: $ h$, such that E T h ,   h E ρ E φ E κ , Mathematical equation: $$ \forall E\in {\mathcal{T}}_h,\enspace \hspace{1em}\frac{{h}_E}{{\rho }_E}\mathbf{\coloneqq} {\phi }_E\le \kappa, $$(28)where h E h Mathematical equation: $ {h}_E\le h$ denotes the diameter of E Mathematical equation: $ E$ and ρ E denotes the diameter of the ball inscribed in E Mathematical equation: $ E$. On this triangulation, we introduce the standard finite element spaces X h = { v h H 1 ( Ω ) 3 ;   E T h , v h | E P k ( E ) 3 } ,   k 1 , Mathematical equation: $$ {{X}}_h=\{{{v}}_h\in {H}^1(\mathrm{\Omega }{)}^3;\enspace \forall E\in {\mathcal{T}}_h,{{v}}_h{|}_E\in {\mathbb{P}}_k(E{)}^3\},\enspace \hspace{1em}k\ge 1, $$ M h = { θ h H 1 ( Ω 1 ) ;   E T h , 1 , θ h | E P m ( E ) } ,   m 1 , Mathematical equation: $$ {M}_h=\{{\theta }_h\in {H}^1({\mathrm{\Omega }}_1);\enspace \forall E\in {\mathcal{T}}_{h,1},{\theta }_h{|}_E\in {\mathbb{P}}_m(E)\},\enspace \hspace{1em}m\ge 1, $$and we set V h = V X h . Mathematical equation: $$ {{V}}_h={V}\cap {{X}}_h. $$As the exact solution may possibly be not very smooth, it is approximated by Scott and Zhang interpolants (see [44]), say R h L ( H 1 ( Ω ) 3 , X h ) ,   Π h L ( H 1 ( Ω 1 ) , M h ) . Mathematical equation: $$ {R}_h\in \mathcal{L}({H}^1(\mathrm{\Omega }{)}^3,{{X}}_h),\enspace {\mathrm{\Pi }}_h\in \mathcal{L}({H}^1({\mathrm{\Omega }}_1),{M}_h). $$Considering the degree of the polynomial functions in X h Mathematical equation: $ {{X}}_h$ and M h Mathematical equation: $ {M}_h$, these interpolants have the following quasi-local approximation errors: E T h , v H s ( E ) ,   | v - R h ( v ) | H j ( E ) C   h E s - j | v | H s ( Δ E ) ,   1 s k + 1 ,   0 j s , Mathematical equation: $$ \forall E\in {\mathcal{T}}_h,\forall v\in {H}^s(E),\enspace |v-{R}_h(v){|}_{{H}^j(E)}\le C\enspace {h}_E^{s-j}|v{|}_{{H}^s({\Delta }_E)},\enspace 1\le s\le k+1,\enspace 0\le j\le s, $$(29) E T h , 1 , q H s ( E ) ,   | q - Π h ( q ) | H j ( E ) C   h E s - j | q | H s ( Δ E ) ,   1 s m + 1 ,   0 j s , Mathematical equation: $$ \forall E\in {\mathcal{T}}_{h,1},\forall q\in {H}^s(E),\enspace \left|q-{\mathrm{\Pi }}_h(q){|}_{{H}^j(E)}\le C\enspace {h}_E^{s-j}\right|q{|}_{{H}^s\left({\Delta }_E\right)},\enspace 1\le s\le m+1,\enspace 0\le j\le s, $$(30)with constants C independent of E and h, where Δ E is a small patch of elements including E containing the values used in computing the approximation.

Regarding approximation in time, we divide the interval [0, T] into N equal subintervals with length Δt and set t n  = nΔt. The choice of equal time steps is also a simplification; the material below extends readily to variable time steps. For the data, we set f n ( x ) = f ( x , t n ) ,   q n ( x ) = q ( x , t n ) ,   t N n ( x ) = t N ( x , t n ) . Mathematical equation: $$ {{f}}^n\left({x}\right)={f}\left({x},{t}_n\right),\enspace {q}^n\left({x}\right)=q\left({x},{t}_n\right),\enspace {{t}}_N^n\left({x}\right)={{t}}_N\left({x},{t}_n\right). $$(31)With these spaces, the fully discrete split problem is:

Initialization. Set p h 0 = Π h ( p 0 ) . Mathematical equation: $$ {p}_h^0={\mathrm{\Pi }}_h\left({p}^0\right). $$(32)Compute u h 0 V h Mathematical equation: $ {{u}}_h^0\in {{V}}_h$ and σ ¯ h 0 Mathematical equation: $ {\overline{\sigma }}_h^0$ by solving v h V h ,   2 G ( ε ( u h 0 ) , ε ( v h ) ) Ω + λ ( · u h 0 , · v h ) Ω = α   ( p h 0 , · v h ) Ω 1 + ( f , v h ) Ω + ( t N 0 , v h ) Γ N , Mathematical equation: $$ \forall {{v}}_h\in {{V}}_h,\enspace 2G({\epsilon }({{u}}_h^0),{\epsilon }({{v}}_h){)}_{\mathrm{\Omega }}+\lambda (\nabla \middot {{u}}_h^0,\nabla \middot {{v}}_h{)}_{\mathrm{\Omega }}=\alpha \enspace ({p}_h^0,\nabla \middot {{v}}_h{)}_{{\mathrm{\Omega }}_1}+({f},{{v}}_h{)}_{\mathrm{\Omega }}+({{t}}_N^0,{{v}}_h{)}_{{\mathrm{\Gamma }}_N}, $$(33)and setting σ ¯ h 0 = λ · u h 0 - α p h 0 . Mathematical equation: $$ {\overline{\sigma }}_h^0=\lambda \nabla \middot {{u}}_h^0-\alpha {p}_h^0. $$(34)

Time step. n ≥ 1.

  1. Set p h n , 0 = p h n - 1 Mathematical equation: $ {p}_h^{n,0}={p}_h^{n-1}$, u h n , 0 = u h n - 1 Mathematical equation: $ {{u}}_h^{n,0}={{u}}_h^{n-1}$, and σ ¯ h n , 0 = σ ¯ h n - 1 Mathematical equation: $ {\overline{\sigma }}_h^{n,0}={\overline{\sigma }}_h^{n-1}$.

  2. For l 1 Mathematical equation: $ \mathcal{l}\ge 1$, compute

(a) p h n , l M h Mathematical equation: $ {p}_h^{n,\mathcal{l}}\in {M}_h$ by solving θ h M h ,   ( 1 M + α 2 λ ) 1 Δ t ( p h n , l - p h n - 1 , θ h ) Ω 1 + 1 μ f ( K ( p h n , l - ρ f , r ) ,   θ h ) Ω 1 = α 2 λ 1 Δ t ( p h n , l - 1 - p h n - 1 , θ h ) Ω 1 - α Δ t ( · ( u h n , l - 1 - u h n - 1 ) , θ h ) Ω 1 + ( q n , θ h ) Ω 1 , Mathematical equation: $$ \forall {\theta }_h\in {M}_h,\enspace \left(\frac{1}{M}+\frac{{\alpha }^2}{\lambda }\right)\frac{1}{\Delta t}({p}_h^{n,\mathcal{l}}-{p}_h^{n-1},{\theta }_h{)}_{{\mathrm{\Omega }}_1}+\frac{1}{{\mu }_f}({K}\nabla ({p}_h^{n,\mathcal{l}}-{\rho }_{f,r}{g\eta }),\nabla \enspace {\theta }_h{)}_{{\mathrm{\Omega }}_1}=\frac{{\alpha }^2}{\lambda }\frac{1}{\Delta t}({p}_h^{n,\mathcal{l}-1}-{p}_h^{n-1},{\theta }_h{)}_{{\mathrm{\Omega }}_1}-\frac{\alpha }{\Delta t}(\nabla \middot ({{u}}_h^{n,\mathcal{l}-1}-{{u}}_h^{n-1}),{\theta }_h{)}_{{\mathrm{\Omega }}_1}+({q}^n,{\theta }_h{)}_{{\mathrm{\Omega }}_1}, $$(35)

(b) compute the predictor of the difference in fluid content δ φ p Mathematical equation: $ {\delta }_{\phi }^p$ by δ φ p : = ( 1 M + α 2 λ ) ( p h n , l - p h n , l - 1 ) , Mathematical equation: $$ \begin{array}{c}{\delta }_{\phi }^p:=(\frac{1}{M}+\frac{{\alpha }^2}{\lambda })({p}_h^{n,\mathcal{l}}-{p}_h^{n,\mathcal{l}-1}),\end{array} $$(36)

(c) σ ¯ h n , l Mathematical equation: $ {\overline{\sigma }}_h^{n,\mathcal{l}}$ by σ ¯ h n , l = λ · u h n , l - α p h n , l , Mathematical equation: $$ {\overline{\sigma }}_h^{n,\mathcal{l}}=\lambda \nabla \middot {{u}}_h^{n,\mathcal{l}}-\alpha {p}_h^{n,\mathcal{l}}, $$(37)

(d) compute the corrector to difference in fluid content δ φ c Mathematical equation: $ {\delta }_{\phi }^c$ by δ φ c : = α ( u h n , l - u h n , l - 1 ) + 1 M ( p h n , l - p h n , l - 1 ) . Mathematical equation: $$ {\delta }_{\phi }^c:=\alpha \nabla \cdot ({u}_h^{n,\mathcal{l}}-{u}_h^{n,\mathcal{l}-1})+\frac{1}{M}({p}_h^{n,\mathcal{l}}-{p}_h^{n,\mathcal{l}-1}). $$

If δ φ c - δ φ p : = α ( u h n , l - u h n , l - 1 ) - α 2 λ ( p h n , l - p h n , l - 1 ) > Mathematical equation: $ {\delta }_{\phi }^c-{\delta }_{\phi }^p:=\alpha \nabla \cdot ({u}_h^{n,\mathcal{l}}-{u}_h^{n,\mathcal{l}-1})-\frac{{\alpha }^2}{\lambda }({p}_h^{n,\mathcal{l}}-{p}_h^{n,\mathcal{l}-1})>$ threshold, increment l Mathematical equation: $ \mathcal{l}$ and return to (a);

if δ φ Mathematical equation: $ {\delta }_{\phi }\le $ threshold, set l n l ,   p h n p h n , l n ,   u h n u h n , l n ,   σ ¯ h n σ ¯ h n , l n , Mathematical equation: $$ {\mathcal{l}}_n\mathbf{\coloneqq} \mathcal{l},\hspace{1em}\enspace {p}_h^n\mathbf{\coloneqq} {p}_h^{n,{\mathcal{l}}_n},\hspace{1em}\enspace {{u}}_h^n\mathbf{\coloneqq} {{u}}_h^{n,{\mathcal{l}}_n},\hspace{1em}\enspace {\overline{\sigma }}_h^n\mathbf{\coloneqq} {\overline{\sigma }}_h^{n,{\mathcal{l}}_n}, $$(38)and march in time, set n ≔ n + 1 and return to step (1).

Considering the uniform positive definiteness of the permeability tensor K and the unique solvability of (20) and (21) for given p Mathematical equation: $ p$, it is clear that this algorithm generates a unique sequence.

3.1 Stability of the scheme and convergence of the algorithm

From the work of Mikelić and Wheeler in [45], see also (Girault et al. [10]), it can be shown that the fixed-stress algorithm (32)(37) produces a contracting sequence. More precisely, let β = 1 α 2 M + 1 λ . Mathematical equation: $$ \beta =\frac{1}{{\alpha }^2M}+\frac{1}{\lambda }. $$(39)

Then, we have for all n 1 Mathematical equation: $ n\ge 1$ and all l 2 Mathematical equation: $ \mathcal{l}\ge 2$, | | σ ¯ h n , l - σ ¯ h n , l - 1 | | L 2 ( Ω 1 ) 1 ( β   λ ) | | σ ¯ h n , l - 1 - σ ¯ h n , l - 2 | | L 2 ( Ω 1 ) , Mathematical equation: $$ {||{\overline{\sigma }}_h^{n,\mathcal{l}}-{\overline{\sigma }}_h^{n,\mathcal{l}-1}||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}\le \frac{1}{\left(\beta \enspace \lambda \right)}{||{\overline{\sigma }}_h^{n,\mathcal{l}-1}-{\overline{\sigma }}_h^{n,\mathcal{l}-2}||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}, $$(40)and since βλ > 1 and is independent of n and h, (40) implies that the sequence of the differences between two consecutive iterates of σ ¯ h n , l Mathematical equation: $ {\overline{\sigma }}_h^{n,\mathcal{l}}$ is contracting, uniformly in n and h. As a consequence, we have | | σ ¯ h n , l - σ ¯ h n , l - 1 | | L 2 ( Ω 1 ) 1 ( β λ ) l - 1 | | σ ¯ h n , 1 - σ ¯ h n - 1 | | L 2 ( Ω 1 ) , Mathematical equation: $$ {||{\overline{\sigma }}_h^{n,\mathcal{l}}-{\overline{\sigma }}_h^{n,\mathcal{l}-1}||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}\le \frac{1}{({\beta \lambda }{)}^{\mathcal{l}-1}}{||{\overline{\sigma }}_h^{n,1}-{\overline{\sigma }}_h^{n-1}||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}, $$(41)which implies convergence for fixed h Mathematical equation: $ h$, Δ t Mathematical equation: $ \Delta t$, and n Mathematical equation: $ n$.

3.1.1 Initial mean stress difference at each time step

It follows from (41) that convergence of the algorithm, uniform in time and space, depends on suitable bounds for σ ¯ h n , 1 - σ ¯ h n - 1 Mathematical equation: $ {\overline{\sigma }}_h^{n,1}-{\overline{\sigma }}_h^{n-1}$. We shall see below that this relies on the stability of the scheme, i.e., the uniform boundedness of the sequence of discrete solutions. Recall that σ ¯ h n , 1 - σ ¯ h n - 1 = - α ( p h n , 1 - p h n - 1 ) + λ · ( u h n , 1 - u h n - 1 ) . Mathematical equation: $$ {\overline{\sigma }}_h^{n,1}-{\overline{\sigma }}_h^{n-1}=-\alpha ({p}_h^{n,1}-{p}_h^{n-1})+\lambda \nabla \middot ({{u}}_h^{n,1}-{{u}}_h^{n-1}). $$Let us start with the second term. The following proposition shows that a bound for the second term reduces to a bound for the first term.

Proposition 3.1.

We have for all n, 1 ≤ n ≤ N, λ | | · ( u h n , 1 - u h n - 1 ) | | L 2 ( Ω 1 ) 2 α 2 λ | | p h n , 1 - p h n - 1 | | L 2 ( Ω 1 ) 2 + 1 2 G ( C 2 | | f n - f n - 1 | | L 2 ( Ω ) 2 + C ̃ 2 | | t N n - t N n - 1 | | L 2 ( Γ N ) 2 ) , Mathematical equation: $$ \lambda {||\nabla \middot \left({{u}}_h^{n,1}-{{u}}_h^{n-1}\right)||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2\le \frac{{\alpha }^2}{\lambda }{||{p}_h^{n,1}-{p}_h^{n-1}||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+\frac{1}{2G}\left({C}^2{||{{f}}^n-{{f}}^{n-1}||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+{\mathop{C}\limits^\tilde}^2{||{{t}}_N^n-{{t}}_N^{n-1}||}_{{L}^2\left({\mathrm{\Gamma }}_N\right)}^2\right), $$(42) where C = C 1 (Ω, Γ)C 2 (Ω, Γ) is the product of the constants of (3) and (4), and C ̃ Mathematical equation: $ \mathop{C}\limits^\tilde$ is the constant of (6).

Proof. The equation satisfied by u h n , 1 - u h n - 1 Mathematical equation: $ {{u}}_h^{n,1}-{{u}}_h^{n-1}$ is ( σ ( u h n , 1 - u h n - 1 ) , ε ( v h ) ) Ω = α ( p h n , 1 - p h n - 1 , · v h ) Ω 1 + ( f n - f n - 1 , v h ) Ω + ( t N n - t N n - 1 , v h ) Γ N , Mathematical equation: $$ ({\sigma }({{u}}_h^{n,1}-{{u}}_h^{n-1}),{\epsilon }({{v}}_h){)}_{\mathrm{\Omega }}=\alpha ({p}_h^{n,1}-{p}_h^{n-1},\nabla \middot {{v}}_h{)}_{{\mathrm{\Omega }}_1}+({{f}}^n-{{f}}^{n-1},{{v}}_h{)}_{\mathrm{\Omega }}+({{t}}_N^n-{{t}}_N^{n-1},{{v}}_h{)}_{{\mathrm{\Gamma }}_N}, $$where σ is defined in (7). By testing this equation with u h n , 1 - u h n - 1 Mathematical equation: $ {{u}}_h^{n,1}-{{u}}_h^{n-1}$ and applying (3), (4), and (6), we derive 2 G | | ε ( u h n , 1 - u h n - 1 ) | | L 2 ( Ω ) 2 + λ | | · ( u h n , 1 - u h n - 1 ) | | L 2 ( Ω ) 2 α | | p h n , 1 - p h n - 1 | | L 2 ( Ω 1 ) | | · ( u h n , 1 - u h n - 1 ) | | L 2 ( Ω 1 ) + ( C | | f n - f n - 1 | | L 2 ( Ω ) + C ̃ | | t N n - t N n - 1 | | L 2 ( Γ N ) ) | | ε ( u h n , 1 - u h n - 1 ) | | L 2 ( Ω ) . Mathematical equation: $$ 2G{||{\epsilon }({{u}}_h^{n,1}-{{u}}_h^{n-1})||}_{{L}^2(\mathrm{\Omega })}^2+\lambda {||\nabla \middot ({{u}}_h^{n,1}-{{u}}_h^{n-1})||}_{{L}^2(\mathrm{\Omega })}^2\le \alpha {||{p}_h^{n,1}-{p}_h^{n-1}||}_{{L}^2({\mathrm{\Omega }}_1)}{||\nabla \middot ({{u}}_h^{n,1}-{{u}}_h^{n-1})||}_{{L}^2({\mathrm{\Omega }}_1)}+(C{||{{f}}^n-{{f}}^{n-1}||}_{{L}^2(\mathrm{\Omega })}+\mathop{C}\limits^\tilde{||{{t}}_N^n-{{t}}_N^{n-1}||}_{{L}^2({\mathrm{\Gamma }}_N)}){||{\epsilon }({{u}}_h^{n,1}-{{u}}_h^{n-1})||}_{{L}^2(\mathrm{\Omega })}. $$Then (42) follows by suitable applications of Young’s inequality

The next proposition treats the first term. The result is easily derived by testing (35) when l = 1 Mathematical equation: $ \mathcal{l}=1$ with θ h = p h n , 1 - p h n - 1 Mathematical equation: $ {\theta }_h={p}_h^{n,1}-{p}_h^{n-1}$, adding and subtracting the term ( K   p h n - 1 ,   θ h ) Ω 1 Mathematical equation: $ ({K}\nabla \enspace {p}_h^{n-1},\nabla \enspace {\theta }_h{)}_{{\mathrm{\Omega }}_1}$ and suitably applying Young’s inequality.

Proposition 3.2.

We have for all n Mathematical equation: $ n$, 1 n N Mathematical equation: $ 1\le n\le N$, α 2 β Δ t | | p h n , 1 - p h n - 1 | | L 2 ( Ω 1 ) 2 + 1 μ f | | K 1 2 ( p h n , 1 - p h n - 1 ) | | L 2 ( Ω 1 ) 2 Δ t α 2 β | | q n | | L 2 ( Ω 1 ) 2 + 1 μ f | | K 1 2 ( p h n - 1 - ρ f , r ) | | L 2 ( Ω 1 ) 2 , Mathematical equation: $$ \frac{{\alpha }^2\beta }{\Delta t}{||{p}_h^{n,1}-{p}_h^{n-1}||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+\frac{1}{{\mu }_f}{||{{K}}^{\frac{1}{2}}\nabla \left({p}_h^{n,1}-{p}_h^{n-1}\right)||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2\le \frac{\Delta t}{{\alpha }^2\beta }{||{q}^n||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+\frac{1}{{\mu }_f}{||{{K}}^{\frac{1}{2}}\nabla \left({p}_h^{n-1}-{\rho }_{f,r}{g\eta }\right)||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2, $$(43) where β is defined by (39).

Hence a bound for σ ¯ h n , 1 - σ ¯ h n - 1 Mathematical equation: $ {\overline{\sigma }}_h^{n,1}-{\overline{\sigma }}_h^{n-1}$ readily follows by combining Propositions 3.1 and 3.2.

Lemma 3.1.

We have for all n, 1 ≤ n ≤ N, with the constants C and C ̃ Mathematical equation: $ \mathop{C}\limits^\tilde$ of Proposition 3.1 , | | σ ¯ h n , 1 - σ ¯ h n - 1 | | L 2 ( Ω 1 ) 2 4 Δ t β ( 1 μ f | | K 1 2 ( p h n - 1 - ρ f , r ) | | L 2 ( Ω 1 ) 2 + Δ t α 2 β | | q n | | L 2 ( Ω 1 ) 2 ) + λ G ( C 2 | | f n - f n - 1 | | L 2 ( Ω ) 2 + C ̃ 2 | | t N n - t N n - 1 | | L 2 ( Γ N ) 2 ) . Mathematical equation: $$ {||{\overline{\sigma }}_h^{n,1}-{\overline{\sigma }}_h^{n-1}||}_{{L}^2({\mathrm{\Omega }}_1)}^2\le 4\frac{\Delta t}{\beta }\left(\frac{1}{{\mu }_f}{||{{K}}^{\frac{1}{2}}\nabla ({p}_h^{n-1}-{\rho }_{f,r}{g\eta })||}_{{L}^2({\mathrm{\Omega }}_1)}^2+\frac{\Delta t}{{\alpha }^2\beta }{||{q}^n||}_{{L}^2({\mathrm{\Omega }}_1)}^2\right)+\frac{\lambda }{G}({C}^2{||{{f}}^n-{{f}}^{n-1}||}_{{L}^2(\mathrm{\Omega })}^2+{\mathop{C}\limits^\tilde}^2{||{{t}}_N^n-{{t}}_N^{n-1}||}_{{L}^2({\mathrm{\Gamma }}_N)}^2). $$(44)

In view of the assumptions on the data, it follows that | | σ ¯ h n , 1 - σ ¯ h n - 1 | | L 2 ( Ω 1 ) 2 Mathematical equation: $ {||{\overline{\sigma }}_h^{n,1}-{\overline{\sigma }}_h^{n-1}||}_{{L}^2({\mathrm{\Omega }}_1)}^2$ is bounded provided Δ t | | K 1 2 ( p h n - 1 - ρ f , r ) | | L 2 ( Ω 1 ) 2 Mathematical equation: $ \Delta t{||{{K}}^{\frac{1}{2}}\nabla ({p}_h^{n-1}-{\rho }_{f,r}{g\eta })||}_{{L}^2({\mathrm{\Omega }}_1)}^2$ is also bounded. This raises the issue of stability.

3.1.2 Stability of the scheme

Here we investigate the uniform boundedness of the sequences ( u h n , p h n ) Mathematical equation: $ ({{u}}_h^n,{p}_h^n)$ generated by the algorithm in (11), i.e., when the threshold is met. Thus the displacement equation (36) is written (without the superscript l Mathematical equation: $ \mathcal{l}$), v h V h ,   2 G ( ε ( u h n ) , ε ( v h ) ) Ω + λ ( · u h n , · v h ) Ω = α ( p h n , · v h ) Ω 1 + ( f n , v h ) Ω + ( t N n , v h ) Γ N , Mathematical equation: $$ \begin{array}{l}\forall {{v}}_h\in {{V}}_h,\enspace 2G({\epsilon }({{u}}_h^n),{\epsilon }({{v}}_h){)}_{\mathrm{\Omega }}+\lambda (\nabla \middot {{u}}_h^n,\nabla \middot {{v}}_h{)}_{\mathrm{\Omega }}=\alpha ({p}_h^n,\nabla \middot {{v}}_h{)}_{{\mathrm{\Omega }}_1}+({{f}}^n,{{v}}_h{)}_{\mathrm{\Omega }}+({{t}}_N^n,{{v}}_h{)}_{{\mathrm{\Gamma }}_N},\end{array} $$(45)while the flow equation (35) written at level l = l n Mathematical equation: $ \mathcal{l}={\mathcal{l}}_n$ can be reformulated as θ h M h ,   1 M 1 Δ t ( p h n - p h n - 1 , θ h ) Ω 1 + α Δ t ( · ( u h n - u h n - 1 ) , θ h ) Ω 1 + 1 μ f ( K ( p h n - ρ f , r ) ,   θ h ) Ω 1 = α λ 1 Δ t ( σ ¯ h n - σ ¯ h n , l n - 1 , θ h ) Ω 1 + ( q n , θ h ) Ω 1 . Mathematical equation: $$ \forall {\theta }_h\in {M}_h,\enspace \frac{1}{M}\frac{1}{\Delta t}({p}_h^n-{p}_h^{n-1},{\theta }_h{)}_{{\mathrm{\Omega }}_1}+\frac{\alpha }{\Delta t}(\nabla \middot ({{u}}_h^n-{{u}}_h^{n-1}),{\theta }_h{)}_{{\mathrm{\Omega }}_1}+\frac{1}{{\mu }_f}({K}\nabla ({p}_h^n-{\rho }_{f,r}{g\eta }),\nabla \enspace {\theta }_h{)}_{{\mathrm{\Omega }}_1}=\frac{\alpha }{\lambda }\frac{1}{\Delta t}({\overline{\sigma }}_h^n-{\overline{\sigma }}_h^{n,{\mathcal{l}}_n-1},{\theta }_h{)}_{{\mathrm{\Omega }}_1}+({q}^n,{\theta }_h{)}_{{\mathrm{\Omega }}_1}. $$(46)

The following proposition is written under the assumption that the time step satisfies Δ t 1 2 Mathematical equation: $ \Delta t\le \frac{1}{2}$, but the choice 1 2 Mathematical equation: $ \frac{1}{2}$ is purely a matter of convenience. Indeed, as the asymptotic analysis must be written for Δt < 1, otherwise the order of the scheme is meaningless, then 1 2 Mathematical equation: $ \frac{1}{2}$ can be replaced by any number strictly smaller than one.

Proposition 3.3.

Let f Mathematical equation: $ {f}$ belong to C 0 ( 0 , T ; L 2 ( Ω ) d ) Mathematical equation: $ {\mathcal{C}}^0(0,T;{L}^2(\Omega {)}^d)$, q Mathematical equation: $ q$ to C 0 ( 0 , T ; L 2 ( Ω 1 ) ) Mathematical equation: $ {\mathcal{C}}^0(0,T;{L}^2({\Omega }_1))$ , and t N Mathematical equation: $ {{t}}_N$ to C 0 ( 0 , T ; L 2 ( Γ N ) d ) Mathematical equation: $ {\mathcal{C}}^0(0,T;{L}^2({\Gamma }_N{)}^d)$ . Assume that Δ t 1 2 Mathematical equation: $ {\Delta t}\le \frac{1}{2}$ . For any m Mathematical equation: $ m$ , let p ¯ h m = p h m - ρ Mathematical equation: $ {\bar{p}}_h^m={p}_h^m-{\rho g\eta }$ . The following bound holds for all n Mathematical equation: $ n$, 1 n N Mathematical equation: $ 1\le n\le N$, 1 M ( | | p ¯ h n | | L 2 ( Ω 1 ) 2 + m = 1 n - 1 | | p h m - p h m - 1 | | L 2 ( Ω 1 ) 2 ) + G ( | | ε ( u h n ) | | L 2 ( Ω ) 2 + 2 m = 1 n | | ε ( u h m - u h m - 1 ) | | L 2 ( Ω ) 2 ) + λ ( m = 1 n | | · ( u h m - u h m - 1 ) | | L 2 ( Ω ) 2 ) + 2 μ f m = 1 n Δ t | | K 1 2   p ¯ h m | | L 2 ( Ω 1 ) 2 1 M m = 1 n - 1 Δ t | | p ¯ h m | | L 2 ( Ω 1 ) 2 + G m = 1 n - 1 Δ t | | ε ( u h m ) | | L 2 ( Ω ) 2 + 5 M α 2 λ 2 1 Δ t m = 1 n | | σ ¯ h m - σ ¯ h m , l m - 1 | | L 2 ( Ω 1 ) 2 + I h 0 + D h n , Mathematical equation: $$ \frac{1}{M}\left({||{\bar{p}}_h^n||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+\sum_{m=1}^{n-1} {||{p}_h^m-{p}_h^{m-1}||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2\right)+G\left({||{\epsilon }\left({{u}}_h^n\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+2\sum_{m=1}^n {||{\epsilon }\left({{u}}_h^m-{{u}}_h^{m-1}\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2\right)+\lambda \left(\sum_{m=1}^n {||\nabla \middot \left({{u}}_h^m-{{u}}_h^{m-1}\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2\right)+\frac{2}{{\mu }_f}\sum_{m=1}^n \Delta t{||{{K}}^{\frac{1}{2}}\nabla \enspace {\bar{p}}_h^m||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2\le \frac{1}{M}\sum_{m=1}^{n-1} \Delta t{||{\bar{p}}_h^m||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+G\sum_{m=1}^{n-1} \Delta t{||{\epsilon }\left({{u}}_h^m\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+5M\frac{{\alpha }^2}{{\lambda }^2}\frac{1}{\Delta t}\sum_{m=1}^n {||{\overline{\sigma }}_h^m-{\overline{\sigma }}_h^{m,{\mathcal{l}}_m-1}||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+{\mathcal{I}}_h^0+{\mathcal{D}}_h^n, $$(47) where I h 0 Mathematical equation: $ {\mathcal{I}}_h^0$ and D h n Mathematical equation: $ {\mathcal{D}}_h^n$ are respectively contributions of the initial terms and data, I h 0 = 1 M | | p ¯ h 0 | | L 2 ( Ω 1 ) 2 + 3 G | | ε ( u h 0 ) | | L 2 ( Ω ) 2 + 2 λ | | · u h 0 | | L 2 ( Ω ) 2 , Mathematical equation: $$ {\mathcal{I}}_h^0=\frac{1}{M}{||{\bar{p}}_h^0||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+3G{||{\epsilon }\left({{u}}_h^0\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+2\lambda {||\nabla \middot {{u}}_h^0||}_{{L}^2\left(\mathrm{\Omega }\right)}^2, $$(48) D h n = 2 C 2 G ( | | f 1 | | L 2 ( Ω ) 2 + | | f n | | L 2 ( Ω ) 2 + m = 1 n - 1 1 Δ t | | f m + 1 - f m | | L 2 ( Ω ) 2 ) + 2 C ̃ 2 G ( | | t N 1 | | L 2 ( Γ N ) 2 + | | t N n | | L 2 ( Γ N ) 2 + m = 1 n - 1 1 Δ t | | t N m + 1 - t N m | | L 2 ( Γ N ) 2 ) + 5 M m = 1 n Δ t | | q m | | L 2 ( Ω 1 ) 2 + 2 λ α 2 | | ρ | | L 2 ( Ω 1 ) 2 , Mathematical equation: $$ {\mathcal{D}}_h^n=\frac{2{C}^2}{G}\left({||{{f}}^1||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+{||{{f}}^n||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+\sum_{m=1}^{n-1} \frac{1}{\Delta t}{||{{f}}^{m+1}-{{f}}^m||}_{{L}^2\left(\mathrm{\Omega }\right)}^2\right)+\frac{2{\mathop{C}\limits^\tilde}^2}{G}\left({||{{t}}_N^1||}_{{L}^2\left({\mathrm{\Gamma }}_N\right)}^2+{||{{t}}_N^n||}_{{L}^2\left({\mathrm{\Gamma }}_N\right)}^2+\sum_{m=1}^{n-1} \frac{1}{\Delta t}{||{{t}}_N^{m+1}-{{t}}_N^m||}_{{L}^2\left({\mathrm{\Gamma }}_N\right)}^2\right)+5M\sum_{m=1}^n \Delta t{||{q}^m||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+\frac{2}{\lambda }{\alpha }^2{||{\rho g\eta }||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2, $$(49) with the constants C and C ̃ Mathematical equation: $ \mathop{C}\limits^\tilde$ of Proposition 3.1 .

Proof. Since ρ f,r is a polynomial of degree one (independent of time), p ¯ h m Mathematical equation: $ {\bar{p}}_h^m$ belongs to M h and (46) can be tested at time t m with θ h = p ¯ h m Mathematical equation: $ {\theta }_h={\bar{p}}_h^m$. Then by testing (45) with v h = 1 Δ t ( u h m - u h m - 1 ) Mathematical equation: $ {{v}}_h=\frac{1}{\Delta t}({{u}}_h^m-{{u}}_h^{m-1})$, adding the resulting equations and multiplying by 2Δt, we derive, 1 M ( | | p ¯ h m | | L 2 ( Ω 1 ) 2 - | | p ¯ h m - 1 | | L 2 ( Ω 1 ) 2 + | | p h m - p h m - 1 | | L 2 ( Ω 1 ) 2 ) + 2 G ( | | ε ( u h m ) | | L 2 ( Ω ) 2 - | | ε ( u h m - 1 ) | | L 2 ( Ω ) 2 + | | ε ( u h m - u h m - 1 ) | | L 2 ( Ω ) 2 ) + λ ( | | · u h m | | L 2 ( Ω ) 2 - | | · u h m - 1 | | L 2 ( Ω ) 2 + | | · ( u h m - u h m - 1 ) | | L 2 ( Ω ) 2 ) + 2 μ f Δ t | | K 1 2   p ¯ h m | | L 2 ( Ω 1 ) 2 = 2 Δ t ( q m , p ¯ h m ) Ω 1 + 2 α λ ( σ ¯ h m - σ ¯ h m , l m - 1 , p ¯ h m ) Ω 1 + 2 ( f m , u h m - u h m - 1 ) Ω + 2 ( t N m , u h m - u h m - 1 ) Γ N + 2 α ( ρ f , r , · ( u h m - u h m - 1 ) ) Ω 1 . Mathematical equation: $$ \frac{1}{M}({||{\bar{p}}_h^m||}_{{L}^2({\mathrm{\Omega }}_1)}^2-{||{\bar{p}}_h^{m-1}||}_{{L}^2({\mathrm{\Omega }}_1)}^2+{||{p}_h^m-{p}_h^{m-1}||}_{{L}^2({\mathrm{\Omega }}_1)}^2)+2G({||{\epsilon }({{u}}_h^m)||}_{{L}^2(\mathrm{\Omega })}^2-{||{\epsilon }({{u}}_h^{m-1})||}_{{L}^2(\mathrm{\Omega })}^2+{||{\epsilon }({{u}}_h^m-{{u}}_h^{m-1})||}_{{L}^2(\mathrm{\Omega })}^2)+\lambda ({||\nabla \middot {{u}}_h^m||}_{{L}^2(\mathrm{\Omega })}^2-{||\nabla \middot {{u}}_h^{m-1}||}_{{L}^2(\mathrm{\Omega })}^2+{||\nabla \middot ({{u}}_h^m-{{u}}_h^{m-1})||}_{{L}^2(\mathrm{\Omega })}^2)+\frac{2}{{\mu }_f}\Delta t{||{{K}}^{\frac{1}{2}}\nabla \enspace {\bar{p}}_h^m||}_{{L}^2({\mathrm{\Omega }}_1)}^2=2\Delta t({q}^m,{\bar{p}}_h^m{)}_{{\mathrm{\Omega }}_1}+2\frac{\alpha }{\lambda }({\overline{\sigma }}_h^m-{\overline{\sigma }}_h^{m,{\mathcal{l}}_m-1},{\bar{p}}_h^m{)}_{{\mathrm{\Omega }}_1}+2({{f}}^m,{{u}}_h^m-{{u}}_h^{m-1}{)}_{\mathrm{\Omega }}+2({{t}}_N^m,{{u}}_h^m-{{u}}_h^{m-1}{)}_{{\mathrm{\Gamma }}_N}+2\alpha ({\rho }_{f,r}{g\eta },\nabla \middot ({{u}}_h^m-{{u}}_h^{m-1}){)}_{{\mathrm{\Omega }}_1}. $$(50)To apply Gronwall’s Lemma, it is convenient to write at level n Mathematical equation: $ n$, p ¯ h n = p h n - p h n - 1 + p ¯ h n - 1 Mathematical equation: $ {\bar{p}}_h^n={p}_h^n-{p}_h^{n-1}+{\bar{p}}_h^{n-1}$. For any γ > 0, we have 2 Δ t | ( q n , p h n - p h n - 1 ) Ω 1 | γ 1 M Δ t | | p h n - p h n - 1 | | L 2 ( Ω 1 ) 2 + 1 γ M Δ t | | q n | | L 2 ( Ω 1 ) 2 . Mathematical equation: $$ 2\Delta t|({q}^n,{p}_h^n-{p}_h^{n-1}{)}_{{\mathrm{\Omega }}_1}|\le \gamma \frac{1}{M}\Delta t{||{p}_h^n-{p}_h^{n-1}||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+\frac{1}{\gamma }M\Delta t{||{q}^n||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2. $$(51)Similarly, 2 α λ | ( σ ¯ h n - σ ¯ h n , l n - 1 , p h n - p h n - 1 ) Ω 1 | γ 1 M Δ t | | p h n - p h n - 1 | | L 2 ( Ω 1 ) 2 + 1 γ M 1 Δ t α 2 λ 2 | | σ ¯ h n - σ ¯ h n , l n - 1 | | L 2 ( Ω 1 ) 2 . Mathematical equation: $$ 2\frac{\alpha }{\lambda }|({\overline{\sigma }}_h^n-{\overline{\sigma }}_h^{n,{\mathcal{l}}_n-1},{p}_h^n-{p}_h^{n-1}{)}_{{\mathrm{\Omega }}_1}|\le \gamma \frac{1}{M}\Delta t{||{p}_h^n-{p}_h^{n-1}||}_{{L}^2({\mathrm{\Omega }}_1)}^2+\frac{1}{\gamma }M\frac{1}{\Delta t}\frac{{\alpha }^2}{{\lambda }^2}{||{\overline{\sigma }}_h^n-{\overline{\sigma }}_h^{n,{\mathcal{l}}_n-1}||}_{{L}^2({\mathrm{\Omega }}_1)}^2. $$(52)Choose γ = 1. Since Δ t 1 2 Mathematical equation: $ \Delta t\le \frac{1}{2}$, the term involving p h n - p h n - 1 Mathematical equation: $ {p}_h^n-{p}_h^{n-1}$ is balanced by the same term in the left-hand side of (23). With another γ > 0, we obtain 2 Δ t | ( q n , p ¯ h n - 1 ) Ω 1 | γ 1 M Δ t | | p ¯ h n - 1 | | L 2 ( Ω 1 ) 2 + 1 γ M Δ t | | q n | | L 2 ( Ω 1 ) 2 , Mathematical equation: $$ 2\Delta t|({q}^n,{\bar{p}}_h^{n-1}{)}_{{\mathrm{\Omega }}_1}|\le \gamma \frac{1}{M}\Delta t{||{\bar{p}}_h^{n-1}||}_{{L}^2({\mathrm{\Omega }}_1)}^2+\frac{1}{\gamma }M\Delta t{||{q}^n||}_{{L}^2({\mathrm{\Omega }}_1)}^2, $$ 2 α λ | ( σ ¯ h n - σ ¯ h n , l n - 1 , p ¯ h n - 1 ) Ω 1 | γ 1 M Δ t | | p ¯ h n - 1 | | L 2 ( Ω 1 ) 2 + 1 γ M 1 Δ t α 2 λ 2 | | σ ¯ h n - σ ¯ h n , l n - 1 | | L 2 ( Ω 1 ) 2 . Mathematical equation: $$ 2\frac{\alpha }{\lambda }|({\overline{\sigma }}_h^n-{\overline{\sigma }}_h^{n,{\mathcal{l}}_n-1},{\bar{p}}_h^{n-1}{)}_{{\mathrm{\Omega }}_1}|\le \gamma \frac{1}{M}\Delta t{||{\bar{p}}_h^{n-1}||}_{{L}^2({\mathrm{\Omega }}_1)}^2+\frac{1}{\gamma }M\frac{1}{\Delta t}\frac{{\alpha }^2}{{\lambda }^2}{||{\overline{\sigma }}_h^n-{\overline{\sigma }}_h^{n,{\mathcal{l}}_n-1}||}_{{L}^2({\mathrm{\Omega }}_1)}^2. $$At level m = n − 1, this splitting is not necessary and we simply write for any γ' > 0, 2 Δ t | ( q m , p ¯ h m ) Ω 1 | γ 1 M Δ t | | p ¯ h m | | L 2 ( Ω 1 ) 2 + 1 γ M Δ t | | q m | | L 2 ( Ω 1 ) 2 , Mathematical equation: $$ 2\Delta t|({q}^m,{\bar{p}}_h^m{)}_{{\mathrm{\Omega }}_1}|\le {\gamma }^\mathrm{\prime}\frac{1}{M}\Delta t{||{\bar{p}}_h^m||}_{{L}^2({\mathrm{\Omega }}_1)}^2+\frac{1}{{\gamma }^\mathrm{\prime}}M\Delta t{||{q}^m||}_{{L}^2({\mathrm{\Omega }}_1)}^2, $$ 2 α λ | ( σ ¯ h m - σ ¯ h m , l m - 1 , p ¯ h m ) Ω 1 | γ 1 M Δ t | | p ¯ h m | | L 2 ( Ω 1 ) 2 + 1 γ M 1 Δ t α 2 λ 2 | | σ ¯ h m - σ ¯ h m , l m - 1 | | L 2 ( Ω 1 ) 2 . Mathematical equation: $$ 2\frac{\alpha }{\lambda }|({\overline{\sigma }}_h^m-{\overline{\sigma }}_h^{m,{\mathcal{l}}_m-1},{\bar{p}}_h^m{)}_{{\mathrm{\Omega }}_1}|\le {\gamma }^\mathrm{\prime}\frac{1}{M}\Delta t{||{\bar{p}}_h^m||}_{{L}^2({\mathrm{\Omega }}_1)}^2+\frac{1}{{\gamma }^\mathrm{\prime}}M\frac{1}{\Delta t}\frac{{\alpha }^2}{{\lambda }^2}{||{\overline{\sigma }}_h^m-{\overline{\sigma }}_h^{m,{\mathcal{l}}_m-1}||}_{{L}^2({\mathrm{\Omega }}_1)}^2. $$By choosing γ = γ = 1 4 Mathematical equation: $ \gamma ={\gamma }^\mathrm{\prime}=\frac{1}{4}$, the total contribution of p ¯ h n - 1 Mathematical equation: $ {\bar{p}}_h^{n-1}$ from levels n and n − 1 is 1 M Δ t | | p ¯ h n - 1 | | L 2 ( Ω 1 ) 2 . Mathematical equation: $$ \frac{1}{M}\Delta t{||{\bar{p}}_h^{n-1}||}_{{L}^2({\mathrm{\Omega }}_1)}^2. $$The levels m ≤ n − 2 are treated as level n − 1; a more favorable value of γ′ can be chosen, but for the sake of simplicity, it is not used here. These inequalities are summed over m from 1 to n, but the three terms in the last line of (50) are summed by parts because we have no control on 1 Δ t ( u h m - u h m - 1 ) Mathematical equation: $ \frac{1}{\Delta t}({{u}}_h^m-{{u}}_h^{m-1})$. Thus, we write in view of (3), (4), and considering (6), | m = 1 n ( f m , u h m - u h m - 1 ) Ω | C ( m = 1 n - 1 | | f m + 1 - f m | | L 2 ( Ω ) | | ε ( u h m ) | | L 2 ( Ω ) + | | f n | | L 2 ( Ω ) | | ε ( u h n ) | | L 2 ( Ω ) + | | f 1 | | L 2 ( Ω ) | | ε ( u h 0 ) | | L 2 ( Ω ) ) , Mathematical equation: $$ \left|\sum_{m=1}^n ({{f}}^m,{{u}}_h^m-{{u}}_h^{m-1}{)}_{\mathrm{\Omega }}\right|\le C\left(\sum_{m=1}^{n-1} {||{{f}}^{m+1}-{{f}}^m||}_{{L}^2\left(\mathrm{\Omega }\right)}{||{\epsilon }({{u}}_h^m)||}_{{L}^2\left(\mathrm{\Omega }\right)}+{||{{f}}^n||}_{{L}^2\left(\mathrm{\Omega }\right)}{||{\epsilon }({{u}}_h^n)||}_{{L}^2\left(\mathrm{\Omega }\right)}+{||{{f}}^1||}_{{L}^2\left(\mathrm{\Omega }\right)}{||{\epsilon }\left({{u}}_h^0\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}\right), $$(53) | m = 1 n ( t N m , u h m - u h m - 1 ) Γ N | C ̃ ( m = 1 n - 1 t N m + 1 - t N m L 2 ( Γ N ) ε ( u h m ) L 2 ( Ω ) + t N n L 2 ( Γ N ) ε ( u h n ) L 2 ( Ω ) + t N 1 L 2 ( Γ N ) ε ( u h 0 ) L 2 ( Ω ) ) . Mathematical equation: $$ \left|\sum_{m=1}^n ({{t}}_N^m,{{u}}_h^m-{{u}}_h^{m-1}{)}_{{\mathrm{\Gamma }}_N}\right|\le \mathop{C}\limits^\tilde\left(\sum_{m=1}^{n-1} {\Vert {{t}}_N^{m+1}-{{t}}_N^m\Vert }_{{L}^2({\mathrm{\Gamma }}_N)}{\Vert {\epsilon }({{u}}_h^m)\Vert }_{{L}^2(\mathrm{\Omega })}+{\Vert {{t}}_N^n\Vert }_{{L}^2({\mathrm{\Gamma }}_N)}{\Vert {\epsilon }({{u}}_h^n)\Vert }_{{L}^2(\mathrm{\Omega })}+{\Vert {{t}}_N^1\Vert }_{{L}^2({\mathrm{\Gamma }}_N)}{\Vert {\epsilon }({{u}}_h^0)\Vert }_{{L}^2(\mathrm{\Omega })}\right). $$Finally, 2 α m = 1 n ( ρ f , r , · ( u h m - u h m - 1 ) ) Ω 1 = 2 α ( ρ f , r , · ( u h n ) ) Ω 1 - 2 α ( ρ f , r , · ( u h 0 ) ) Ω 1 . Mathematical equation: $$ 2\alpha \sum_{m=1}^n ({\rho }_{f,r}{g\eta },\nabla \middot ({{u}}_h^m-{{u}}_h^{m-1}){)}_{{\mathrm{\Omega }}_1}=2\alpha ({\rho }_{f,r}{g\eta },\nabla \middot ({{u}}_h^n){)}_{{\mathrm{\Omega }}_1}-2\alpha ({\rho }_{f,r}{g\eta },\nabla \middot ({{u}}_h^0){)}_{{\mathrm{\Omega }}_1}. $$The desired result follows by applying Young’s inequality to the above terms.

In view of (32) and (33), the initial terms of (48) are easily bounded independently of h Mathematical equation: $ h$. If, in addition to the assumptions of Proposition 3.3, f Mathematical equation: $ {f}$ and t N Mathematical equation: $ {{t}}_N$ are H 1 Mathematical equation: $ {H}^1$ in time then the terms of (49) are bounded independently of n Mathematical equation: $ n$, h Mathematical equation: $ h$, and Δt. Therefore, it remains to control the term σ ¯ h m - σ ¯ h m , l m - 1 Mathematical equation: $ {\overline{\sigma }}_h^m-{\overline{\sigma }}_h^{m,{\mathcal{l}}_m-1}$. This is done by combining the contraction property (41) with Lemma 3.1 and it yields α 2 λ 2 5 M 1 Δ   t | | σ ¯ h m - σ ¯ h m , l m - 1 | | L 2 ( Ω 1 ) 2 α 2 λ 2 5 M 1 ( β 2 λ 2 ) l m - 1 × ( 4 β ( 1 μ f | | K 1 2 ( p h m - 1 - ρ f , r ) | | L 2 ( Ω 1 ) 2 + Δ t α 2 β | | q m | | L 2 ( Ω 1 ) 2 ) + λ G 1 Δ   t ( C 2 | | f m - f m - 1 | | L 2 ( Ω ) 2 + C ̃ 2 | | t N m - t N m - 1 | | L 2 ( Γ N ) 2 ) ) . Mathematical equation: $$ \frac{{\alpha }^2}{{\lambda }^2}5M\frac{1}{\Delta \enspace t}{||{\overline{\sigma }}_h^m-{\overline{\sigma }}_h^{m,{\mathcal{l}}_m-1}||}_{{L}^2({\mathrm{\Omega }}_1)}^2\le \frac{{\alpha }^2}{{\lambda }^2}5M\frac{1}{({\beta }^2{\lambda }^2{)}^{{\mathcal{l}}_m-1}}\times \left(\frac{4}{\beta }\left(\frac{1}{{\mu }_f}{||{{K}}^{\frac{1}{2}}\nabla ({p}_h^{m-1}-{\rho }_{f,r}{g\eta })||}_{{L}^2({\mathrm{\Omega }}_1)}^2+\frac{\Delta t}{{\alpha }^2\beta }{||{q}^m||}_{{L}^2({\mathrm{\Omega }}_1)}^2\right)+\frac{\lambda }{G}\frac{1}{\Delta \enspace t}\left({C}^2{||{{f}}^m-{{f}}^{m-1}||}_{{L}^2(\mathrm{\Omega })}^2+{\mathop{C}\limits^\tilde}^2{||{{t}}_N^m-{{t}}_N^{m-1}||}_{{L}^2({\mathrm{\Gamma }}_N)}^2\right)\right). $$(54)All terms above are easily bounded except for the one involving K 1 2 ( p h m - 1 - ρ f , r ) Mathematical equation: $ {{K}}^{\frac{1}{2}}\nabla ({p}_h^{m-1}-{\rho }_{f,r}{g\eta })$ because it lacks a factor Δt in order to be controlled by the left-hand side of (47). To recover a factor Δt, we use the contraction and assume that the number of iterations is sufficiently large. This implies stability of the scheme.

Theorem 3.1.

Let f belong to H 1 ( 0 , T ; L 2 ( Ω ) d ) Mathematical equation: $ {H}^1(0,T;{L}^2(\Omega {)}^d)$, q Mathematical equation: $ q$ to C 0 ( 0 , T ; L 2 ( Ω 1 ) ) Mathematical equation: $ {\mathcal{C}}^0(0,T;{L}^2({\Omega }_1))$ , and t N Mathematical equation: $ {{t}}_N$ to H 1 ( 0 , T ; L 2 ( Γ N ) d ) Mathematical equation: $ {H}^1(0,T;{L}^2({\Gamma }_N{)}^d)$ . Assume that Δ t 1 2 Mathematical equation: $ {\Delta t}\le \frac{1}{2}$ . If for each m, 1 ≤ m ≤ N, the number of iterations l m Mathematical equation: $ {\mathcal{l}}_m$ satisfies 1 ( β λ ) 2 l m 1 M Δ t 10 α 2 β , Mathematical equation: $$ \frac{1}{({\beta \lambda }{)}^{2{\mathcal{l}}_m}}\le \frac{1}{M}\frac{\Delta t}{10{\alpha }^2\beta }, $$(55) then there exists a constant C independent of n, h, and Δt, such that 1 M | | p h n | | L 2 ( Ω 1 ) 2 + G | | ε ( u h n ) | | L 2 ( Ω ) 2 + λ | | · u h n | | L 2 ( Ω ) 2 + 1 μ f m = 1 n Δ t | | K 1 2   p h m | | L 2 ( Ω 1 ) 2 C   exp ( t n ) . Mathematical equation: $$ \frac{1}{M}{||{p}_h^n||}_{{L}^2({\mathrm{\Omega }}_1)}^2+G{||{\epsilon }({{u}}_h^n)||}_{{L}^2(\mathrm{\Omega })}^2+\lambda {||\nabla \middot {{u}}_h^n||}_{{L}^2(\mathrm{\Omega })}^2+\frac{1}{{\mu }_f}\sum_{m=1}^n \Delta t{||{{K}}^{\frac{1}{2}}\nabla \enspace {p}_h^m||}_{{L}^2({\mathrm{\Omega }}_1)}^2\le C\enspace \mathrm{exp}({t}_n). $$(56)

Proof. The assumption (55) implies that the factor of K 1 2   p ¯ h m - 1 Mathematical equation: $ {{K}}^{\frac{1}{2}}\nabla \enspace {\bar{p}}_h^{m-1}$ satisfies α 2 λ 2 20 β M 1 ( β 2 λ 2 ) l m - 1 2 Δ t . Mathematical equation: $$ \frac{{\alpha }^2}{{\lambda }^2}\frac{20}{\beta }M\frac{1}{({\beta }^2{\lambda }^2{)}^{{\mathcal{l}}_m-1}}\le 2\Delta t. $$(57)Therefore this term is controlled by the same term in the left-hand side of (47). With the above regularity of the data, an application of Gronwall’s Lemma yields a uniform bound for p h n Mathematical equation: $ {p}_h^n$ and ε ( u h n ) Mathematical equation: $ {\epsilon }({{u}}_h^n)$. In turn, this bound permits to estimate · ( u h n ) Mathematical equation: $ \nabla \middot ({{u}}_h^n)$ and 1 μ f m = 1 n Δ t | | K 1 2   p h m | | L 2 ( Ω 1 ) 2 Mathematical equation: $ \frac{1}{{\mu }_f}{\sum }_{m=1}^n \Delta t{||{{K}}^{\frac{1}{2}}\nabla \enspace {p}_h^m||}_{{L}^2({\mathrm{\Omega }}_1)}^2$, uniformly with respect to h Mathematical equation: $ h$, n Mathematical equation: $ n$, and Δt. Finally, the regularity of ρgη implies a similar bound for p h n Mathematical equation: $ {p}_h^n$.

Remark 3.1. The exponential factor in the right-hand side of (56) can be avoided by using L − L1 bounds in time such as | m = 1 n Δ t ( q m , p ¯ h m ) Ω 1 | sup 1 m n | | p ¯ h m | | L 2 ( Ω 1 ) m = 1 n Δ t | | q m | | L 2 ( Ω 1 ) . Mathematical equation: $$ |\sum_{m=1}^n \Delta t({q}^m,{\bar{p}}_h^m{)}_{{\mathrm{\Omega }}_1}|\le \underset{1\le m\le n}{\mathrm{sup}}{||{\bar{p}}_h^m||}_{{L}^2({\mathrm{\Omega }}_1)}\sum_{m=1}^n \Delta t{||{q}^m||}_{{L}^2({\mathrm{\Omega }}_1)}. $$This is sound, as long as it is done with data, but the same strategy applied to | m = 1 n ( σ ¯ h m - σ ¯ h m , l m - 1 , p ¯ h m ) Ω 1 | Mathematical equation: $$ |\sum_{m=1}^n ({\overline{\sigma }}_h^m-{\overline{\sigma }}_h^{m,{\mathcal{l}}_{m-1}},{\bar{p}}_h^m{)}_{{\mathrm{\Omega }}_1}| $$leads to a relation between l m Mathematical equation: $ {\mathcal{l}}_m$ and Δt that is less favorable than that given by (55).

4 A priori error estimates

As expected, the above stability proof will be extended to derive a priori error estimates. As the main ingredient is the contribution of the algorithmic error, we begin by revisiting this error. Throughout this section, we use the notation (31) and for convenience we denote by δ the finite difference in time for any function f, δ f = f n - f n - 1 . Mathematical equation: $$ {\delta f}={f}^n-{f}^{n-1}. $$(58)

4.1 The algorithmic error

Let us start with an arbitrary value of l Mathematical equation: $ \mathcal{l}$. Recall that the contraction property yields (41), | | σ ¯ h n , l - σ ¯ h n , l - 1 | | L 2 ( Ω 1 ) 1 ( β   λ ) l - 1 | | σ ¯ h n , 1 - σ ¯ h n - 1 | | L 2 ( Ω 1 ) , Mathematical equation: $$ {||{\overline{\sigma }}_h^{n,\mathcal{l}}-{\overline{\sigma }}_h^{n,\mathcal{l}-1}||}_{{L}^2({\mathrm{\Omega }}_1)}\le \frac{1}{(\beta \enspace \lambda {)}^{\mathcal{l}-1}}{||{\overline{\sigma }}_h^{n,1}-{\overline{\sigma }}_h^{n-1}||}_{{L}^2({\mathrm{\Omega }}_1)}, $$where σ ¯ h n , 1 - σ ¯ h n - 1 = λ · ( u h n , 1 - u h n - 1 ) - α ( p h n , 1 - p h n - 1 ) . Mathematical equation: $$ {\overline{\sigma }}_h^{n,1}-{\overline{\sigma }}_h^{n-1}=\lambda \nabla \middot ({{u}}_h^{n,1}-{{u}}_h^{n-1})-\alpha ({p}_h^{n,1}-{p}_h^{n-1}). $$We have seen in Proposition 3.1 that λ 2 | | · ( u h n , 1 - u h n - 1 ) | | L 2 ( Ω 1 ) 2 α 2 | | p h n , 1 - p h n - 1 | | L 2 ( Ω 1 ) 2 + λ 2 G ( C 2 | | f n - f n - 1 | | L 2 ( Ω ) 2 + C ̃ 2 | | t N n - t N n - 1 | | L 2 ( Γ N ) 2 ) , Mathematical equation: $$ {\lambda }^2{||\nabla \middot \left({{u}}_h^{n,1}-{{u}}_h^{n-1}\right)||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2\le {\alpha }^2{||{p}_h^{n,1}-{p}_h^{n-1}||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+\frac{\lambda }{2G}\left({C}^2{||{{f}}^n-{{f}}^{n-1}||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+{\mathop{C}\limits^\tilde}^2{||{{t}}_N^n-{{t}}_N^{n-1}||}_{{L}^2\left({\mathrm{\Gamma }}_N\right)}^2\right), $$(59)with the constants C and C ̃ Mathematical equation: $ \mathop{C}\limits^\tilde$ of (42). The next proposition sharpens the bound for the pressure in Proposition 3.2. Below, we use the notation for any function q, q ¯ m = q m - ρ f , r , Mathematical equation: $$ {\bar{q}}^m={q}^m-{\rho }_{f,r}{g\eta }, $$(60)Π h denotes an arbitrary space approximation operator that takes its values in M h and for any function q in L1(0, T), m(q) is the average of q in time, m ( q ) = 1 Δ t t n - 1 t n q ( s ) d s . Mathematical equation: $$ m(q)=\frac{1}{\Delta t}{\int }_{{t}_{n-1}}^{{t}_n} q(s)\mathrm{d}s. $$(61)

Proposition 4.1.

Assuming that the solution is sufficiently smooth in time, we have for all n, 1 ≤ n ≤ N, α 2 | | p ¯ h n , 1 - p ¯ h n - 1 | | L 2 ( Ω 1 ) 2 Δ t β   μ f ( | | K 1 2 ( p ¯ h n - 1 - Π h ( p ¯ n - 1 ) ) | | L 2 ( Ω 1 ) 2 + | | K 1 2 ( Π h ( p ¯ n - 1 ) - m ( p ¯ ) ) | | L 2 ( Ω 1 ) 2 ) + 2 ( Δ t ) 2 α 2 β 2 | | q n - m ( q ) | | L 2 ( Ω 1 ) 2 + 2 Δ t α 2 β 2 | | t ( 1 M p + α · u ) | | L 2 ( Ω 1 × ] t n - 1 , t n [ ) 2 , Mathematical equation: $$ {\alpha }^2{||{\bar{p}}_h^{n,1}-{\bar{p}}_h^{n-1}||}_{{L}^2({\mathrm{\Omega }}_1)}^2\le \frac{\Delta t}{\beta \enspace {\mu }_f}({||{{K}}^{\frac{1}{2}}\nabla ({\bar{p}}_h^{n-1}-{\mathrm{\Pi }}_h({\bar{p}}^{n-1}))||}_{{L}^2({\mathrm{\Omega }}_1)}^2+{||{{K}}^{\frac{1}{2}}\nabla ({\mathrm{\Pi }}_h({\bar{p}}^{n-1})-m(\bar{p}))||}_{{L}^2({\mathrm{\Omega }}_1)}^2)+2\frac{(\Delta t{)}^2}{{\alpha }^2{\beta }^2}{||{q}^n-m(q)||}_{{L}^2({\mathrm{\Omega }}_1)}^2+2\frac{\Delta t}{{\alpha }^2{\beta }^2}{||{\mathrm{\partial }}_t(\frac{1}{M}p+\alpha \nabla \middot {u})||}_{{L}^2({\mathrm{\Omega }}_1\times ]{t}_{n-1},{t}_n[)}^2, $$(62) where β is defined by (39).

Proof. By proceeding as in Proposition 3.2, subtracting K   Π h ( p ¯ n - 1 ) Mathematical equation: $ {K}\nabla \enspace {\mathrm{\Pi }}_h({\bar{p}}^{n-1})$, and K   m ( p ¯ ) Mathematical equation: $ {K}\nabla \enspace m(\bar{p})$, and recalling that ρ f,r is independent of time, we first write α 2 β Δ t | | p ¯ h n , 1 - p ¯ h n - 1 | | L 2 ( Ω 1 ) 2 + 1 μ f | | K 1 2 ( p ¯ h n , 1 - p ¯ h n - 1 ) | | L 2 ( Ω 1 ) 2 = - 1 μ f ( K ( p ¯ h n - 1 - Π h ( p ¯ n - 1 ) ) , ( p ¯ h n , 1 - p ¯ h n - 1 ) ) Ω 1 - 1 μ f ( K ( Π h ( p ¯ n - 1 ) - m ( p ¯ ) ) , ( p ¯ h n , 1 - p ¯ h n - 1 ) ) Ω 1 - 1 μ f ( K   m ( p ¯ ) , ( p ¯ h n , 1 - p ¯ h n - 1 ) ) Ω 1 + ( q n , p ¯ h n , 1 - p ¯ h n - 1 ) Ω 1 . Mathematical equation: $$ \frac{{\alpha }^2\beta }{\Delta t}{||{\bar{p}}_h^{n,1}-{\bar{p}}_h^{n-1}||}_{{L}^2({\mathrm{\Omega }}_1)}^2+\frac{1}{{\mu }_f}{||{{K}}^{\frac{1}{2}}\nabla ({\bar{p}}_h^{n,1}-{\bar{p}}_h^{n-1})||}_{{L}^2({\mathrm{\Omega }}_1)}^2=-\frac{1}{{\mu }_f}({K}\nabla ({\bar{p}}_h^{n-1}-{\mathrm{\Pi }}_h({\bar{p}}^{n-1})),\nabla ({\bar{p}}_h^{n,1}-{\bar{p}}_h^{n-1}){)}_{{\mathrm{\Omega }}_1}-\frac{1}{{\mu }_f}({K}\nabla ({\mathrm{\Pi }}_h({\bar{p}}^{n-1})-m(\bar{p})),\nabla ({\bar{p}}_h^{n,1}-{\bar{p}}_h^{n-1}){)}_{{\mathrm{\Omega }}_1}-\frac{1}{{\mu }_f}({K}\nabla \enspace m(\bar{p}),\nabla ({\bar{p}}_h^{n,1}-{\bar{p}}_h^{n-1}){)}_{{\mathrm{\Omega }}_1}+({q}^n,{\bar{p}}_h^{n,1}-{\bar{p}}_h^{n-1}{)}_{{\mathrm{\Omega }}_1}. $$By integrating the flow equation (21) over]t n − 1, t n [, the end of the last line above can be written as ( q n - m ( q ) + 1 Δ t t n - 1 t n t ( 1 M p ( s ) + α · u ( s ) ) , p ¯ h n , 1 - p ¯ h n - 1 ) Ω 1 d s . Mathematical equation: $$ {\left({q}^n-m(q)+\frac{1}{\Delta t}{\int }_{{t}_{n-1}}^{{t}_n} {\mathrm{\partial }}_t\left(\frac{1}{M}p(s)+\alpha \nabla \middot {u}(s)\right),{\bar{p}}_h^{n,1}-{\bar{p}}_h^{n-1}\right)}_{{\mathrm{\Omega }}_1}\mathrm{d}{s}. $$Then (62) follows by suitable applications of Young’s inequality.

Thus, by combining (59), (62), and (41), we derive an upper bound for | | σ ¯ h n , l - σ ¯ h n , l - 1 | | L 2 ( Ω 1 ) 2 Mathematical equation: $ {||{\overline{\sigma }}_h^{n,\mathcal{l}}-{\overline{\sigma }}_h^{n,\mathcal{l}-1}||}_{{L}^2({\mathrm{\Omega }}_1)}^2$, | | σ ¯ h n , l - σ ¯ h n , l - 1 | | L 2 ( Ω 1 ) 2 1 ( β   λ ) 2 l - 2 [ λ G ( C 2 | | f n - f n - 1 | | L 2 ( Ω ) 2 + C ̃ 2 | | t N n - t N n - 1 | | L 2 ( Γ N ) 2 ) + 4 ( Δ t μ f β ( | | K 1 2 ( p ¯ h n - 1 - Π h ( p ¯ n - 1 ) ) | | L 2 ( Ω 1 ) 2 + | | K 1 2 ( Π h ( p ¯ n - 1 ) - m ( p ¯ ) ) | | L 2 ( Ω 1 ) 2 ) + 2 ( Δ t ) 2 α 2 β 2 | | q n - m ( q ) | | L 2 ( Ω 1 ) 2 + 2 Δ t α 2 β 2 t ( 1 M p + α · u ) L ( Ω 1 × ] t n - 1 , t n [ ) 2 2 ) ] . Mathematical equation: $$ {||{\overline{\sigma }}_h^{n,\mathcal{l}}-{\overline{\sigma }}_h^{n,\mathcal{l}-1}||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2\le \frac{1}{(\beta \enspace \lambda {)}^{2\mathcal{l}-2}}\left[\frac{\lambda }{G}\left({C}^2{||{{f}}^n-{{f}}^{n-1}||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+{\mathop{C}\limits^\tilde}^2{||{{t}}_N^n-{{t}}_N^{n-1}||}_{{L}^2\left({\mathrm{\Gamma }}_N\right)}^2\right)+4\left(\frac{\Delta t}{{\mu }_f\beta }\left({||{{K}}^{\frac{1}{2}}\nabla ({\bar{p}}_h^{n-1}-{\mathrm{\Pi }}_h({\bar{p}}^{n-1}))||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+{||{{K}}^{\frac{1}{2}}\nabla ({\mathrm{\Pi }}_h({\bar{p}}^{n-1})-m(\bar{p}))||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2\right)+2\frac{(\Delta t{)}^2}{{\alpha }^2{\beta }^2}{||{q}^n-m(q)||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+2\frac{\Delta t}{{\alpha }^2{\beta }^2}{\Vert {\mathrm{\partial }}_t\left(\frac{1}{M}p+\alpha \nabla \middot {u}\right)\Vert }_{{L}_{\left({\mathrm{\Omega }}_1\times \right]{t}_{n-1},{t}_n[)}^2}^2\right)\right]. $$(63)

4.2 Error equation

In addition to Π h , we shall apply to the displacement an arbitrary approximation operator R h that takes its values in V h .

Let us integrate the flow equation (21) over]t n − 1, t n [, tested with θ h , and divide both sides by Δt; with the notation (58), (60), and (61), this gives 1 M 1 Δ t ( δ p ¯ n , θ h ) Ω 1 + α Δ t ( · δ u n , θ h ) Ω 1 + 1 μ f 1 Δ t t n - 1 t n ( K ( p ¯ ( s ) ,   θ h ) Ω 1 d s = ( m ( q ) , θ h ) Ω 1 . Mathematical equation: $$ \frac{1}{M}\frac{1}{\Delta t}(\delta {\bar{p}}^n,{\theta }_h{)}_{{\mathrm{\Omega }}_1}+\frac{\alpha }{\Delta t}(\nabla \middot \delta {{u}}^n,{\theta }_h{)}_{{\mathrm{\Omega }}_1}+\frac{1}{{\mu }_f}\frac{1}{\Delta t}{\int }_{{t}_{n-1}}^{{t}_n} ({K}\nabla (\bar{p}(s),\nabla \enspace {\theta }_h{)}_{{\mathrm{\Omega }}_1}\mathrm{d}s=(m(q),{\theta }_h{)}_{{\mathrm{\Omega }}_1}. $$By subtracting (35) at level l = l n Mathematical equation: $ \mathcal{l}={\mathcal{l}}_n$ from this equation (see (46)), we obtain for all θ h  ∈ M h , 1 M 1 Δ t ( δ ( p ¯ n - p ¯ h n ) , θ h ) Ω 1 + α Δ t ( · ( δ ( u n - u h n ) ) , θ h ) Ω 1 + 1 μ f 1 Δ t t n - 1 t n ( K ( p ¯ ( s ) - p ¯ h n ) ,   θ h ) Ω 1 d s = 1 Δ t t n - 1 t n ( q ( s ) - q n , θ h ) Ω 1 d s - α λ 1 Δ t ( σ ¯ h n - σ ¯ h n , l n - 1 , θ h ) Ω 1 . Mathematical equation: $$ \frac{1}{M}\frac{1}{\Delta t}(\delta ({\bar{p}}^n-{\bar{p}}_h^n),{\theta }_h{)}_{{\mathrm{\Omega }}_1}+\frac{\alpha }{\Delta t}(\nabla \middot (\delta ({{u}}^n-{{u}}_h^n)),{\theta }_h{)}_{{\mathrm{\Omega }}_1}+\frac{1}{{\mu }_f}\frac{1}{\Delta t}{\int }_{{t}_{n-1}}^{{t}_n} ({K}\nabla (\bar{p}(s)-{\bar{p}}_h^n),\nabla \enspace {\theta }_h{)}_{{\mathrm{\Omega }}_1}\mathrm{d}s=\frac{1}{\Delta t}{\int }_{{t}_{n-1}}^{{t}_n} (q(s)-{q}^n,{\theta }_h{)}_{{\mathrm{\Omega }}_1}\mathrm{d}s-\frac{\alpha }{\lambda }\frac{1}{\Delta t}({\overline{\sigma }}_h^n-{\overline{\sigma }}_h^{n,{\mathcal{l}}_n-1},{\theta }_h{)}_{{\mathrm{\Omega }}_1}. $$The final error equation for flow is derived by adding and subtracting approximations of p and u , and multiplying all terms by Δt. This yields 1 M ( δ ( Π h ( p ¯ n ) - p ¯ h n ) , θ h ) Ω 1 + α ( · ( δ ( R h ( u n ) - u h n ) ) , θ h ) Ω 1 + Δ t μ f ( K ( Π h ( p ¯ n ) - p ¯ h n ) ,   θ h ) Ω 1 = 1 M ( δ ( Π h ( p ¯ n ) - p ¯ n ) , θ h ) Ω 1 + α ( · ( δ ( R h ( u n ) - u n ) ) , θ h ) Ω 1 + Δ t μ f ( K ( Π h ( p ¯ n ) - p ¯ n ) ,   θ h ) Ω 1 + 1 μ f t n - 1 t n ( K ( p ¯ n - p ¯ ( s ) ) ,   θ h ) Ω 1 d s + t n - 1 t n ( q ( s ) - q n , θ h ) Ω 1 d s - α λ ( σ ¯ h n - σ ¯ h n , l n - 1 , θ h ) Ω 1 . Mathematical equation: $$ \frac{1}{M}(\delta ({\mathrm{\Pi }}_h({\bar{p}}^n)-{\bar{p}}_h^n),{\theta }_h{)}_{{\mathrm{\Omega }}_1}+\alpha (\nabla \middot (\delta ({R}_h({{u}}^n)-{{u}}_h^n)),{\theta }_h{)}_{{\mathrm{\Omega }}_1}+\frac{\Delta t}{{\mu }_f}({K}\nabla ({\mathrm{\Pi }}_h({\bar{p}}^n)-{\bar{p}}_h^n),\nabla \enspace {\theta }_h{)}_{{\mathrm{\Omega }}_1}=\frac{1}{M}(\delta ({\mathrm{\Pi }}_h({\bar{p}}^n)-{\bar{p}}^n),{\theta }_h{)}_{{\mathrm{\Omega }}_1}+\alpha (\nabla \middot (\delta ({R}_h({{u}}^n)-{{u}}^n)),{\theta }_h{)}_{{\mathrm{\Omega }}_1}+\frac{\Delta t}{{\mu }_f}({K}\nabla ({\mathrm{\Pi }}_h({\bar{p}}^n)-{\bar{p}}^n),\nabla \enspace {\theta }_h{)}_{{\mathrm{\Omega }}_1}+\frac{1}{{\mu }_f}{\int }_{{t}_{n-1}}^{{t}_n} ({K}\nabla ({\bar{p}}^n-\bar{p}(s)),\nabla \enspace {\theta }_h{)}_{{\mathrm{\Omega }}_1}\mathrm{d}s+{\int }_{{t}_{n-1}}^{{t}_n} (q(s)-{q}^n,{\theta }_h{)}_{{\mathrm{\Omega }}_1}\mathrm{d}s-\frac{\alpha }{\lambda }({\overline{\sigma }}_h^n-{\overline{\sigma }}_h^{n,{\mathcal{l}}_n-1},{\theta }_h{)}_{{\mathrm{\Omega }}_1}. $$(64)

Now, we turn to the displacement and write (20) tested with v h at time t n . We obtain 2 G ( ε ( u n ) , ε ( v h ) ) Ω + λ ( · u n , · v h ) Ω - α ( p n , · v h ) Ω 1 = ( f n , v h ) Ω + ( t N n , v h ) Γ N . Mathematical equation: $$ 2G({\epsilon }({{u}}^n),{\epsilon }({{v}}_h){)}_{\mathrm{\Omega }}+\lambda (\nabla \middot {{u}}^n,\nabla \middot {{v}}_h{)}_{\mathrm{\Omega }}-\alpha ({p}^n,\nabla \middot {{v}}_h{)}_{{\mathrm{\Omega }}_1}=({{f}}^n,{{v}}_h{)}_{\mathrm{\Omega }}+({{t}}_N^n,{{v}}_h{)}_{{\mathrm{\Gamma }}_N}. $$By observing that p n - p h n = p ¯ n - p ¯ h n Mathematical equation: $ {p}^n-{p}_h^n={\bar{p}}^n-{\bar{p}}_h^n$, the difference between this equation and (36) again with l = l n Mathematical equation: $ \mathcal{l}={\mathcal{l}}_n$ reads 2 G ( ε ( u n - u h n ) , ε ( v h ) ) Ω + λ ( · ( u n - u h n ) , · v h ) Ω - α ( p ¯ n - p ¯ h n , · v h ) Ω 1 = 0 . Mathematical equation: $$ 2G({\epsilon }({{u}}^n-{{u}}_h^n),{\epsilon }({{v}}_h){)}_{\mathrm{\Omega }}+\lambda (\nabla \middot ({{u}}^n-{{u}}_h^n),\nabla \middot {{v}}_h{)}_{\mathrm{\Omega }}-\alpha ({\bar{p}}^n-{\bar{p}}_h^n,\nabla \middot {{v}}_h{)}_{{\mathrm{\Omega }}_1}=0. $$It remains to add and subtract approximations of p Mathematical equation: $ p$ and u , to derive the final error displacement equation for all v h V h Mathematical equation: $ {{v}}_h\in {{V}}_h$, 2 G ( ε ( R h ( u n ) - u h n ) , ε ( v h ) ) Ω + λ ( · ( R h ( u n ) - u h n ) , · v h ) Ω - α ( Π h ( p ¯ n ) - p ¯ h n , · v h ) Ω 1 = 2 G ( ε ( R h ( u n ) - u n ) , ε ( v h ) ) Ω + λ ( · ( R h ( u n ) - u n ) , · v h ) Ω - α ( Π h ( p ¯ n ) - p ¯ n , · v h ) Ω 1 . Mathematical equation: $$ \begin{array}{ll}& 2G({\epsilon }({R}_h({{u}}^n)-{{u}}_h^n),{\epsilon }({{v}}_h){)}_{\mathrm{\Omega }}+\lambda (\nabla \middot ({R}_h({{u}}^n)-{{u}}_h^n),\nabla \middot {{v}}_h{)}_{\mathrm{\Omega }}-\alpha ({\mathrm{\Pi }}_h({\bar{p}}^n)-{\bar{p}}_h^n,\nabla \middot {{v}}_h{)}_{{\mathrm{\Omega }}_1}\\ & =2G({\epsilon }({R}_h({{u}}^n)-{{u}}^n),{\epsilon }({{v}}_h){)}_{\mathrm{\Omega }}+\lambda (\nabla \middot ({R}_h({{u}}^n)-{{u}}^n),\nabla \middot {{v}}_h{)}_{\mathrm{\Omega }}-\alpha ({\mathrm{\Pi }}_h({\bar{p}}^n)-{\bar{p}}^n,\nabla \middot {{v}}_h{)}_{{\mathrm{\Omega }}_1}.\end{array} $$(65)Let us set e p n = Π h ( p n ) - p h n ,   e u n = R h ( u n ) - u h n , a p n = Π h ( p n ) - p n , a u n = R h ( u n ) - u n . Mathematical equation: $$ {e}_p^n={\mathrm{\Pi }}_h({p}^n)-{p}_h^n,\enspace \hspace{1em}{e}_{{u}}^n={R}_h({{u}}^n)-{{u}}_h^n,\hspace{1em}{a}_p^n={\mathrm{\Pi }}_h({p}^n)-{p}^n,\hspace{1em}{a}_{{u}}^n={R}_h({{u}}^n)-{{u}}^n. $$(66)The final error equality is obtained by testing (64) with θ h = e ¯ p n = Π h ( p ¯ n ) - p ¯ h n Mathematical equation: $ {\theta }_h={\bar{e}}_p^n={\mathrm{\Pi }}_h({\bar{p}}^n)-{\bar{p}}_h^n$ and (65) by v h = δ ( e u n ) Mathematical equation: $ {{v}}_h=\delta ({e}_{{u}}^n)$, for 1 ≤ n ≤ N, and multiplying both sides by 2 1 M ( | | e ¯ p n | | L 2 ( Ω 1 ) 2 - | | e ¯ p n - 1 | | L 2 ( Ω 1 ) 2 + | | δ ( e p n ) | | L 2 ( Ω 1 ) 2 ) + 2 G ( | | ε ( e u n ) | | L 2 ( Ω ) 2 - | | ε ( e u n - 1 ) | | L 2 ( Ω ) 2 + | | ε ( δ ( e u n ) ) | | L 2 ( Ω ) 2 ) + λ ( | | · ( e u n ) | | L 2 ( Ω ) 2 - | | · ( e u n - 1 ) | | L 2 ( Ω ) 2 + | | · ( δ ( e u n ) ) | | L 2 ( Ω ) 2 ) + 2 Δ t μ f | | K 1 2   e ¯ p n | | L 2 ( Ω 1 ) 2 = 2 [ 1 M ( δ ( a ¯ p n ) , e ¯ p n ) Ω 1 + α ( · ( δ ( a u n ) , e ¯ p n ) ) Ω 1 + 2 G ( ε ( a u n ) , ε ( δ ( e u n ) ) ) Ω + λ ( · ( a u n ) , · δ ( e u n ) ) Ω + Δ t μ f ( K a ¯ p n ,   e ¯ p n ) Ω 1 - α ( a ¯ p n , · ( δ ( e u n ) ) ) Ω 1 - α λ ( σ ¯ h n - σ ¯ h n , l n - 1 , e ¯ p n ) Ω 1 + 1 μ f t n - 1 t n ( K ( p ¯ n - p ¯ ( s ) ) ,   e ¯ p n ) Ω 1 d s + t n - 1 t n ( q ( s ) - q n , e ¯ p n ) Ω 1 d s ] . Mathematical equation: $$ \frac{1}{M}\left({||{\bar{e}}_p^n||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2-{||{\bar{e}}_p^{n-1}||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+{||\delta \left({e}_p^n\right)||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2\right)+2G\left({||{\epsilon }\left({e}_{{u}}^n\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2-{||{\epsilon }\left({e}_{{u}}^{n-1}\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+{||{\epsilon }\left(\delta \left({e}_{{u}}^n\right)\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2\right)+\lambda \left({||\nabla \middot \left({e}_{{u}}^n\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2-{||\nabla \middot \left({e}_{{u}}^{n-1}\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+{||\nabla \middot \left(\delta \left({e}_{{u}}^n\right)\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2\right)+\frac{2\Delta t}{{\mu }_f}{||{{K}}^{\frac{1}{2}}\nabla \enspace {\bar{e}}_p^n||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2=2\left[\frac{1}{M}(\delta ({\bar{a}}_p^n),{\bar{e}}_p^n{)}_{{\mathrm{\Omega }}_1}+\alpha (\nabla \middot (\delta ({a}_{{u}}^n),{\bar{e}}_p^n{))}_{{\mathrm{\Omega }}_1}+2G({\epsilon }({a}_{{u}}^n),{\epsilon }(\delta ({e}_{{u}}^n)){)}_{\mathrm{\Omega }}+\lambda (\nabla \middot ({a}_{{u}}^n),\nabla \middot \delta ({e}_{{u}}^n){)}_{\mathrm{\Omega }}+\frac{\Delta t}{{\mu }_f}({K}\nabla {\bar{a}}_p^n,\nabla \enspace {\bar{e}}_p^n{)}_{{\mathrm{\Omega }}_1}-\alpha ({\bar{a}}_p^n,\nabla \middot (\delta ({e}_{{u}}^n)){)}_{{\mathrm{\Omega }}_1}-\frac{\alpha }{\lambda }({\overline{\sigma }}_h^n-{\overline{\sigma }}_h^{n,{\mathcal{l}}_n-1},{\bar{e}}_p^n{)}_{{\mathrm{\Omega }}_1}+\frac{1}{{\mu }_f}{\int }_{{t}_{n-1}}^{{t}_n} ({K}\nabla ({\bar{p}}^n-\bar{p}(s)),\nabla \enspace {\bar{e}}_p^n{)}_{{\mathrm{\Omega }}_1}\mathrm{d}s+{\int }_{{t}_{n-1}}^{{t}_n} (q(s)-{q}^n,{\bar{e}}_p^n{)}_{{\mathrm{\Omega }}_1}\mathrm{d}s\right]. $$(67)

4.3 Error inequality

To simplify, set E n ( q ) = m ( q ) - q n = 1 Δ t t n - 1 t n q ( s ) d s - q n . Mathematical equation: $$ {E}^n(q)=m(q)-{q}^n=\frac{1}{\Delta t}{\int }_{{t}_{n-1}}^{{t}_n} q(s)\mathrm{d}s-{q}^n. $$(68)By comparing (67) at level m with (50), we see that their left-hand sides have much the same structure. Therefore, to deduce an error inequality from (67), it suffices to suitably group the terms in its right-hand side so as to associate them with corresponding terms in the right-hand side of (50). First, the term 2 α λ ( σ ¯ h m - σ ¯ h m , l m - 1 , e ¯ p m ) Ω 1 Mathematical equation: $$ 2\frac{\alpha }{\lambda }({\overline{\sigma }}_h^m-{\overline{\sigma }}_h^{m,{\mathcal{l}}_m-1},{\bar{e}}_p^m{)}_{{\mathrm{\Omega }}_1} $$can be treated as 2 α λ ( σ ¯ h m - σ ¯ h m , l m - 1 , p ¯ h m ) Ω 1 . Mathematical equation: $$ 2\frac{\alpha }{\lambda }({\overline{\sigma }}_h^m-{\overline{\sigma }}_h^{m,{\mathcal{l}}_m-1},{\bar{p}}_h^m{)}_{{\mathrm{\Omega }}_1}. $$Next, we can write 2 ( 1 M δ ( a ¯ p m ) + α · ( δ ( a u m ) ) + Δ t E m ( q ) , e ¯ p m ) Ω 1 = 2 Δ t ( 1 M 1 Δ t δ ( a ¯ p m ) + α Δ t · ( δ ( a u m ) ) + E m ( q ) , e ¯ p m ) Ω 1 . Mathematical equation: $$ 2{{\left(\frac{1}{M}\delta ({\bar{a}}_p^m)+\alpha \nabla \middot (\delta ({a}_{{u}}^m))+\Delta t{E}^m(q),{\bar{e}}_p^m\right)}_{{\mathrm{\Omega }}_1}=2\Delta t\left(\frac{1}{M}\frac{1}{\Delta t}\delta ({\bar{a}}_p^m)+\frac{\alpha }{\Delta t}\nabla \middot (\delta ({a}_{{u}}^m))+{E}^m(q),{\bar{e}}_p^m\right)}_{{\mathrm{\Omega }}_1}. $$Thus, this term can be treated as 2 Δ t ( q m , p ¯ h m ) Ω 1 . Mathematical equation: $$ 2\Delta t({q}^m,{\bar{p}}_h^m{)}_{{\mathrm{\Omega }}_1}. $$Hence, proceeding as in the proof of Proposition 3.3, assuming again that Δ t 1 2 Mathematical equation: $ \Delta t\le \frac{1}{2}$, and summing over m, from 1 to n, the part of the right-hand side of (67) corresponding to these two terms is bounded by R 1 1 M m = 1 n - 1 Δ t | | e ¯ p m | | L 2 ( Ω 1 ) 2 + 5 M α 2 λ 2 1 Δ t m = 1 n | | σ ¯ h m - σ ¯ h m , l m - 1 | | L 2 ( Ω 1 ) 2 + 5 M m = 1 n Δ t | | 1 M 1 Δ t δ ( a p m ) + α Δ t · ( δ ( a u m ) ) + E m ( q ) | | L 2 ( Ω 1 ) 2 . Mathematical equation: $$ {R}_1\mathbf{\coloneqq} \frac{1}{M}\sum_{m=1}^{n-1} \Delta t{||{\bar{e}}_p^m||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+5M\frac{{\alpha }^2}{{\lambda }^2}\frac{1}{\Delta t}\sum_{m=1}^n {||{\overline{\sigma }}_h^m-{\overline{\sigma }}_h^{m,{\mathcal{l}}_m-1}||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+5M\sum_{m=1}^n \Delta t{||\frac{1}{M}\frac{1}{\Delta t}\delta \left({a}_p^m\right)+\frac{\alpha }{\Delta t}\nabla \middot \left(\delta \left({a}_{{u}}^m\right)\right)+{E}^m(q)||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2. $$(69)The corresponding first group of terms in the left-hand side is L 1 1 M ( | | e ¯ p n | | L 2 ( Ω 1 ) 2 - | | e ¯ p 0 | | L 2 ( Ω 1 ) 2 + m = 1 n - 1 | | δ ( e ¯ p m ) | | L 2 ( Ω 1 ) 2 ) . Mathematical equation: $$ {L}_1\mathbf{\coloneqq} \frac{1}{M}\left({||{\bar{e}}_p^n||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2-{||{\bar{e}}_p^0||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+\sum_{m=1}^{n-1} ||\delta \left({\bar{e}}_p^m\right){||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2\right). $$(70)Next, we consider the terms involving ε ( δ ( e u n ) ) Mathematical equation: $ {\epsilon }(\delta ({e}_{{u}}^n))$ and · δ ( e u n ) Mathematical equation: $ \nabla \middot \delta ({e}_{{u}}^n)$ that must be summed by parts. For the first term, we write 4 G | m = 1 n ( ε ( a u m ) , ε ( δ ( e u m ) ) ) Ω | 4 G [ m = 1 n - 1 ε ( δ ( a u m + 1 ) ) L 2 ( Ω ) ε ( e u m ) L 2 ( Ω ) + ε ( a u n ) L 2 ( Ω ) ε ( e u n ) L 2 ( Ω ) + ε ( a u 1 ) L 2 ( Ω ) ε ( e u 0 ) L 2 ( Ω ) ] . Mathematical equation: $$ \begin{array}{ll}4G\left|\sum_{m=1}^n({\epsilon }({a}_{{u}}^m),{\epsilon }(\delta ({e}_{{u}}^m)){)}_{\mathrm{\Omega }}\right|\le 4G\left[\sum_{m=1}^{n-1} {\Vert {\epsilon }\left(\delta \left({a}_{{u}}^{m+1}\right)\right)\Vert }_{{L}^2\left(\mathrm{\Omega }\right)}{\Vert {\epsilon }\left({e}_{{u}}^m\right)\Vert }_{{L}^2\left(\mathrm{\Omega }\right)}+{\Vert {\epsilon }\left({a}_{{u}}^n\right)\Vert }_{{L}^2\left(\mathrm{\Omega }\right)}{\Vert {\epsilon }\left({e}_{{u}}^n\right)\Vert }_{{L}^2\left(\mathrm{\Omega }\right)}+{\Vert {\epsilon }\left({a}_{{u}}^1\right)\Vert }_{{L}^2\left(\mathrm{\Omega }\right)}{\Vert {\epsilon }\left({e}_{{u}}^0\right)\Vert }_{{L}^2\left(\mathrm{\Omega }\right)}\right].& \\ & \end{array} $$Young’s inequality gives 4 G | m = 1 n ( ε ( a u m ) , ε ( δ ( e u m ) ) ) Ω | 2 G [ 1 2 m = 1 n - 1 Δ t | | ε ( e u m ) | | L 2 ( Ω ) 2 + 2 m = 1 n - 1 Δ t | | 1 Δ t ε ( δ ( a u m + 1 ) ) | | L 2 ( Ω ) 2 + 1 2 | | ε ( e u n ) | | L 2 ( Ω ) 2 + 2 | | ε ( a u n ) | | L 2 ( Ω ) 2 + 1 2 | | ε ( e u 0 ) | | L 2 ( Ω ) 2 + 2 | | ε ( a u 1 ) | | L 2 ( Ω ) 2 ] . Mathematical equation: $$ 4G\left|\sum_{m=1}^n ({\epsilon }({a}_{{u}}^m),{\epsilon }(\delta ({e}_{{u}}^m)){)}_{\mathrm{\Omega }}\right|\le 2G\left[\frac{1}{2}\sum_{m=1}^{n-1} \Delta t{||{\epsilon }({e}_{{u}}^m)||}_{{L}^2(\mathrm{\Omega })}^2+2\sum_{m=1}^{n-1} \Delta t{||\frac{1}{\Delta t}{\epsilon }(\delta ({a}_{{u}}^{m+1}))||}_{{L}^2(\mathrm{\Omega })}^2+\frac{1}{2}{||{\epsilon }({e}_{{u}}^n)||}_{{L}^2(\mathrm{\Omega })}^2+2{||{\epsilon }({a}_{{u}}^n)||}_{{L}^2(\mathrm{\Omega })}^2+\frac{1}{2}{||{\epsilon }({e}_{{u}}^0)||}_{{L}^2(\mathrm{\Omega })}^2+2{||{\epsilon }({a}_{{u}}^1)||}_{{L}^2(\mathrm{\Omega })}^2\right]. $$The contribution of this term to the right-hand side is R 2 G [ m = 1 n - 1 Δ t ε ( e u m ) L 2 ( Ω ) 2 + 4 m = 1 n - 1 Δ t 1 Δ t ε ( δ ( a u m + 1 ) ) L 2 ( Ω ) 2 + 4 ε ( a u n ) L 2 ( Ω ) 2 + 2 ε ( e u 0 ) L 2 ( Ω ) 2 + 2 ε ( a u 1 ) L 2 ( Ω ) 2 ] Mathematical equation: $$ {R}_2\mathbf{\coloneqq} G\left[\sum_{m=1}^{n-1} \Delta t{\Vert {\epsilon }\left({e}_{{u}}^m\right)\Vert }_{{L}^2\left(\mathrm{\Omega }\right)}^2+4\sum_{m=1}^{n-1} \Delta t{\Vert \frac{1}{\Delta t}{\epsilon }\left(\delta \left({a}_{{u}}^{m+1}\right)\right)\Vert }_{{L}^2\left(\mathrm{\Omega }\right)}^2+4{\Vert {\epsilon }\left({a}_{{u}}^n\right)\Vert }_{{L}^2\left(\mathrm{\Omega }\right)}^2+2{\Vert {\epsilon }\left({e}_{{u}}^0\right)\Vert }_{{L}^2\left(\mathrm{\Omega }\right)}^2+2{\Vert {\epsilon }\left({a}_{{u}}^1\right)\Vert }_{{L}^2\left(\mathrm{\Omega }\right)}^2\right] $$(71)and the corresponding group of terms that remain in the left-hand side is L 2 G [ | | ε ( e u n ) | | L 2 ( Ω ) 2 - 2 | | ε ( e u 0 ) | | L 2 ( Ω ) 2 + 2 m = 1 n | | ε ( δ ( e u m ) ) | | L 2 ( Ω ) 2 ] . Mathematical equation: $$ {L}_2\mathbf{\coloneqq} G\left[{||{\epsilon }\left({e}_{{u}}^n\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2-2{||{\epsilon }\left({e}_{{u}}^0\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+2\sum_{m=1}^n {||{\epsilon }\left(\delta \left({e}_{{u}}^m\right)\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2\right]. $$(72)To simplify the treatment of the terms involving · δ ( e u n ) Mathematical equation: $ \nabla \middot \delta ({e}_{{u}}^n)$, it is convenient to extend α Mathematical equation: $ \alpha $ by zero outside Ω1. With this convention, we write 2 λ ( · ( a u n ) , · δ ( e u n ) ) Ω - 2 α ( a ¯ p n , · ( δ ( e u n ) ) ) Ω 1 = 2 ( λ · ( a u n ) - α a ¯ p n , · ( δ ( e u n ) ) ) Ω . Mathematical equation: $$ 2\lambda (\nabla \middot ({a}_{{u}}^n),\nabla \middot \delta ({e}_{{u}}^n){)}_{\mathrm{\Omega }}-2\alpha ({\bar{a}}_p^n,\nabla \middot (\delta ({e}_{{u}}^n)){)}_{{\mathrm{\Omega }}_1}=2(\lambda \nabla \middot ({a}_{{u}}^n)-\alpha {\bar{a}}_p^n,\nabla \middot (\delta ({e}_{{u}}^n)){)}_{\mathrm{\Omega }}. $$Then we deduce by the above argument 2 | m = 1 n ( λ · ( a u n ) - α a ¯ p n , · ( δ ( e u n ) ) ) Ω | λ 2 m = 1 n - 1 Δ t | | · ( e u m ) | | L 2 ( Ω ) 2 + 2 λ m = 1 n - 1 Δ t | | 1 Δ t ( λ · ( δ ( a u m + 1 ) ) - α δ ( a ¯ p m + 1 ) ) | | L 2 ( Ω ) 2 + λ 2 | | · ( e u n ) | | L 2 ( Ω ) 2 + 2 λ | | λ · ( a u n ) - α a ¯ p n | | L 2 ( Ω ) 2 + λ 2 | | · ( e u 0 ) | | L 2 ( Ω ) 2 + 2 λ | | λ · ( a u 1 ) - α a ¯ p 1 | | L 2 ( Ω ) 2 . Mathematical equation: $$ 2\left|\sum_{m=1}^n (\lambda \nabla \middot ({a}_{{u}}^n)-\alpha {\bar{a}}_p^n,\nabla \middot (\delta ({e}_{{u}}^n)){)}_{\mathrm{\Omega }}\right|\le \frac{\lambda }{2}\sum_{m=1}^{n-1} \Delta t{||\nabla \middot ({e}_{{u}}^m)||}_{{L}^2(\mathrm{\Omega })}^2+\frac{2}{\lambda }\sum_{m=1}^{n-1} \Delta t{||\frac{1}{\Delta t}(\lambda \nabla \middot (\delta ({a}_{{u}}^{m+1}))-{\alpha \delta }({\bar{a}}_p^{m+1}))||}_{{L}^2(\mathrm{\Omega })}^2+\frac{\lambda }{2}{||\nabla \middot ({e}_{{u}}^n)||}_{{L}^2(\mathrm{\Omega })}^2+\frac{2}{\lambda }{||\lambda \nabla \middot ({a}_{{u}}^n)-\alpha {\bar{a}}_p^n||}_{{L}^2(\mathrm{\Omega })}^2+\frac{\lambda }{2}{||\nabla \middot ({e}_{{u}}^0)||}_{{L}^2(\mathrm{\Omega })}^2+\frac{2}{\lambda }{||\lambda \nabla \middot ({a}_{{u}}^1)-\alpha {\bar{a}}_p^1||}_{{L}^2(\mathrm{\Omega })}^2. $$The contribution of this term to the right-hand side is R 3 λ 2 m = 1 n - 1 Δ t | | · ( e u m ) | | L 2 ( Ω ) 2 + 2 λ m = 1 n - 1 Δ t | | 1 Δ t ( λ · ( δ ( a u m + 1 ) ) - α δ ( a ¯ p m + 1 ) ) | | L 2 ( Ω ) 2 + 2 λ | | λ · ( a u n ) - α a ¯ p n | | L 2 ( Ω ) 2 + λ 2 | | · ( e u 0 ) | | L 2 ( Ω ) 2 + 2 λ | | λ · ( a u 1 ) - α a ¯ p 1 | | L 2 ( Ω ) 2 , Mathematical equation: $$ {R}_3\mathbf{\coloneqq} \frac{\lambda }{2}\sum_{m=1}^{n-1} \Delta t{||\nabla \middot \left({e}_{{u}}^m\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+\frac{2}{\lambda }\sum_{m=1}^{n-1} \Delta t{||\frac{1}{\Delta t}\left(\lambda \nabla \middot \left(\delta \left({a}_{{u}}^{m+1}\right)\right)-{\alpha \delta }({\bar{a}}_p^{m+1})\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+\frac{2}{\lambda }{||\lambda \nabla \middot \left({a}_{{u}}^n\right)-\alpha {\bar{a}}_p^n||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+\frac{\lambda }{2}{||\nabla \middot \left({e}_{{u}}^0\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+\frac{2}{\lambda }{||\lambda \nabla \middot \left({a}_{{u}}^1\right)-\alpha {\bar{a}}_p^1||}_{{L}^2\left(\mathrm{\Omega }\right)}^2, $$(73)and the corresponding group of terms that remain in the left-hand side is L 3 λ 2 [ | | · ( e u n ) | | L 2 ( Ω ) 2 - 2 | | · ( e u 0 ) | | L 2 ( Ω ) 2 + 2 m = 1 n | | · ( δ ( e u m ) ) | | L 2 ( Ω ) 2 ] . Mathematical equation: $$ {L}_3\mathbf{\coloneqq} \frac{\lambda }{2}\left[{||\nabla \middot \left({e}_{{u}}^n\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2-2{||\nabla \middot \left({e}_{{u}}^0\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+2\sum_{m=1}^n {||\nabla \middot \left(\delta \left({e}_{{u}}^m\right)\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2\right]. $$(74)There remain the two terms involving the gradient of e ¯ p n Mathematical equation: $ {\bar{e}}_p^n$; with the notation (68), they can be written as 2 μ f [ Δ t ( K a ¯ p n ,   e ¯ p n ) Ω 1 + t n - 1 t n ( K ( p ¯ n - p ¯ ( s ) ) ,   e ¯ p n ) Ω 1 d s ] = 2 Δ t μ f ( K ( a ¯ p n - E n ( p ¯ ) ) ,   e ¯ p n ) Ω 1 . Mathematical equation: $$ \frac{2}{{\mu }_f}[\Delta t({K}\nabla {\bar{a}}_p^n,\nabla \enspace {\bar{e}}_p^n{)}_{{\mathrm{\Omega }}_1}+{\int }_{{t}_{n-1}}^{{t}_n} ({K}\nabla ({\bar{p}}^n-\bar{p}(s)),\nabla \enspace {\bar{e}}_p^n{)}_{{\mathrm{\Omega }}_1}\mathrm{d}s]=\frac{2\Delta t}{{\mu }_f}({K}\nabla ({\bar{a}}_p^n-{E}^n(\bar{p})),\nabla \enspace {\bar{e}}_p^n{)}_{{\mathrm{\Omega }}_1}. $$By Young’s inequality, when summed over m, this term has the bound for any γ > 0, 2 Δ t μ f m = 1 n | ( K ( a ¯ p m - E m ( p ¯ ) ) ,   e ¯ p m ) Ω 1 | 1 μ f [ γ m = 1 n Δ t | | K 1 2 e ¯ p m | | L 2 ( Ω 1 ) 2 + 1 γ m = 1 n Δ t | | K 1 2 ( a ¯ p m - E m ( p ¯ ) ) | | L 2 ( Ω 1 ) 2 ] . Mathematical equation: $$ \frac{2\Delta t}{{\mu }_f}\sum_{m=1}^n |({K}\nabla ({\bar{a}}_p^m-{E}^m(\bar{p})),\nabla \enspace {\bar{e}}_p^m{)}_{{\mathrm{\Omega }}_1}|\le \frac{1}{{\mu }_f}\left[\gamma \sum_{m=1}^n \Delta t{||{{K}}^{\frac{1}{2}}\nabla {\bar{e}}_p^m||}_{{L}^2({\mathrm{\Omega }}_1)}^2+\frac{1}{\gamma }\sum_{m=1}^n \Delta t{||{{K}}^{\frac{1}{2}}\nabla ({\bar{a}}_p^m-{E}^m(\bar{p}))||}_{{L}^2({\mathrm{\Omega }}_1)}^2\right]. $$Thus the contribution of this term to the right-hand side is R 4 1 γ 1 μ f m = 1 n Δ t | | K 1 2 ( a ¯ p m - E m ( p ¯ ) ) | | L 2 ( Ω 1 ) 2 , Mathematical equation: $$ {R}_4\mathbf{\coloneqq} \frac{1}{\gamma }\frac{1}{{\mu }_f}\sum_{m=1}^n \Delta t{||{{K}}^{\frac{1}{2}}\nabla \left({\bar{a}}_p^m-{E}^m\left(\bar{p}\right)\right)||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2, $$(75)and the corresponding term that remain in the left-hand side is L 4 ( 2 - γ ) 1 μ f m = 1 n Δ t | | K 1 2 e ¯ p m | | L 2 ( Ω 1 ) 2 . Mathematical equation: $$ {L}_4\mathbf{\coloneqq} \left(2-\gamma \right)\frac{1}{{\mu }_f}\sum_{m=1}^n \Delta t{||{{K}}^{\frac{1}{2}}\nabla {\bar{e}}_p^m||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2. $$(76)

By collecting the terms L i in the left-hand side and R i in the right-hand side, for 1 ≤ i ≤ 4, we deduce the following error inequality (compare with Proposition 3.3):

Proposition 4.2.

Let q belong to C 0 ( 0 , T ; L 2 ( Ω 1 ) ) Mathematical equation: $ {\mathcal{C}}^0(0,T;{L}^2({\Omega }_1))$, u Mathematical equation: $ {u}$ to C 0 ( 0 , T ; V ) Mathematical equation: $ {\mathcal{C}}^0(0,T;{V})$ , and p Mathematical equation: $ p$ to C 0 ( 0 , T ; H 1 ( Ω 1 ) ) Mathematical equation: $ {\mathcal{C}}^0(0,T;{H}^1({\Omega }_1))$ . Assume that Δ t 1 2 Mathematical equation: $ {\Delta t}\le \frac{1}{2}$ and that α Mathematical equation: $ \alpha $ is extended by zero outside Ω 1 Mathematical equation: $ {\Omega }_1$ . With the notation (60), (66), and (68) , the following bound holds for all n, 1 ≤ n ≤ N, and any γ ∈ ]0, 2[, 1 M ( | | e ¯ p n | | L 2 ( Ω 1 ) 2 + m = 1 n - 1 | | δ ( e ¯ p m ) | | L 2 ( Ω 1 ) 2 ) + G ( | | ε ( e u n ) | | L 2 ( Ω ) 2 + 2 m = 1 n | | ε ( δ ( e u m ) ) | | L 2 ( Ω ) 2 ) + λ 2 ( | | · ( e u n ) | | L 2 ( Ω ) 2 + 2 m = 1 n | | · ( δ ( e u m ) ) | | L 2 ( Ω ) 2 ) + 2 - γ μ f m = 1 n Δ t | | K 1 2   e ¯ p m | | L 2 ( Ω 1 ) 2 1 M m = 1 n - 1 Δ t | | e ¯ p m | | L 2 ( Ω 1 ) 2 + G m = 1 n - 1 Δ t | | ε ( e u m ) | | L 2 ( Ω ) 2 + λ 2 m = 1 n - 1 Δ t | | · ( e u m ) | | L 2 ( Ω ) 2 + 5 M α 2 λ 2 1 Δ t m = 1 n | | σ ¯ h m - σ ¯ h m , l m - 1 | | L 2 ( Ω 1 ) 2 + E h 0 + A h n , Mathematical equation: $$ \frac{1}{M}\left({||{\bar{e}}_p^n||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+\sum_{m=1}^{n-1} {||\delta ({\bar{e}}_p^m)||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2)+G({||{\epsilon }({e}_{{u}}^n)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+2\sum_{m=1}^n {||{\epsilon }(\delta ({e}_{{u}}^m))||}_{{L}^2\left(\mathrm{\Omega }\right)}^2\right)+\frac{\lambda }{2}\left({||\nabla \middot \left({e}_{{u}}^n\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+2\sum_{m=1}^n {||\nabla \middot \left(\delta \left({e}_{{u}}^m\right)\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2\right)+\frac{2-\gamma }{{\mu }_f}\sum_{m=1}^n \Delta t{||{{K}}^{\frac{1}{2}}\nabla \enspace {\bar{e}}_p^m||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2\le \frac{1}{M}\sum_{m=1}^{n-1} \Delta t{||{\bar{e}}_p^m||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+G\sum_{m=1}^{n-1} \Delta t{||{\epsilon }\left({e}_{{u}}^m\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+\frac{\lambda }{2}\sum_{m=1}^{n-1} \Delta t{||\nabla \middot \left({e}_{{u}}^m\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+5M\frac{{\alpha }^2}{{\lambda }^2}\frac{1}{\Delta t}\sum_{m=1}^n {||{\overline{\sigma }}_h^m-{\overline{\sigma }}_h^{m,{\mathcal{l}}_m-1}||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+{\mathcal{E}}_h^0+{\mathcal{A}}_h^n, $$(77) where E h 0 Mathematical equation: $ {\mathcal{E}}_h^0$ and A h n Mathematical equation: $ {\mathcal{A}}_h^n$ are respectively contributions of the initial errors and interpolation errors in space and time, E h 0 = 1 M | | e ¯ p 0 | | L 2 ( Ω 1 ) 2 + 4 G | | ε ( e u 0 ) | | L 2 ( Ω ) 2 + 3 2 λ | | · e u 0 | | L 2 ( Ω ) 2 , Mathematical equation: $$ {\mathcal{E}}_h^0=\frac{1}{M}{||{\bar{e}}_p^0||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+4G{||{\epsilon }\left({e}_{{u}}^0\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+\frac{3}{2}\lambda {||\nabla \middot {e}_{{u}}^0||}_{{L}^2\left(\mathrm{\Omega }\right)}^2, $$(78) A h n = 5 M m = 1 n Δ t | | 1 M 1 Δ   t δ ( a ¯ p m ) + α Δ   t · ( δ a u m ) + E m ( q ) | | L 2 ( Ω 1 ) 2 + 4 G m = 1 n - 1 Δ   t | | 1 Δ   t ε ( δ ( a u m + 1 ) ) | | L 2 ( Ω ) 2 + 2 λ m = 1 n - 1 Δ t | | λ Δ t · ( δ ( a u m + 1 ) ) - α Δ t δ ( a ¯ p m + 1 ) | | L 2 ( Ω ) 2 + 1 γ 1 μ f m = 1 n Δ t | | K 1 2 ( a ¯ p m - E m ( p ¯ ) ) | | L 2 ( Ω 1 ) 2 + 4 G | | ε ( a u n ) | | L 2 ( Ω ) 2 + 2 λ | | λ · ( a u n ) - α a ¯ p n | | L 2 ( Ω ) 2 + 4 G | | ε ( a u 1 ) | | L 2 ( Ω ) 2 + 2 λ | | λ · ( a u 1 ) - α a ¯ p 1 | | L 2 ( Ω ) 2 . Mathematical equation: $$ {\mathcal{A}}_h^n=5M\sum_{m=1}^n \Delta t{||\frac{1}{M}\frac{1}{\Delta \enspace t}\delta ({\bar{a}}_p^m)+\frac{\alpha }{\Delta \enspace t}\nabla \middot (\delta {a}_{{u}}^m)+{E}^m(q)||}_{{L}^2({\mathrm{\Omega }}_1)}^2+4G\sum_{m=1}^{n-1} \Delta \enspace t{||\frac{1}{\Delta \enspace t}{\epsilon }(\delta ({a}_{{u}}^{m+1}))||}_{{L}^2(\mathrm{\Omega })}^2+\frac{2}{\lambda }\sum_{m=1}^{n-1} \Delta t{||\frac{\lambda }{\Delta t}\nabla \middot (\delta ({a}_{{u}}^{m+1}))-\frac{\alpha }{\Delta t}\delta ({\bar{a}}_p^{m+1})||}_{{L}^2(\mathrm{\Omega })}^2+\frac{1}{\gamma }\frac{1}{{\mu }_f}\sum_{m=1}^n \Delta t{||{{K}}^{\frac{1}{2}}\nabla ({\bar{a}}_p^m-{E}^m(\bar{p}))||}_{{L}^2({\mathrm{\Omega }}_1)}^2+4G{||{\epsilon }({a}_{{u}}^n)||}_{{L}^2(\mathrm{\Omega })}^2+\frac{2}{\lambda }{||\lambda \nabla \middot ({a}_{{u}}^n)-\alpha {\bar{a}}_p^n||}_{{L}^2(\mathrm{\Omega })}^2+4G{||{\epsilon }({a}_{{u}}^1)||}_{{L}^2(\mathrm{\Omega })}^2+\frac{2}{\lambda }{||\lambda \nabla \middot ({a}_{{u}}^1)-\alpha {\bar{a}}_p^1||}_{{L}^2(\mathrm{\Omega })}^2. $$(79)

4.4 Error estimate

With the notation (66) and (68), (63) reads 5 M α 2 λ 2 1 Δ t m = 1 n | | σ ¯ h m - σ ¯ h m , l m - 1 | | L 2 ( Ω 1 ) 2 5 M α 2 λ 2 1 Δ t m = 1 n 1 ( β   λ ) 2 l m - 2 [ λ G ( C 2 | | f m - f m - 1 | | L 2 ( Ω ) 2 + C ̃ 2 | | t N m - t N m - 1 | | L 2 ( Γ N ) 2 ) + 4 ( Δ t μ f β ( | | K 1 2 ( e ¯ p m - 1 ) | | L 2 ( Ω 1 ) 2 + 2 | | K 1 2   a ¯ p m - 1 | | L 2 ( Ω 1 ) 2 + 2 | | K 1 2   E m - 1 ( p ¯ ) | | L 2 ( Ω 1 ) 2 ) + 2 ( Δ t ) 2 α 2 β 2 | | E m ( q ) | | L 2 ( Ω 1 ) 2 + 2 Δ t α 2 β 2 t ( 1 M p + α · u ) L 2 ( Ω 1 × ] t m - 1 , t m [ ) 2 ) ] . Mathematical equation: $$ 5M\frac{{\alpha }^2}{{\lambda }^2}\frac{1}{\Delta t}\sum_{m=1}^n {||{\overline{\sigma }}_h^m-{\overline{\sigma }}_h^{m,{\mathcal{l}}_m-1}||}_{{L}^2({\mathrm{\Omega }}_1)}^2\le 5M\frac{{\alpha }^2}{{\lambda }^2}\frac{1}{\Delta t}\sum_{m=1}^n \frac{1}{(\beta \enspace \lambda {)}^{2{\mathcal{l}}_m-2}}\left[\frac{\lambda }{G}\left({C}^2{||{{f}}^m-{{f}}^{m-1}||}_{{L}^2(\mathrm{\Omega })}^2+{\mathop{C}\limits^\tilde}^2{||{{t}}_N^m-{{t}}_N^{m-1}||}_{{L}^2({\mathrm{\Gamma }}_N)}^2\right)+4\left(\frac{\Delta t}{{\mu }_f\beta }\left({||{{K}}^{\frac{1}{2}}\nabla ({\bar{e}}_p^{m-1})||}_{{L}^2({\mathrm{\Omega }}_1)}^2+2{||{{K}}^{\frac{1}{2}}\nabla \enspace {\bar{a}}_p^{m-1}||}_{{L}^2({\mathrm{\Omega }}_1)}^2+2{||{{K}}^{\frac{1}{2}}\nabla \enspace {E}^{m-1}(\bar{p})||}_{{L}^2({\mathrm{\Omega }}_1)}^2\right)+2\frac{(\Delta t{)}^2}{{\alpha }^2{\beta }^2}{||{E}^m(q)||}_{{L}^2({\mathrm{\Omega }}_1)}^2+2\frac{\Delta t}{{\alpha }^2{\beta }^2}{\Vert {\mathrm{\partial }}_t\left(\frac{1}{M}p+\alpha \nabla \middot {u}\right)\Vert }_{{L}^2({\mathrm{\Omega }}_1\times ]{t}_{m-1},{t}_m[)}^2\right)\right]. $$(80)

The factor of the term involving K 1 2 ( e ¯ p m - 1 ) Mathematical equation: $ {{K}}^{\frac{1}{2}}\nabla ({\bar{e}}_p^{m-1})$ is 20 M α 2 λ 2 1 μ f β 1 ( β   λ ) 2 l m - 2 , Mathematical equation: $$ 20M\frac{{\alpha }^2}{{\lambda }^2}\frac{1}{{\mu }_f\beta }\frac{1}{(\beta \enspace \lambda {)}^{2{\mathcal{l}}_m-2}}, $$and this factor must be controlled in the left-hand side of (77) by 1 μ f ( 2 - γ ) Δ t , Mathematical equation: $$ \frac{1}{{\mu }_f}(2-\gamma )\Delta t, $$with a parameter γ ∈ ]0, 2[to be chosen. If we choose for instance γ = 1 2 Mathematical equation: $ \gamma =\frac{1}{2}$, a sufficient condition for this control is 20 M α 2 λ 2 1 μ f β 1 ( β   λ ) 2 l m - 2 3 2 1 μ f Δ t , Mathematical equation: $$ 20M\frac{{\alpha }^2}{{\lambda }^2}\frac{1}{{\mu }_f\beta }\frac{1}{(\beta \enspace \lambda {)}^{2{\mathcal{l}}_m-2}}\le \frac{3}{2}\frac{1}{{\mu }_f}\Delta t, $$which resembles formula (57) that guarantees stability. However, in contrast to the situation of Theorem 3.1, this assumption does not guarantee a satisfactory error bound. Indeed, with this assumption, the first term in the right-hand side of (80) is bounded by 3 8 β λ C 2 G m = 1 n | | f m - f m - 1 | | L 2 ( Ω ) 2 . Mathematical equation: $$ \frac{3}{8}\beta \frac{\lambda {C}^2}{G}\sum_{m=1}^n {||{{f}}^m-{{f}}^{m-1}||}_{{L}^2(\mathrm{\Omega })}^2. $$

Considering that | | f m - f m - 1 | | L 2 ( Ω ) 2 Δ t   | | t f | | L 2 ( Ω × ] t m - 1 , t m [ ) 2 , Mathematical equation: $$ {||{{f}}^m-{{f}}^{m-1}||}_{{L}^2(\mathrm{\Omega })}^2\le \Delta t\enspace {||{\mathrm{\partial }}_t{f}||}_{{L}^2(\mathrm{\Omega }\times ]{t}_{m-1},{t}_m[)}^2, $$this assumption implies 3 8 β λ C 2 G m = 1 n | | f m - f m - 1 | | L 2 ( Ω ) 2 3 8 β λ C 2 G Δ t   | | t f | | L 2 ( Ω × ] 0 , t n [ ) 2 , Mathematical equation: $$ \frac{3}{8}\beta \frac{\lambda {C}^2}{G}\sum_{m=1}^n {||{{f}}^m-{{f}}^{m-1}||}_{{L}^2(\mathrm{\Omega })}^2\le \frac{3}{8}\beta \frac{\lambda {C}^2}{G}\Delta t\enspace {||{\mathrm{\partial }}_t{f}||}_{{L}^2(\mathrm{\Omega }\times ]0,{t}_n[)}^2, $$which is not sufficient to guarantee a first order in time that requires a factor (Δt)2. The second and last terms of (80) are plagued by the same shortcoming. Note that they reflect the inconsistency of the first iteration of the algorithm at each time step.

These considerations suggest to replace the above variant of (57) by the stronger condition, m , 1 m n ,   l m L ,   where   1 ( β   λ ) L min ( ( 3 40 1 M Δ t α 2 β ) 1 2 , Δ t ) . Mathematical equation: $$ \forall m,1\le m\le n,\enspace {\mathcal{l}}_m\ge L,\enspace \hspace{1em}\mathrm{where}\enspace \frac{1}{(\beta \enspace \lambda {)}^L}\le \mathrm{min}\left({\left(\frac{3}{40}\frac{1}{M}\frac{\Delta t}{{\alpha }^2\beta }\right)}^{\frac{1}{2}},\Delta t\right). $$(81)

With this assumption, the following error estimate holds:

Theorem 4.1.

In addition to the assumptions and notation of Proposition 4.2 , we suppose that the data satisfy ∂ t f  ∈ L2(Ω × ]0, T[) d , t t N  ∈ L 2 (Γ N × ]0, T[) d , and ∂ t q ∈ L 2 1 × ]0, T[), that the solution satisfies ∂ t p ∈ L2(0, T; H11)) and ∂ t u  ∈ L2(0, T; H1(Ω)d), and that the assumption (81) on the number of iterations holds. Then, we have the following error estimate for all n, 1 ≤ n ≤ N, 1 M ( | | e ¯ p n | | L 2 ( Ω 1 ) 2 + m = 1 n - 1 | | δ ( e ¯ p m ) | | L 2 ( Ω 1 ) 2 ) + G ( | | ε ( e u n ) | | L 2 ( Ω ) 2 + 2 m = 1 n | | ε ( δ ( e u m ) ) | | L 2 ( Ω ) 2 ) + λ 2 ( | | · ( e u n ) | | L 2 ( Ω ) 2 + 2 m = 1 n | | · ( δ ( e u m ) ) | | L 2 ( Ω ) 2 ) ( E time n + E space n + E initial ) exp ( t n ) , Mathematical equation: $$ \frac{1}{M}\left({||{\bar{e}}_p^n||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+\sum_{m=1}^{n-1} {||\delta ({\bar{e}}_p^m)||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2\right)+G\left({||{\epsilon }({e}_{{u}}^n)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+2\sum_{m=1}^n {||{\epsilon }(\delta ({e}_{{u}}^m))||}_{{L}^2\left(\mathrm{\Omega }\right)}^2\right)+\frac{\lambda }{2}\left({||\nabla \middot \left({e}_{{u}}^n\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+2\sum_{m=1}^n {||\nabla \middot \left(\delta \left({e}_{{u}}^m\right)\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2\right)\le ({\mathcal{E}}_{\mathrm{time}}^n+{\mathcal{E}}_{\mathrm{space}}^n+{\mathcal{E}}_{\mathrm{initial}})\mathrm{exp}({t}_n), $$(82) where E initial = 1 M | | e ¯ p 0 | | L 2 ( Ω 1 ) 2 + 3 Δ t 2 μ f | | K 1 2   e ¯ p 0 | | L 2 ( Ω 1 ) 2 + 4 G | | ε ( e u 0 ) | | L 2 ( Ω ) 2 + 3 2 λ | | · e u 0 | | L 2 ( Ω ) 2 , Mathematical equation: $$ {\mathcal{E}}_{\mathrm{initial}}=\frac{1}{M}{||{\bar{e}}_p^0||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+\frac{3\Delta t}{2{\mu }_f}{||{{K}}^{\frac{1}{2}}\nabla \enspace {\bar{e}}_p^0||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+4G{||{\epsilon }\left({e}_{{u}}^0\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+\frac{3}{2}\lambda {||\nabla \middot {e}_{{u}}^0||}_{{L}^2\left(\mathrm{\Omega }\right)}^2, $$(83) E time n = ( Δ t ) 2 [ 5 M { α 2 β 2 λ G ( C 2 | | t f | | L 2 ( Ω × ] 0 , t n [ ) 2 + C ̃ 2 | | t t N | | L 2 ( Γ N × ] 0 , t n [ ) 2 ) + 8 t ( 1 M p + α · u ) L 2 ( Ω 1 × ] 0 , t n [ ) 2 } + 7 3 μ f | | K 1 2   t p | | L 2 ( Ω 1 × ] 0 , t n [ ) 2 + ( Δ t α 2 β + 5 M ) | | t q | | L 2 ( Ω 1 × ] 0 , t n [ ) 2 ] , Mathematical equation: $$ {\mathcal{E}}_{\mathrm{time}}^n=(\Delta t{)}^2\left[5M\left\{\frac{{\alpha }^2{\beta }^2\lambda }{G}({C}^2{||{\mathrm{\partial }}_t{f}||}_{{L}^2\left(\mathrm{\Omega }\times \right]0,{t}_n[)}^2+{\mathop{C}\limits^\tilde}^2{||{\mathrm{\partial }}_t{{t}}_N||}_{{L}^2\left({\mathrm{\Gamma }}_N\times \right]0,{t}_n[)}^2)+8{\Vert {\mathrm{\partial }}_t\left(\frac{1}{M}p+\alpha \nabla \middot {u}\right)\Vert }_{{L}^2\left({\mathrm{\Omega }}_1\times \right]0,{t}_n[)}^2\right\}+\frac{7}{3{\mu }_f}{||{{K}}^{\frac{1}{2}}\nabla \enspace {\mathrm{\partial }}_tp||}_{{L}^2\left({\mathrm{\Omega }}_1\times \right]0,{t}_n[)}^2+\left(\frac{\Delta t}{{\alpha }^2\beta }+5M\right){||{\mathrm{\partial }}_tq||}_{{L}^2\left({\mathrm{\Omega }}_1\times \right]0,{t}_n[)}^2\right], $$(84) E space n = ( 15 1 M + 4 α 2 λ ) | | t a ¯ p | | L 2 ( Ω 1 × ] 0 , t n - 1 [ ) 2 + ( 15 α 2 M + 4 λ ) | | · t ( a u ) | | L 2 ( Ω 1 × ] 0 , t n - 1 [ ) 2 + 4 G | | ε ( t ( a u ) ) | | L 2 ( Ω × ] 0 , t n [ ) 2 + 7 μ f m = 1 n Δ t | | K 1 2   a ¯ p m - 1 | | L 2 ( Ω 1 ) 2 + 4 G | | ε ( a u n ) | | L 2 ( Ω ) 2 + 4 λ | | · a u n | | L 2 ( Ω ) 2 + 4 α 2 λ | | a ¯ p n | | L 2 ( Ω 1 ) 2 + 4 G | | ε ( a u 1 ) | | L 2 ( Ω ) 2 + 4 λ | | · a u 1 | | L 2 ( Ω ) 2 + 4 α 2 λ | | a ¯ p 1 | | L 2 ( Ω 1 ) 2 . Mathematical equation: $$ {\mathcal{E}}_{\mathrm{space}}^n=\left(15\frac{1}{M}+4\frac{{\alpha }^2}{\lambda }\right){||{\mathrm{\partial }}_t{\bar{a}}_p||}_{{L}^2\left({\mathrm{\Omega }}_1\times \right]0,{t}_{n-1}[)}^2+\left(15{\alpha }^2M+4\lambda \right){||\nabla \middot {\mathrm{\partial }}_t\left({a}_{{u}}\right)||}_{{L}^2\left({\mathrm{\Omega }}_1\times \right]0,{t}_{n-1}[)}^2+4G{||{\epsilon }\left({\mathrm{\partial }}_t\left({a}_{{u}}\right)\right)||}_{{L}^2\left(\mathrm{\Omega }\times \right]0,{t}_n[)}^2+\frac{7}{{\mu }_f}\sum_{m=1}^n \Delta t{||{{K}}^{\frac{1}{2}}\nabla \enspace {\bar{a}}_p^{m-1}||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+4G{||{\epsilon }\left({a}_{{u}}^n\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+4\lambda {||\nabla \middot {a}_{{u}}^n||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+\frac{4{\alpha }^2}{\lambda }{||{\bar{a}}_p^n||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+4G{||{\epsilon }\left({a}_{{u}}^1\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+4\lambda {||\nabla \middot {a}_{{u}}^1||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+\frac{4{\alpha }^2}{\lambda }{||{\bar{a}}_p^1||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2. $$(85)

Proof. By applying the second part of (81) to the first, second, and last terms of the right-hand side of (80) and the first part to the remaining terms, we derive 5 M α 2 λ 2 1 Δ t m = 1 n | | σ ¯ h m - σ ¯ h m , l m - 1 | | L 2 ( Ω 1 ) 2 5 M α 2 β 2 ( Δ t ) 2 λ G ( C 2 | | t f | | L 2 ( Ω × ] 0 , t n [ ) 2 + C ̃ 2 | | t t N | | L 2 ( Γ N × ] 0 , t n [ ) 2 ) + 3 2 1 μ f m = 1 n Δ t ( | | K 1 2   e ¯ p m - 1 | | L 2 ( Ω 1 ) 2 + 2 | | K 1 2   a ¯ p m - 1 | | L 2 ( Ω 1 ) 2 + 2 | | K 1 2   E m - 1 ( p ¯ ) | | L 2 ( Ω 1 ) 2 ) + 3 α 2 β ( Δ t ) 2 m = 1 n | | E m ( q ) | | L 2 ( Ω 1 ) 2 + 40 M ( Δ t ) 2 t ( 1 M p + α · u ) L 2 ( Ω 1 × ] 0 , t n [ ) 2 . Mathematical equation: $$ 5M\frac{{\alpha }^2}{{\lambda }^2}\frac{1}{\Delta t}\sum_{m=1}^n {||{\overline{\sigma }}_h^m-{\overline{\sigma }}_h^{m,{\mathcal{l}}_m-1}||}_{{L}^2({\mathrm{\Omega }}_1)}^2\le 5M{\alpha }^2{\beta }^2(\Delta t{)}^2\frac{\lambda }{G}({C}^2{||{\mathrm{\partial }}_t{f}||}_{{L}^2(\mathrm{\Omega }\times ]0,{t}_n[)}^2+{\mathop{C}\limits^\tilde}^2{||{\mathrm{\partial }}_t{{t}}_N||}_{{L}^2({\mathrm{\Gamma }}_N\times ]0,{t}_n[)}^2)+\frac{3}{2}\frac{1}{{\mu }_f}\sum_{m=1}^n \Delta t({||{{K}}^{\frac{1}{2}}\nabla \enspace {\bar{e}}_p^{m-1}||}_{{L}^2({\mathrm{\Omega }}_1)}^2+2{||{{K}}^{\frac{1}{2}}\nabla \enspace {\bar{a}}_p^{m-1}||}_{{L}^2({\mathrm{\Omega }}_1)}^2+2{||{{K}}^{\frac{1}{2}}\nabla \enspace {E}^{m-1}(\bar{p})||}_{{L}^2({\mathrm{\Omega }}_1)}^2)+\frac{3}{{\alpha }^2\beta }(\Delta t{)}^2\sum_{m=1}^n {||{E}^m(q)||}_{{L}^2({\mathrm{\Omega }}_1)}^2+40M(\Delta t{)}^2{\Vert {\mathrm{\partial }}_t\left(\frac{1}{M}p+\alpha \nabla \middot {u}\right)\Vert }_{{L}^2({\mathrm{\Omega }}_1\times ]0,{t}_n[)}^2. $$(86)Now, we substitute (86) into (77) with the choice γ = 1 2 Mathematical equation: $ \gamma =\frac{1}{2}$. The first sum in the second line of the above right-hand side cancels with the corresponding sum in the left-hand side of (77) with the exception of the first and last term. More precisely, there remains a term (that is neglected for the moment) in the left-hand side 3 2 μ f Δ t | | K 1 2   e ¯ p n | | L 2 ( Ω 1 ) 2 Mathematical equation: $$ \frac{3}{2{\mu }_f}\Delta t{||{{K}}^{\frac{1}{2}}\nabla \enspace {\bar{e}}_p^n||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2 $$and a term in the right-hand side that is included in the initial error, 3 2 μ f Δ t | | K 1 2   e ¯ p 0 | | L 2 ( Ω 1 ) 2 . Mathematical equation: $$ \frac{3}{2{\mu }_f}\Delta t{||{{K}}^{\frac{1}{2}}\nabla \enspace {\bar{e}}_p^0||}_{{L}^2({\mathrm{\Omega }}_1)}^2. $$All other remaining terms, apart from the approximation errors, contain time errors and interpolation errors. The latter are left as such since they depend on the degree of the finite element functions and the regularity of the solution. For the time errors, we observe that for any function f in L1(0, T), | E m ( f ) | = 1 Δ t | t m - 1 t m ( s t m t f ( τ ) d τ ) d s | ( Δ t 3 ) 1 2 | | t f | | L 2 ( ] t m - 1 , t m [ ) . Mathematical equation: $$ |{E}^m(f)|=\frac{1}{\Delta t}\left|{\int }_{{t}_{m-1}}^{{t}_m} \left({\int }_s^{{t}_m} {\mathrm{\partial }}_tf(\tau )\mathrm{d}\tau \right)\mathrm{d}s\right|\le {\left(\frac{\Delta t}{3}\right)}^{\frac{1}{2}}{||{\mathrm{\partial }}_tf||}_{{L}^2(]{t}_{m-1},{t}_m[)}. $$(87)Hence, grouping terms and applying (87) for the time errors we deduce the following intermediate result: 1 M ( | | e ¯ p n | | L 2 ( Ω 1 ) 2 + m = 1 n - 1 | | δ ( e ¯ p m ) | | L 2 ( Ω 1 ) 2 ) + G ( | | ε ( e u n ) | | L 2 ( Ω ) 2 + 2 m = 1 n | | ( ε ( δ ( e u m ) ) | | L 2 ( Ω ) 2 ) + λ 2 ( | | · ( e u n ) | | L 2 ( Ω ) 2 + 2 m = 1 n | | · ( δ ( e u m ) | | L 2 ( Ω ) 2 ) + 3 2 μ f Δ   t | | K 1 2   e ¯ p n | | L 2 ( Ω 1 ) 2 1 M m = 1 n - 1 Δ t | | e ¯ p m | | L 2 ( Ω 1 ) 2 + G m = 1 n - 1 Δ t | | ε ( e u m ) | | L 2 ( Ω ) 2 + λ 2 m = 1 n - 1 Δ t | | · ( e u m ) | | L 2 ( Ω ) 2 + E time n + E space n + E initial . Mathematical equation: $$ \frac{1}{M}\left({\left|\left|{\bar{e}}_p^n\right|\right|}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+\sum_{m=1}^{n-1} {||\delta ({\bar{e}}_p^m)||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2\right)+G\left({||{\epsilon }({e}_{{u}}^n)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+2\sum_{m=1}^n {||({\epsilon }(\delta ({e}_{{u}}^m))||}_{{L}^2\left(\mathrm{\Omega }\right)}^2\right)+\frac{\lambda }{2}\left({||\nabla \middot ({e}_{{u}}^n)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+2\sum_{m=1}^n {||\nabla \middot (\delta ({e}_{{u}}^m)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2\right)+\frac{3}{2{\mu }_f}\Delta \enspace t{||{{K}}^{\frac{1}{2}}\nabla \enspace {\bar{e}}_p^n||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2\le \frac{1}{M}\sum_{m=1}^{n-1} \Delta t{||{\bar{e}}_p^m||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+G\sum_{m=1}^{n-1} \Delta t{||{\epsilon }\left({e}_{{u}}^m\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+\frac{\lambda }{2}\sum_{m=1}^{n-1} \Delta t{||\nabla \middot \left({e}_{{u}}^m\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+{\mathcal{E}}_{\mathrm{time}}^n+{\mathcal{E}}_{\mathrm{space}}^n+{\mathcal{E}}_{\mathrm{initial}}. $$(88)Then (82) follows from Gronwall’s lemma.

Note that (82) does not address the error on the gradient of the pressure; it has been eliminated to decrease the restriction on the number of iterations. But this error is an easy consequence of the error equality (67) and the bounds resulting from (82). Thus we obtain with a constant D that is independent of n, Δt and h, 1 μ f m = 1 n Δ t | | K 1 2   e ¯ p m | | L 2 ( Ω 1 ) 2 D ( E time n + E space n + E initial ) exp ( t n ) . Mathematical equation: $$ \frac{1}{{\mu }_f}\sum_{m=1}^n \Delta t{||{{K}}^{\frac{1}{2}}\nabla \enspace {\bar{e}}_p^m||}_{{L}^2({\mathrm{\Omega }}_1)}^2\le D({\mathcal{E}}_{\mathrm{time}}^n+{\mathcal{E}}_{\mathrm{space}}^n+{\mathcal{E}}_{\mathrm{initial}})\mathrm{exp}({t}_n). $$(89)

There remains to take into account the interpolation error in space and the initial errors. Suppose that ∂ t p belongs to L 2 ( 0 , T ; H s 1 ( Ω 1 ) ) Mathematical equation: $ {L}^2(0,T;{H}^{{s}_1}({\mathrm{\Omega }}_1))$ and ∂ t u belongs to L 2 ( 0 , T ; H s 2 ( Ω 1 ) d ) , s 1 , s 2 1 Mathematical equation: $ {L}^2(0,T;{H}^{{s}_2}\left({\mathrm{\Omega }}_1{)}^d\right),{s}_1,{s}_2\ge 1$. Recall that k ≥ 1, respectively m ≥ 1, is the degree of the finite element polynomials of the displacement, respectively the pressure. By taking into account the approximation properties (30) of Π h and (29) of R h and the regularity (28) of the triangulation, we deduce, with various constants C independent of n, Δt, and h, | | t a p | | L 2 ( Ω 1 × ] 0 , T [ ) 2 C h 2 min ( s 1 , m ) | | t p | | L 2 ( 0 , T ; H s 1 ( Ω 1 ) ) 2 , | | ε ( t a u ) | | L 2 ( Ω × ] 0 , T [ ) 2 + | | · ( t a u ) | | L 2 ( Ω × ] 0 , T [ ) 2 C h 2 ( min ( s 2 , k ) - 1 ) | | t u | | L 2 ( 0 , T ; H s 2 ( Ω ) ) 2 , | | a ¯ p n | | L 2 ( Ω 1 ) 2 = | | Π h ( p ¯ n ) - p ¯ n | | L 2 ( Ω 1 ) 2 = | | Π h ( p n ) - p n | | L 2 ( Ω 1 ) 2 C h 2 ( min ( s 1 , m ) ) sup t ] 0 , T [ | p | H s 1 ( Ω 1 ) 2 , | | ε ( a u n ) | | L 2 ( Ω ) 2 + | | · ( a u n ) | | L 2 ( Ω ) 2 C h 2 ( min ( s 2 , k ) - 1 ) sup t ] 0 , T [ | u | H s 2 ( Ω ) 2 , m = 1 n Δ t | | K 1 2   a ¯ p m - 1 | | L 2 ( Ω 1 ) 2 = m = 1 n Δ t | | K 1 2 ( Π h ( p m - 1 ) - p m - 1 ) | | L 2 ( Ω 1 ) 2 T λ max h 2 ( min ( s 1 , k ) - 1 ) sup t ] 0 , T [ | p | H s 1 ( Ω 1 ) 2 . Mathematical equation: $$ \begin{array}{ll}{||{\mathrm{\partial }}_t{a}_p||}_{{L}^2({\mathrm{\Omega }}_1\times ]0,T[)}^2& \le C{h}^{2\mathrm{min}({s}_1,m)}{||{\mathrm{\partial }}_tp||}_{{L}^2(0,T;{H}^{{s}_1}({\mathrm{\Omega }}_1))}^2,\\ {||{\epsilon }({\mathrm{\partial }}_t{a}_{{u}})||}_{{L}^2(\mathrm{\Omega }\times ]0,T[)}^2+{||\nabla \middot ({\mathrm{\partial }}_t{a}_{{u}})||}_{{L}^2(\mathrm{\Omega }\times ]0,T[)}^2& \le C{h}^{2(\mathrm{min}({s}_2,k)-1)}{||{\mathrm{\partial }}_t{u}||}_{{L}^2(0,T;{H}^{{s}_2}(\mathrm{\Omega }))}^2,\\ {||{\bar{a}}_p^n||}_{{L}^2({\mathrm{\Omega }}_1)}^2={||{\mathrm{\Pi }}_h({\bar{p}}^n)-{\bar{p}}^n||}_{{L}^2({\mathrm{\Omega }}_1)}^2={||{\mathrm{\Pi }}_h({p}^n)-{p}^n||}_{{L}^2({\mathrm{\Omega }}_1)}^2& \le C{h}^{2(\mathrm{min}({s}_1,m))}\underset{t\in ]0,T[}{\mathrm{sup}}|p{|}_{{H}^{{s}_1}({\mathrm{\Omega }}_1)}^2,\\ {||{\epsilon }({a}_{{u}}^n)||}_{{L}^2(\mathrm{\Omega })}^2+{||\nabla \middot ({a}_{{u}}^n)||}_{{L}^2(\mathrm{\Omega })}^2& \le C{h}^{2(\mathrm{min}({s}_2,k)-1)}\underset{t\in ]0,T[}{\mathrm{sup}}|{u}{|}_{{H}^{{s}_2}(\mathrm{\Omega })}^2,\\ \sum_{m=1}^n \Delta t{||{{K}}^{\frac{1}{2}}\nabla \enspace {\bar{a}}_p^{m-1}||}_{{L}^2({\mathrm{\Omega }}_1)}^2=\sum_{m=1}^n \Delta t{||{{K}}^{\frac{1}{2}}\nabla ({\mathrm{\Pi }}_h({p}^{m-1})-{p}^{m-1})||}_{{L}^2({\mathrm{\Omega }}_1)}^2& \le T{\lambda }_{\mathrm{max}}{h}^{2(\mathrm{min}({s}_1,k)-1)}\underset{t\in ]0,T[}{\mathrm{sup}}|p{|}_{{H}^{{s}_1}({\mathrm{\Omega }}_1)}^2.\end{array} $$(90)

Finally, we turn to the initial errors. By (32), the initial pressure error vanishes, e ¯ p 0 = Π h ( p 0 ) - Π h ( p 0 ) = 0 . Mathematical equation: $$ {\bar{e}}_p^0={\mathrm{\Pi }}_h({p}^0)-{\mathrm{\Pi }}_h({p}^0)=0. $$

The initial displacement errors follow from (65) at n = 0, 2 G ( ε ( R h ( u 0 ) - u h 0 ) , ε ( v h ) ) Ω + λ ( · ( R h ( u 0 ) - u h 0 ) , · v h ) Ω = 2 G ( ε ( R h ( u 0 ) - u 0 ) , ε ( v h ) ) Ω + λ ( · ( R h ( u 0 ) - u 0 ) , · v h ) Ω - α ( p ¯ h 0 - p ¯ 0 , · v h ) Ω 1 . Mathematical equation: $$ 2G({\epsilon }({R}_h({{u}}^0)-{{u}}_h^0),{\epsilon }({{v}}_h){)}_{\mathrm{\Omega }}+\lambda (\nabla \middot ({R}_h({{u}}^0)-{{u}}_h^0),\nabla \middot {{v}}_h{)}_{\mathrm{\Omega }}=2G({\epsilon }({R}_h({{u}}^0)-{{u}}^0),{\epsilon }({{v}}_h){)}_{\mathrm{\Omega }}+\lambda (\nabla \middot ({R}_h({{u}}^0)-{{u}}^0),\nabla \middot {{v}}_h{)}_{\mathrm{\Omega }}-\alpha ({\bar{p}}_h^0-{\bar{p}}^0,\nabla \middot {{v}}_h{)}_{{\mathrm{\Omega }}_1}. $$

By testing this equation with v h = R h ( u 0 ) - u h 0 Mathematical equation: $ {{v}}_h={R}_h({{u}}^0)-{{u}}_h^0$, standard applications of Young’s inequality yield G | | ε ( R h ( u 0 ) - u h 0 ) | | L 2 ( Ω ) 2 G | | ε ( R h ( u 0 ) - u 0 ) | | L 2 ( Ω ) 2 + λ 2 | | · ( R h ( u 0 ) - u 0 ) | | L 2 ( Ω ) 2 + α 2 2 λ | | Π h ( p 0 ) - p 0 | | L 2 ( Ω 1 ) 2 , Mathematical equation: $$ G{||{\epsilon }({R}_h({{u}}^0)-{{u}}_h^0)||}_{{L}^2(\mathrm{\Omega })}^2\le G{||{\epsilon }({R}_h({{u}}^0)-{{u}}^0)||}_{{L}^2(\mathrm{\Omega })}^2+\frac{\lambda }{2}{||\nabla \middot ({R}_h({{u}}^0)-{{u}}^0)||}_{{L}^2(\mathrm{\Omega })}^2+\frac{{\alpha }^2}{2\lambda }{||{\mathrm{\Pi }}_h({p}^0)-{p}^0||}_{{L}^2({\mathrm{\Omega }}_1)}^2, $$ λ | | · ( R h ( u 0 ) - u h 0 ) | | L 2 ( Ω ) 2 G 2 | | ε ( R h ( u 0 ) - u 0 ) | | L 2 ( Ω ) 2 + 2 λ | | · ( R h ( u 0 ) - u 0 ) | | L 2 ( Ω ) 2 + 2 α 2 λ | | Π h ( p 0 ) - p 0 | | L 2 ( Ω 1 ) 2 . Mathematical equation: $$ \lambda {||\nabla \middot \left({R}_h\left({{u}}^0\right)-{{u}}_h^0\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2\le \frac{G}{2}{||{\epsilon }\left({R}_h\left({{u}}^0\right)-{{u}}^0\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+2\lambda {||\nabla \middot \left({R}_h\left({{u}}^0\right)-{{u}}^0\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+\frac{2{\alpha }^2}{\lambda }{||{\mathrm{\Pi }}_h\left({p}^0\right)-{p}^0||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2. $$

Hence the initial error has the same order of convergence as the other errors in space. The next theorem collects these results.

Theorem 4.2.

In addition to the assumptions and notation of Proposition 4.2 , we suppose that the data satisfy ∂ t f  ∈ L2(Ω × ]0, T[) d , t t N  ∈ L2 N  × ]0, T[) d , and ∂ t q ∈ L 2 1 × ]0, T[), that the solution satisfies p H 1 ( 0 , T ; H s 1 ( Ω 1 ) ) Mathematical equation: $ p\in {H}^1(0,T;{H}^{{s}_1}({\mathrm{\Omega }}_1))$ and u H 1 ( 0 , T ; H s 2 ( Ω ) d ) Mathematical equation: $ {u}\in {H}^1(0,T;{H}^{{s}_2}(\mathrm{\Omega }{)}^d)$ , and that the assumption (81) on the number of iterations holds. Then, the solution of the fully discrete scheme (32)(37) satisfies the error bounds for all n, 1 ≤ n ≤ N, sup 0 n N | | p h n - p n | | L 2 ( Ω 1 ) + sup 0 n N | | ε ( u h n - u n ) | | L 2 ( Ω ) + ( m = 1 N Δ t | | K 1 2 ( p h m - p m ) | | L 2 ( Ω 1 ) 2 ) 1 2 C ( h min ( s 1 , m ) - 1 + h min ( s 2 , k ) - 1 + Δ t ) , Mathematical equation: $$ \begin{array}{ll}\underset{0\le n\le N}{\mathrm{sup}}{||{p}_h^n-{p}^n||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}+& \underset{0\le n\le N}{\mathrm{sup}}{||{\epsilon }({{u}}_h^n-{{u}}^n)||}_{{L}^2\left(\mathrm{\Omega }\right)}+{\left(\sum_{m=1}^N \Delta t{||{{K}}^{\frac{1}{2}}\nabla ({p}_h^m-{p}^m)||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2\right)}^{\frac{1}{2}}\\ & \le C\left({h}^{\mathrm{min}({s}_1,m)-1}+{h}^{\mathrm{min}({s}_2,k)-1}+\Delta t\right),\end{array} $$(91) with a constant C independent of h and Δt.

5 Mixed approximation and algorithm

The material of Sections 3 and 4 is easily adapted to the mixed formulation (25)(27), with initial condition (11), and to avoid repetitions, we sketch here the main ideas. The displacement is discretized in the same spaces X h and V h , but the velocity and pressure spaces are discretized by a standard mixed pair, ( Z h , Q h ), where Z h is a finite element subspace of Z with interpolation operator P h and Q h a finite element subspace of L21), with interpolation operator ρ h , ( Z h , Q h ) being compatible in the sense that they satisfy a uniform discrete inf-sup condition. In particular, we make the assumption, commonly used in mixed methods, q L 2 ( Ω 1 ) ,   ζ h Z h ,   ( ϱ ( q ) - q , · ζ h ) Ω 1 = 0 . Mathematical equation: $$ \forall q\in {L}^2({\mathrm{\Omega }}_1),\enspace \hspace{1em}\forall {{\zeta }}_h\in {{Z}}_h,\hspace{1em}\enspace (\mathrm{\varrho }(q)-q,\nabla \middot {{\zeta }}_h{)}_{{\mathrm{\Omega }}_1}=0. $$(92)

As previously, we denote p ¯ h m = p h m - ρ f , r Mathematical equation: $ {\bar{p}}_h^m={p}_h^m-{\rho }_{f,r}{g\eta }$. Starting from p h 0 = ϱ h ( p 0 ) , Mathematical equation: $$ {p}_h^0={\mathrm{\varrho }}_h\left({p}_0\right), $$(93)the fixed-stress splitting algorithm computes u h 0 V h Mathematical equation: $ {{u}}_h^0\in {{V}}_h$ by solving (33), v h V h ,   2 G ( ε ( u h 0 ) , ε ( v h ) ) Ω + λ ( · u h 0 , · v h ) Ω = α   ( p h 0 , · v h ) Ω 1 + ( f , v h ) Ω + ( t N 0 , v h ) Γ N , Mathematical equation: $$ \forall {{v}}_h\in {{V}}_h,\enspace 2G({\epsilon }({{u}}_h^0),{\epsilon }({{v}}_h){)}_{\mathrm{\Omega }}+\lambda (\nabla \middot {{u}}_h^0,\nabla \middot {{v}}_h{)}_{\mathrm{\Omega }}=\alpha \enspace ({p}_h^0,\nabla \middot {{v}}_h{)}_{{\mathrm{\Omega }}_1}+({f},{{v}}_h{)}_{\mathrm{\Omega }}+({{t}}_N^0,{{v}}_h{)}_{{\mathrm{\Gamma }}_N}, $$ z h 0 Z h Mathematical equation: $ {{z}}_h^0\in {{Z}}_h$ by solving ζ h Z h ,   μ f ( K - 1 z h 0 , ζ h ) Ω 1 = ( p ¯ h 0 , · ζ h ) Ω 1 Mathematical equation: $$ \forall {{\zeta }}_h\in {{Z}}_h,\enspace {\mu }_f({{K}}^{-1}{{z}}_h^0,{{\zeta }}_h{)}_{{\mathrm{\Omega }}_1}=({\bar{p}}_h^0,\nabla \middot {{\zeta }}_h{)}_{{\mathrm{\Omega }}_1} $$(94)and σ ¯ h 0 Mathematical equation: $ {\overline{\sigma }}_h^0$ by (34), σ ¯ h 0 = λ · u h 0 - α p h 0 . Mathematical equation: $$ {\overline{\sigma }}_h^0=\lambda \nabla \middot {{u}}_h^0-\alpha {p}_h^0. $$

Then for n 1 Mathematical equation: $ n\ge 1$,

  1. Set p h n , 0 = p h n - 1 Mathematical equation: $ {p}_h^{n,0}={p}_h^{n-1}$, u h n , 0 = u h n - 1 Mathematical equation: $ {{u}}_h^{n,0}={{u}}_h^{n-1}$, z h n , 0 = z h n - 1 Mathematical equation: $ {{z}}_h^{n,0}={{z}}_h^{n-1}$, and σ ¯ h n , 0 = σ ¯ h n - 1 Mathematical equation: $ {\overline{\sigma }}_h^{n,0}={\overline{\sigma }}_h^{n-1}$.

  2. For l 1 Mathematical equation: $ \mathcal{l}\ge 1$, compute

(a) the pair ( p h n , l , z h n , l ) Mathematical equation: $ ({p}_h^{n,\mathcal{l}},{{z}}_h^{n,\mathcal{l}})$ in Q h × Z h Mathematical equation: $ {Q}_h\times {{Z}}_h$ by solving θ h Q h ,   ( 1 M + α 2 λ ) 1 Δ t ( p h n , l - p h n - 1 , θ h ) Ω 1 + ( · z h n , l , θ h ) Ω 1 = - α λ 1 Δ t ( σ ¯ h n , l - 1 - σ ¯ h n - 1 , θ h ) Ω 1 + ( q n , θ h ) Ω 1 , Mathematical equation: $$ \forall {\theta }_h\in {Q}_h,\enspace \left(\frac{1}{M}+\frac{{\alpha }^2}{\lambda }\right)\frac{1}{\Delta t}({p}_h^{n,\mathcal{l}}-{p}_h^{n-1},{\theta }_h{)}_{{\mathrm{\Omega }}_1}+(\nabla \middot {{z}}_h^{n,\mathcal{l}},{\theta }_h{)}_{{\mathrm{\Omega }}_1}=-\frac{\alpha }{\lambda }\frac{1}{\Delta t}({\overline{\sigma }}_h^{n,\mathcal{l}-1}-{\overline{\sigma }}_h^{n-1},{\theta }_h{)}_{{\mathrm{\Omega }}_1}+({q}^n,{\theta }_h{)}_{{\mathrm{\Omega }}_1}, $$(95) ζ h Z h ,   μ f ( K - 1 z h n , l , ζ h ) Ω 1 = ( p ¯ h n , l , · ζ h ) Ω 1 , Mathematical equation: $$ \forall {{\zeta }}_h\in {{Z}}_h,\enspace {\mu }_f({{K}}^{-1}{{z}}_h^{n,\mathcal{l}},{{\zeta }}_h{)}_{{\mathrm{\Omega }}_1}=({\bar{p}}_h^{n,\mathcal{l}},\nabla \middot {{\zeta }}_h{)}_{{\mathrm{\Omega }}_1}, $$(96)

(b) compute the predictor of the difference in fluid content δ φ p Mathematical equation: $ {\delta }_{\phi }^p$ by δ φ p : = ( 1 M + α 2 λ ) ( p h n , l - p h n , l - 1 ) . Mathematical equation: $$ {\delta }_{\phi }^p:=(\frac{1}{M}+\frac{{\alpha }^2}{\lambda })({p}_h^{n,\mathcal{l}}-{p}_h^{n,\mathcal{l}-1}). $$

(c) σ ¯ h n , l Mathematical equation: $ {\overline{\sigma }}_h^{n,\mathcal{l}}$ by (37) σ ¯ h n , l = λ · u h n , l - α p h n , l , Mathematical equation: $$ {\overline{\sigma }}_h^{n,\mathcal{l}}=\lambda \nabla \middot {{u}}_h^{n,\mathcal{l}}-\alpha {p}_h^{n,\mathcal{l}}, $$

(d) compute the corrector to difference in fluid content δ φ c Mathematical equation: $ {\delta }_{\phi }^c$ by δ φ c : = α ( u h n , l - u h n , l - 1 ) + 1 M ( p h n , l - p h n , l - 1 ) . Mathematical equation: $$ {\delta }_{\phi }^c:=\alpha \nabla \cdot ({u}_h^{n,\mathcal{l}}-{u}_h^{n,\mathcal{l}-1})+\frac{1}{M}({p}_h^{n,\mathcal{l}}-{p}_h^{n,\mathcal{l}-1}). $$

If δ φ c - δ φ p : = α ( u h n , l - u h n , l - 1 ) - α 2 λ ( p h n , l - p h n , l - 1 ) > Mathematical equation: $ {\delta }_{\phi }^c-{\delta }_{\phi }^p:=\alpha \nabla \cdot ({u}_h^{n,\mathcal{l}}-{u}_h^{n,\mathcal{l}-1})-\frac{{\alpha }^2}{\lambda }({p}_h^{n,\mathcal{l}}-{p}_h^{n,\mathcal{l}-1})>$ threshold, increment l Mathematical equation: $ \mathcal{l}$ and return to (a);

if δ φ Mathematical equation: $ {\delta }_{\phi }\le $ threshold, set l n l ,   p h n p h n , l n ,   u h n u h n , l n ,   σ ¯ h n σ ¯ h n , l n , Mathematical equation: $$ {\mathcal{l}}_n\mathbf{\coloneqq} \mathcal{l},\hspace{1em}\enspace {p}_h^n\mathbf{\coloneqq} {p}_h^{n,{\mathcal{l}}_n},\hspace{1em}\enspace {{u}}_h^n\mathbf{\coloneqq} {{u}}_h^{n,{\mathcal{l}}_n},\enspace \hspace{1em}{\overline{\sigma }}_h^n\mathbf{\coloneqq} {\overline{\sigma }}_h^{n,{\mathcal{l}}_n}, $$(97)and march in time, set n ≔ n + 1 and return to step (1).

It is easy to check that this algorithm generates a unique sequence of discrete functions.

5.1 Contraction of the algorithm and stability of the mixed scheme

The contraction proof for the mixed scheme is very similar to that for (32)(38). With the notation (39) for β and δ v n , l = v n , l - v n , l - 1 , Mathematical equation: $$ \delta {v}^{n,\mathcal{l}}={v}^{n,\mathcal{l}}-{v}^{n,\mathcal{l}-1}, $$we derive by the same argument | | δ σ ¯ h n , l | | L 2 ( Ω 1 ) 2 + λ 2 | | · ( δ u h n , l ) | | L 2 ( Ω 1 ) 2 + 2 λ 2 | | · ( δ u h n , l ) | | L 2 ( Ω 2 ) 2 + 2 Δ t μ f β | | K - 1 2 δ z h n , l | | L 2 ( Ω 1 ) 2 + 4 | | ε ( δ u h n , l ) | | L 2 ( Ω ) 2 1 ( β λ ) 2 | | δ σ ¯ h n , l - 1 | | L 2 ( Ω 1 ) 2 . Mathematical equation: $$ {||\delta {\overline{\sigma }}_h^{n,\mathcal{l}}||}_{{L}^2({\mathrm{\Omega }}_1)}^2+{\lambda }^2{||\nabla \middot (\delta {{u}}_h^{n,\mathcal{l}})||}_{{L}^2({\mathrm{\Omega }}_1)}^2+2{\lambda }^2{||\nabla \middot (\delta {{u}}_h^{n,\mathcal{l}})||}_{{L}^2({\mathrm{\Omega }}_2)}^2+2\Delta t\frac{{\mu }_f}{\beta }{||{{K}}^{-\frac{1}{2}}\delta {{z}}_h^{n,\mathcal{l}}||}_{{L}^2({\mathrm{\Omega }}_1)}^2+4{G\lambda }{||{\epsilon }(\delta {{u}}_h^{n,\mathcal{l}})||}_{{L}^2(\mathrm{\Omega })}^2\le \frac{1}{({\beta \lambda }{)}^2}{||\delta {\overline{\sigma }}_h^{n,\mathcal{l}-1}||}_{{L}^2({\mathrm{\Omega }}_1)}^2. $$

Therefore | | δ σ ¯ h n , l | | L 2 ( Ω 1 ) 1 ( β λ ) l - 1 | | δ σ ¯ h n , 1 | | L 2 ( Ω 1 ) , | | · ( δ u h n , l ) | | L 2 ( Ω ) 1 λ 1 ( β λ ) l - 1 | | δ σ ¯ h n , 1 | | L 2 ( Ω 1 ) , | | K - 1 2 δ z h n , l | | L 2 ( Ω 1 ) ( β 2 Δ t μ f ) 1 2 1 ( β λ ) l - 1 | | δ σ ¯ h n , 1 | | L 2 ( Ω 1 ) , | | ε ( δ u h n , l ) | | L 2 ( Ω ) 1 2 λ G 1 ( β λ ) l - 1 | | δ σ ¯ h n , 1 | | L 2 ( Ω 1 ) , Mathematical equation: $$ \begin{array}{ll}{||\delta {\overline{\sigma }}_h^{n,\mathcal{l}}||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}& \le \frac{1}{({\beta \lambda }{)}^{\mathcal{l}-1}}{||\delta {\overline{\sigma }}_h^{n,1}||}_{{L}^2\left({\mathrm{\Omega }}_1\right)},\\ {||\nabla \middot \left(\delta {{u}}_h^{n,\mathcal{l}}\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}& \le \frac{1}{\lambda }\frac{1}{({\beta \lambda }{)}^{\mathcal{l}-1}}{||\delta {\overline{\sigma }}_h^{n,1}||}_{{L}^2\left({\mathrm{\Omega }}_1\right)},\\ {||{{K}}^{-\frac{1}{2}}\delta {{z}}_h^{n,\mathcal{l}}||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}& \le {\left(\frac{\beta }{2\Delta t{\mu }_f}\right)}^{\frac{1}{2}}\frac{1}{({\beta \lambda }{)}^{\mathcal{l}-1}}{||\delta {\overline{\sigma }}_h^{n,1}||}_{{L}^2\left({\mathrm{\Omega }}_1\right)},\\ {||{\epsilon }\left(\delta {{u}}_h^{n,\mathcal{l}}\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}& \le \frac{1}{2\sqrt{{\lambda G}}}\frac{1}{({\beta \lambda }{)}^{\mathcal{l}-1}}{||\delta {\overline{\sigma }}_h^{n,1}||}_{{L}^2\left({\mathrm{\Omega }}_1\right)},\\ & \end{array} $$(98)and again we must estimate | | δ σ ¯ h n , 1 | | L 2 ( Ω 1 ) Mathematical equation: $ {||\delta {\overline{\sigma }}_h^{n,1}||}_{{L}^2({\mathrm{\Omega }}_1)}$. As the discrete displacement equation (36) is unchanged, formula (42) is also valid here and we must derive the analogue of (43). This is readily done by testing (95) at level l = 1 Mathematical equation: $ \mathcal{l}=1$ with θ h = p ¯ h n , 1 - p ¯ h n - 1 Mathematical equation: $ {\theta }_h={\bar{p}}_h^{n,1}-{\bar{p}}_h^{n-1}$, splitting ( · z h n , 1 , p ¯ h n , 1 - p ¯ h n - 1 ) Ω 1 = ( · ( z h n , 1 - z h n - 1 ) , p ¯ h n , 1 - p ¯ h n - 1 ) Ω 1 + ( · z h n - 1 , p ¯ h n , 1 - p ¯ h n - 1 ) Ω 1 , Mathematical equation: $$ (\nabla \middot {{z}}_h^{n,1},{\bar{p}}_h^{n,1}-{\bar{p}}_h^{n-1}{)}_{{\mathrm{\Omega }}_1}=(\nabla \middot ({{z}}_h^{n,1}-{{z}}_h^{n-1}),{\bar{p}}_h^{n,1}-{\bar{p}}_h^{n-1}{)}_{{\mathrm{\Omega }}_1}+(\nabla \middot {{z}}_h^{n-1},{\bar{p}}_h^{n,1}-{\bar{p}}_h^{n-1}{)}_{{\mathrm{\Omega }}_1}, $$and using the velocity-pressure equation to eliminate the divergence in both terms of the above right-hand side. This gives ( · z h n , 1 , p ¯ h n , 1 - p ¯ h n - 1 ) Ω 1 = μ f | | K - 1 2 ( z h n , 1 - z h n - 1 ) | | L 2 ( Ω 1 ) 2 + μ f ( K - 1 ( z h n , 1 - z h n - 1 ) , z h n - 1 ) Ω 1 . Mathematical equation: $$ (\nabla \middot {{z}}_h^{n,1},{\bar{p}}_h^{n,1}-{\bar{p}}_h^{n-1}{)}_{{\mathrm{\Omega }}_1}={\mu }_f{||{{K}}^{-\frac{1}{2}}({{z}}_h^{n,1}-{{z}}_h^{n-1})||}_{{L}^2({\mathrm{\Omega }}_1)}^2+{\mu }_f({{K}}^{-1}({{z}}_h^{n,1}-{{z}}_h^{n-1}),{{z}}_h^{n-1}{)}_{{\mathrm{\Omega }}_1}. $$Thus, we have the analogue of Proposition 3.2, with the same notation.

Proposition 5.1.

We have for all n, 1 ≤ n ≤ N, α 2 β Δ t | | p h n , 1 - p h n - 1 | | L 2 ( Ω 1 ) 2 + μ f | | K - 1 2 ( z h n , 1 - z h n - 1 ) | | L 2 ( Ω 1 ) 2 Δ t α 2 β | | q n | | L 2 ( Ω 1 ) 2 + μ f | | K - 1 2 z h n - 1 | | L 2 ( Ω 1 ) 2 . Mathematical equation: $$ \frac{{\alpha }^2\beta }{\Delta t}{||{p}_h^{n,1}-{p}_h^{n-1}||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+{\mu }_f{||{{K}}^{-\frac{1}{2}}\left({{z}}_h^{n,1}-{{z}}_h^{n-1}\right)||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2\le \frac{\Delta t}{{\alpha }^2\beta }{||{q}^n||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+{\mu }_f{||{{K}}^{-\frac{1}{2}}{{z}}_h^{n-1}||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2. $$(99)

Then a combination of (42) and (99) yields the analogue of (44), | | σ ¯ h n , 1 - σ ¯ h n - 1 | | L 2 ( Ω 1 ) 2 4 Δ t β ( μ f | | K - 1 2 z h n - 1 | | L 2 ( Ω 1 ) 2 + Δ t α 2 β | | q n | | L 2 ( Ω 1 ) 2 ) + λ G ( C 2 | | f n - f n - 1 | | L 2 ( Ω ) 2 + C ̃ 2 | | t N n - t N n - 1 | | L 2 ( Γ N ) 2 ) , Mathematical equation: $$ \begin{array}{ll}{||{\overline{\sigma }}_h^{n,1}-{\overline{\sigma }}_h^{n-1}||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2\le & 4\frac{\Delta t}{\beta }\left({\mu }_f{||{{K}}^{-\frac{1}{2}}{{z}}_h^{n-1}||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+\frac{\Delta t}{{\alpha }^2\beta }{||{q}^n||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2\right)\\ & +\frac{\lambda }{G}\left({C}^2{||{{f}}^n-{{f}}^{n-1}||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+{\mathop{C}\limits^\tilde}^2{||{{t}}_N^n-{{t}}_N^{n-1}||}_{{L}^2\left({\mathrm{\Gamma }}_N\right)}^2\right),\end{array} $$(100)which again relies on the stability of the scheme.

Now, by using again the velocity-pressure equation, so that ( · z h n , p ¯ h n ) Ω 1 = μ f | | K - 1 2 z h n | | L 2 ( Ω 1 ) 2 , Mathematical equation: $$ (\nabla \middot {{z}}_h^n,{\bar{p}}_h^n{)}_{{\mathrm{\Omega }}_1}={\mu }_f{||{{K}}^{-\frac{1}{2}}{{z}}_h^n||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2, $$it is easy to check that all steps of the proof of the stability Proposition 3.3 carry over to the mixed scheme without modification, and we have the following proposition.

Proposition 5.2.

Under the assumptions and notation of Proposition 3.3 , the following bound holds for all n, 1 ≤ n ≤ N, 1 M ( | | p ¯ h n | | L 2 ( Ω 1 ) 2 + m = 1 n - 1 | | p h m - p h m - 1 | | L 2 ( Ω 1 ) 2 ) + G ( | | ε ( u h n ) | | L 2 ( Ω ) 2 + 2 m = 1 n | | ε ( u h m - u h m - 1 ) | | L 2 ( Ω ) 2 ) + λ ( m = 1 n | | · ( u h m - u h m - 1 ) | | L 2 ( Ω ) 2 ) + 2 μ f m = 1 n Δ t | | K - 1 2 z h m | | L 2 ( Ω 1 ) 2 1 M m = 1 n - 1 Δ t | | p ¯ h m | | L 2 ( Ω 1 ) 2 + G m = 1 n - 1 Δ t | | ε ( u h m ) | | L 2 ( Ω ) 2 + 5 M α 2 λ 2 1 Δ t m = 1 n | | σ ¯ h m - σ ¯ h m , l m - 1 | | L 2 ( Ω 1 ) 2 + I h 0 + D h n . Mathematical equation: $$ \begin{array}{ll}& \frac{1}{M}\left({||{\bar{p}}_h^n||}_{{L}^2({\mathrm{\Omega }}_1)}^2+\sum_{m=1}^{n-1} {||{p}_h^m-{p}_h^{m-1}||}_{{L}^2({\mathrm{\Omega }}_1)}^2\right)+G\left({||{\epsilon }({{u}}_h^n)||}_{{L}^2(\mathrm{\Omega })}^2+2\sum_{m=1}^n {||{\epsilon }({{u}}_h^m-{{u}}_h^{m-1})||}_{{L}^2(\mathrm{\Omega })}^2\right)\\ & +\lambda \left(\sum_{m=1}^n {||\nabla \middot ({{u}}_h^m-{{u}}_h^{m-1})||}_{{L}^2(\mathrm{\Omega })}^2\right)+2{\mu }_f\sum_{m=1}^n \Delta t{||{{K}}^{-\frac{1}{2}}{{z}}_h^m||}_{{L}^2({\mathrm{\Omega }}_1)}^2\\ & \le \frac{1}{M}\sum_{m=1}^{n-1} \Delta t{||{\bar{p}}_h^m||}_{{L}^2({\mathrm{\Omega }}_1)}^2+G\sum_{m=1}^{n-1} \Delta t{||{\epsilon }({{u}}_h^m)||}_{{L}^2(\mathrm{\Omega })}^2+5M\frac{{\alpha }^2}{{\lambda }^2}\frac{1}{\Delta t}\sum_{m=1}^n {||{\overline{\sigma }}_h^m-{\overline{\sigma }}_h^{m,{\mathcal{l}}_m-1}||}_{{L}^2({\mathrm{\Omega }}_1)}^2\\ & +{\mathcal{I}}_h^0+{\mathcal{D}}_h^n.\end{array} $$(101)

With this result, by reproducing the argument at the end of Section 3.1, we derive stability of the mixed scheme.

Theorem 5.1.

Under the assumptions on the data and the number of iterations (55) of Theorem 3.1 , there exists a constant C independent of n, h, and Δt, such that 1 M | | p h n | | L 2 ( Ω 1 ) 2 + G | | ε ( u h n ) | | L 2 ( Ω ) 2 + λ | | · u h n | | L 2 ( Ω ) 2 + μ f m = 1 n Δ t | | K - 1 2 z h m | | L 2 ( Ω 1 ) 2 C   exp ( t n ) . Mathematical equation: $$ \frac{1}{M}{||{p}_h^n||}_{{L}^2({\mathrm{\Omega }}_1)}^2+G{||{\epsilon }({{u}}_h^n)||}_{{L}^2(\mathrm{\Omega })}^2+\lambda {||\nabla \middot {{u}}_h^n||}_{{L}^2(\mathrm{\Omega })}^2+{\mu }_f\sum_{m=1}^n \Delta t{||{{K}}^{-\frac{1}{2}}{{z}}_h^m||}_{{L}^2({\mathrm{\Omega }}_1)}^2\le C\enspace \mathrm{exp}({t}_n). $$(102)

5.2 A priori error estimates for the mixed scheme

Let us start with the algorithmic error. We retain the notation of Section 4.1, but we replace the approximation operator Π h by the operator P h that takes its values in Z h . Proposition 4.1 is replaced by a slightly more complex result. Indeed, by proceeding as in Proposition 3.2, we introduce the term ( · z h n - 1 , p h n , 1 - p h n - 1 ) Ω 1 Mathematical equation: $ (\nabla \middot {{z}}_h^{n-1},{p}_h^{n,1}-{p}_h^{n-1}{)}_{{\mathrm{\Omega }}_1}$ that we write as ( · z h n - 1 , p h n , 1 - p h n - 1 ) Ω 1 = ( · ( z h n - 1 - P h ( z n - 1 ) ) , p h n , 1 - p h n - 1 ) Ω 1 + ( · ( P h ( z n - 1 ) - m ( z ) ) , p h n , 1 - p h n - 1 ) Ω 1 + ( · m ( z ) , p h n , 1 - p h n - 1 ) Ω 1 . Mathematical equation: $$ \begin{array}{ll}(\nabla \middot {{z}}_h^{n-1},{p}_h^{n,1}-{p}_h^{n-1}{)}_{{\mathrm{\Omega }}_1}=& (\nabla \middot ({{z}}_h^{n-1}-{P}_h({{z}}^{n-1})),{p}_h^{n,1}-{p}_h^{n-1}{)}_{{\mathrm{\Omega }}_1}+(\nabla \middot ({P}_h({{z}}^{n-1})-m({z})),{p}_h^{n,1}-{p}_h^{n-1}{)}_{{\mathrm{\Omega }}_1}\\ & +(\nabla \middot m({z}),{p}_h^{n,1}-{p}_h^{n-1}{)}_{{\mathrm{\Omega }}_1}.\end{array} $$

For the first term, since z h n - 1 - P h ( z n - 1 ) Z h Mathematical equation: $ {{z}}_h^{n-1}-{P}_h({{z}}^{n-1})\in {{Z}}_h$, we apply the discrete velocity-pressure relation, whereas the other two terms are left unchanged in order to be combined with q n . Thus, we obtain the next proposition.

Proposition 5.3.

Assuming that the solution is sufficiently smooth in space and time, we have for all n, 1 ≤ n ≤ N, α 2 | | p ¯ h n , 1 - p ¯ h n - 1 | | L 2 ( Ω 1 ) 2 μ f Δ t 2 β | | K - 1 2 ( z h n - 1 - P h ( z n - 1 ) ) | | L 2 ( Ω 1 ) 2 + 3 α 2 β 2 ( Δ t ) 2 | | · ( P h ( z n - 1 ) - m ( z ) ) | | L 2 ( Ω 1 ) 2 + 3 ( Δ t ) 2 α 2 β 2 | | q n - m ( q ) | | L 2 ( Ω 1 ) 2 + 3 Δ t α 2 β 2 | | t ( 1 M p + α · u ) | | L 2 ( Ω 1 × ] t n - 1 , t n [ ) 2 . Mathematical equation: $$ \begin{array}{ll}& {\alpha }^2{||{\bar{p}}_h^{n,1}-{\bar{p}}_h^{n-1}||}_{{L}^2({\mathrm{\Omega }}_1)}^2\le {\mu }_f\frac{\Delta t}{2\beta }{||{{K}}^{-\frac{1}{2}}({{z}}_h^{n-1}-{P}_h({{z}}^{n-1}))||}_{{L}^2({\mathrm{\Omega }}_1)}^2+\frac{3}{{\alpha }^2{\beta }^2}(\Delta t{)}^2{||\nabla \middot ({P}_h({{z}}^{n-1})-m({z}))||}_{{L}^2({\mathrm{\Omega }}_1)}^2\\ & +3\frac{(\Delta t{)}^2}{{\alpha }^2{\beta }^2}{||{q}^n-m(q)||}_{{L}^2({\mathrm{\Omega }}_1)}^2+3\frac{\Delta t}{{\alpha }^2{\beta }^2}{||{\mathrm{\partial }}_t(\frac{1}{M}p+\alpha \nabla \middot {u})||}_{{L}^2({\mathrm{\Omega }}_1\times ]{t}_{n-1},{t}_n[)}^2.\end{array} $$(103)

Then (63) is replaced by | | σ ¯ h n , l - σ ¯ h n , l - 1 | | L 2 ( Ω 1 ) 2 1 ( β   λ ) 2 l - 2 [ λ G ( C 2 | | f n - f n - 1 | | L 2 ( Ω ) 2 + C ̃ 2 | | t N n - t N n - 1 | | L 2 ( Γ N ) 2 ) + 4 ( μ f Δ t 2 β K - 1 2 ( z h n - 1 - P h ( z n - 1 ) ) L 2 ( Ω 1 ) 2 + 3 α 2 β 2 ( Δ t ) 2 | | · ( P h ( z n - 1 ) - m ( z ) ) | | L 2 ( Ω 1 ) 2 + 3 ( Δ t ) 2 α 2 β 2 | | q n - m ( q ) | | L 2 ( Ω 1 ) 2 + 3 Δ t α 2 β 2 t ( 1 M p + α · u ) L 2 ( Ω 1 × ] t n - 1 , t n [ ) 2 ) ] . Mathematical equation: $$ {||{\overline{\sigma }}_h^{n,\mathcal{l}}-{\overline{\sigma }}_h^{n,\mathcal{l}-1}||}_{{L}^2({\mathrm{\Omega }}_1)}^2\le \frac{1}{(\beta \enspace \lambda {)}^{2\mathcal{l}-2}}\left[\frac{\lambda }{G}({C}^2{||{{f}}^n-{{f}}^{n-1}||}_{{L}^2(\mathrm{\Omega })}^2+{\mathop{C}\limits^\tilde}^2{||{{t}}_N^n-{{t}}_N^{n-1}||}_{{L}^2({\mathrm{\Gamma }}_N)}^2)+4\left({\mu }_f\frac{\Delta t}{2\beta }{\Vert {{K}}^{-\frac{1}{2}}({{z}}_h^{n-1}-{P}_h({{z}}^{n-1}))\Vert }_{{L}^2({\mathrm{\Omega }}_1)}^2+\frac{3}{{\alpha }^2{\beta }^2}(\Delta t{)}^2{||\nabla \middot ({P}_h({{z}}^{n-1})-m({z}))||}_{{L}^2({\mathrm{\Omega }}_1)}^2+3\frac{(\Delta t{)}^2}{{\alpha }^2{\beta }^2}{||{q}^n-m(q)||}_{{L}^2({\mathrm{\Omega }}_1)}^2+3\frac{\Delta t}{{\alpha }^2{\beta }^2}{\Vert {\mathrm{\partial }}_t\left(\frac{1}{M}p+\alpha \nabla \middot {u}\right)\Vert }_{{L}^2({\mathrm{\Omega }}_1\times ]{t}_{n-1},{t}_n[)}^2\right)\right]. $$(104)

Note that the factor of K - 1 2 ( z h n - 1 - P h ( z n - 1 ) ) Mathematical equation: $ {{K}}^{-\frac{1}{2}}({{z}}_h^{n-1}-{P}_h({{z}}^{n-1}))$ in the right-hand side of (104) is smaller than its counter part in (36) by a factor of 1 2 Mathematical equation: $ \frac{1}{2}$. In contrast, the factors of the other terms in the right-hand side involving the interpolation errors are slightly larger, but this does not change their order of convergence.

Next, we turn to the error equation. Its derivation follows the lines of Section 4.2, up to the error of the velocity-pressure relation in which we make use of the assumption (92). Thus, we write μ f ( K - 1 z n , ζ h ) Ω 1 = ( p ¯ n , · ζ h ) Ω 1 = ( ρ h ( p ¯ n ) , · ζ h ) Ω 1 , Mathematical equation: $$ {\mu }_f({{K}}^{-1}{{z}}^n,{{\zeta }}_h{)}_{{\mathrm{\Omega }}_1}=({\bar{p}}^n,\nabla \middot {{\zeta }}_h{)}_{{\mathrm{\Omega }}_1}=({\rho }_h({\bar{p}}^n),\nabla \middot {{\zeta }}_h{)}_{{\mathrm{\Omega }}_1}, $$and hence the difference between the exact and discrete velocity-pressure equations reads μ f ( K - 1 ( P h ( z n ) - z h n ) , ζ h ) Ω 1 + μ f ( K - 1 ( z n - P h ( z n ) ) , ζ h ) Ω 1 = ( ρ h ( p ¯ n ) - p ¯ h n , · ζ h ) Ω 1 . Mathematical equation: $$ {\mu }_f({{K}}^{-1}({P}_h({{z}}^n)-{{z}}_h^n),{{\zeta }}_h{)}_{{\mathrm{\Omega }}_1}+{\mu }_f({{K}}^{-1}({{z}}^n-{P}_h({{z}}^n)),{{\zeta }}_h{)}_{{\mathrm{\Omega }}_1}=({\rho }_h({\bar{p}}^n)-{\bar{p}}_h^n,\nabla \middot {{\zeta }}_h{)}_{{\mathrm{\Omega }}_1}. $$(105)

This is an important simplification because it will eliminate the factor · ζ h Mathematical equation: $ \nabla \middot {{\zeta }}_h$ from the error equation. In addition to the notation e u n Mathematical equation: $ {e}_{{u}}^n$ and a u n Mathematical equation: $ {a}_{{u}}^n$ of (66), we set e p n = ρ h ( p n ) - p h n ,   e z n = P h ( z n ) - z h n ,   a p n = ρ h ( p n ) - p n ,   a z n = P h ( z n ) - z n . Mathematical equation: $$ {e}_p^n={\rho }_h\left({p}^n\right)-{p}_h^n,\enspace {e}_{{z}}^n={P}_h\left({{z}}^n\right)-{{z}}_h^n,\enspace {a}_p^n={\rho }_h\left({p}^n\right)-{p}^n,\enspace {a}_{{z}}^n={P}_h\left({{z}}^n\right)-{{z}}^n. $$(106)

Then (67) is replaced by 1 M ( | | e ¯ p n | | L 2 ( Ω 1 ) 2 - | | e ¯ p n - 1 | | L 2 ( Ω 1 ) 2 + | | δ ( e p n ) | | L 2 ( Ω 1 ) 2 ) + 2 G ( | | ε ( e u n ) | | L 2 ( Ω ) 2 - | | ε ( e u n - 1 ) | | L 2 ( Ω ) 2 + | | ε ( δ ( e u n ) ) | | L 2 ( Ω ) 2 ) + λ ( | | · ( e u n ) | | L 2 ( Ω ) 2 - | | · ( e u n - 1 ) | | L 2 ( Ω ) 2 + | | · ( δ ( e u n ) ) | | L 2 ( Ω ) 2 ) + 2 μ f Δ t K - 1 2 e z n L 2 ( Ω 1 ) 2 = 2 [ 1 M ( δ ( a p n ) , e ¯ p n ) Ω 1 + α ( · ( δ ( a u n ) ) , e ¯ p n ) Ω 1 + 2 G ( ε ( a u n ) , ε ( δ ( e u n ) ) ) Ω + λ ( · ( a u n ) , · δ ( e u n ) ) Ω - μ f Δ t ( K - 1 a z n , e z n ) Ω 1 - α ( a ¯ p n , · ( δ ( e u n ) ) ) Ω 1 - α λ ( σ ¯ h n - σ ¯ h n , l n - 1 , e ¯ p n ) Ω 1 + t n - 1 t n ( q ( s ) - q n + · ( z n - z ( s ) ) , e ¯ p n ) Ω 1 d s ] . Mathematical equation: $$ \frac{1}{M}({||{\bar{e}}_p^n||}_{{L}^2({\mathrm{\Omega }}_1)}^2-{||{\bar{e}}_p^{n-1}||}_{{L}^2({\mathrm{\Omega }}_1)}^2+{||\delta ({e}_p^n)||}_{{L}^2({\mathrm{\Omega }}_1)}^2)+2G({||{\epsilon }({e}_{{u}}^n)||}_{{L}^2(\mathrm{\Omega })}^2-{||{\epsilon }({e}_{{u}}^{n-1})||}_{{L}^2(\mathrm{\Omega })}^2+{||{\epsilon }(\delta ({e}_{{u}}^n))||}_{{L}^2(\mathrm{\Omega })}^2)+\lambda ({||\nabla \middot ({e}_{{u}}^n)||}_{{L}^2(\mathrm{\Omega })}^2-{||\nabla \middot ({e}_{{u}}^{n-1})||}_{{L}^2(\mathrm{\Omega })}^2+{||\nabla \middot (\delta ({e}_{{u}}^n))||}_{{L}^2(\mathrm{\Omega })}^2)+2{\mu }_f\Delta t{\Vert {{K}}^{-\frac{1}{2}}{e}_{{z}}^n\Vert }_{{L}^2({\mathrm{\Omega }}_1)}^2=2\left[\frac{1}{M}(\delta ({a}_p^n),{\bar{e}}_p^n{)}_{{\mathrm{\Omega }}_1}+\alpha (\nabla \middot (\delta ({a}_{{u}}^n)),{\bar{e}}_p^n{)}_{{\mathrm{\Omega }}_1}+2G({\epsilon }({a}_{{u}}^n),{\epsilon }(\delta ({e}_{{u}}^n)){)}_{\mathrm{\Omega }}+\lambda (\nabla \middot ({a}_{{u}}^n),\nabla \middot \delta ({e}_{{u}}^n){)}_{\mathrm{\Omega }}-{\mu }_f\Delta t({{K}}^{-1}{a}_{{z}}^n,{e}_{{z}}^n{)}_{{\mathrm{\Omega }}_1}-\alpha ({\bar{a}}_p^n,\nabla \middot (\delta ({e}_{{u}}^n)){)}_{{\mathrm{\Omega }}_1}-\frac{\alpha }{\lambda }({\overline{\sigma }}_h^n-{\overline{\sigma }}_h^{n,{\mathcal{l}}_n-1},{\bar{e}}_p^n{)}_{{\mathrm{\Omega }}_1}+{\int }_{{t}_{n-1}}^{{t}_n} (q(s)-{q}^n+\nabla \middot ({{z}}^n-{z}(s)),{\bar{e}}_p^n{)}_{{\mathrm{\Omega }}_1}\mathrm{d}s\right]. $$(107)

A comparison with (67) immediately shows that the conclusion of Proposition 4.2 holds with the same initial error E h 0 Mathematical equation: $ {\mathcal{E}}_h^0$ and slightly different interpolation error A ̃ h n Mathematical equation: $ {\stackrel{\tilde }{\mathcal{A}}}_h^n$, of the same order, and provided the solution and data are sufficiently smooth. For the sake of brevity the details are skipped, and (77) is replaced by 1 M ( | | e ¯ p n | | L 2 ( Ω 1 ) 2 + m = 1 n - 1 | | δ ( e ¯ p m ) | | L 2 ( Ω 1 ) 2 ) + G ( | | ε ( e u n ) | | L 2 ( Ω ) 2 + 2 m = 1 n | | ε ( δ ( e u m ) ) | | L 2 ( Ω ) 2 ) + λ 2 ( | | · ( e u n ) | | L 2 ( Ω ) 2 + 2 m = 1 n | | · ( δ ( e u m ) ) | | L 2 ( Ω ) 2 ) + ( 2 - γ ) μ f m = 1 n Δ t | | K - 1 2 e z m | | L 2 ( Ω 1 ) 2 1 M m = 1 n - 1 Δ t | | e ¯ p m | | L 2 ( Ω 1 ) 2 + G m = 1 n - 1 Δ t | | ε ( e u m ) | | L 2 ( Ω ) 2 + λ 2 m = 1 n - 1 Δ t | | · ( e u m ) | | L 2 ( Ω ) 2 + 5 M α 2 λ 2 1 Δ t m = 1 n | | σ ¯ h m - σ ¯ h m , l m - 1 | | L 2 ( Ω 1 ) 2 + E h 0 + A ̃ h n . Mathematical equation: $$ \begin{array}{ll}\frac{1}{M}& \left({||{\bar{e}}_p^n||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+\sum_{m=1}^{n-1} {||\delta ({\bar{e}}_p^m)||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2\right)+G\left({||{\epsilon }({e}_{{u}}^n)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+2\sum_{m=1}^n {||{\epsilon }(\delta \left({e}_{{u}}^m\right))||}_{{L}^2\left(\mathrm{\Omega }\right)}^2\right)\\ & +\frac{\lambda }{2}\left({||\nabla \middot \left({e}_{{u}}^n\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+2\sum_{m=1}^n {||\nabla \middot \left(\delta \left({e}_{{u}}^m\right)\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2\right)+\left(2-\gamma \right){\mu }_f\sum_{m=1}^n \Delta t{||{{K}}^{-\frac{1}{2}}{e}_{{z}}^m||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2\\ & \le \frac{1}{M}\sum_{m=1}^{n-1} \Delta t{||{\bar{e}}_p^m||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+G\sum_{m=1}^{n-1} \Delta t{||{\epsilon }\left({e}_{{u}}^m\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2+\frac{\lambda }{2}\sum_{m=1}^{n-1} \Delta t{||\nabla \middot \left({e}_{{u}}^m\right)||}_{{L}^2\left(\mathrm{\Omega }\right)}^2\\ & +5M\frac{{\alpha }^2}{{\lambda }^2}\frac{1}{\Delta t}\sum_{m=1}^n {||{\overline{\sigma }}_h^m-{\overline{\sigma }}_h^{m,{\mathcal{l}}_m-1}||}_{{L}^2\left({\mathrm{\Omega }}_1\right)}^2+{\mathcal{E}}_h^0+{\stackrel{\tilde }{\mathcal{A}}}_h^n.\end{array} $$(108)

From here, by comparing with the material of Section 4.4, we easily verify that the error of the mixed scheme has the same order as that of the continuous Galerkin scheme, provided the solution, including the Darcy velocity, is smooth enough. The sufficient condition on the number of iterations (81) is slightly improved. Owing to the gain of the 1 2 Mathematical equation: $ \frac{1}{2}$ factor mentioned above, it becomes m , 1 m n ,   l m L , where   1 ( β   λ ) L min ( ( 3 20 1 M Δ t α 2 β ) 1 2 , Δ t ) . Mathematical equation: $$ \forall m,1\le m\le n,\enspace {\mathcal{l}}_m\ge L,\hspace{0.5em}\mathrm{where}\enspace \frac{1}{(\beta \enspace \lambda {)}^L}\le \mathrm{min}\left({\left(\frac{3}{20}\frac{1}{M}\frac{\Delta t}{{\alpha }^2\beta }\right)}^{\frac{1}{2}},\Delta t\right). $$(109)

6 A numerical result

The problem considered here is that of flow to a rate specified injection well in a confined compressible aquifer of thickness H as shown in Figure 2. The analytical solution for the pore pressure in the pay-zone (or aquifer or flow domain) is given as (Verruijt [46]) p = Q μ f 4 π kH E 1 ( r 2 / 4 ct ) , Mathematical equation: $$ p=\frac{Q{\mu }_f}{4{\pi kH}}{E}_1({r}^2/4{ct}), $$(110)where k is the permeability, Q is the injection rate, H is the aquifer thickness, r is the radial coordinate measured from the center of the well, t is the time, E 1(x) is the exponential integral given by E 1 ( x ) = x exp ( - t ) t d t , Mathematical equation: $$ {E}_1(x)=\underset{x}{\overset{\mathrm{\infty }}{\int }} \frac{\mathrm{exp}(-t)}{t}\mathrm{d}t, $$(111)and c is the diffusivity coefficient given by c = k μ f ( K b + 4 G 3 ) α 2 + ( φ 0 c f + ( α - φ 0 ) ( 1 - α ) K b ) ( K b + 4 G 3 ) , Mathematical equation: $$ c=\frac{\frac{k}{{\mu }_f}({K}_{\mathrm{b}}+\frac{4G}{3})}{{\alpha }^2+({\phi }_0{c}_{\mathrm{f}}+\frac{(\alpha -{\phi }_0)(1-\alpha )}{{K}_{\mathrm{b}}})({K}_{\mathrm{b}}+\frac{4G}{3})}, $$where K b = E 3 ( 1 - 2 ν ) Mathematical equation: $ {K}_{\mathrm{b}}=\frac{E}{3(1-2\nu )}$ is the drained bulk modulus and G = E 2 ( 1 + ν ) Mathematical equation: $ G=\frac{E}{2(1+\nu )}$ is the shear modulus. The underlying assumptions in the development of (110) are that there are no horizontal deformations in the aquifer and that the total vertical stress remains constant during the development of the hydrological process. We employ the parameters given in Table 1. The flow domain (aquifer) is at a depth of 244 m with the mechanics domain extending all the way to the traction free surface. The aquifer thickness is 61 m. The lateral extents of both the flow and mechanics domains are 915 Mathematical equation: $ 915$ m. An underburden with a thickness of 61 Mathematical equation: $ 61$ m is also provided. No flow boundary conditions are imposed on the pay-zone. Gravity is ignored. Denoting the top surface of the mechanics domain as Γ T Mathematical equation: $ {\mathrm{\Gamma }}_T$, the boundary conditions for the mechanics subproblem are t = 0   on   Γ T , u · n = 0 on   Ω / Γ T . Mathematical equation: $$ \begin{array}{cc}{t}=\mathbf{0}\enspace & \mathrm{on}\enspace {\mathrm{\Gamma }}_T,\\ {u}\middot {n}=0& \mathrm{on}\enspace \mathrm{\partial \Omega }/{\mathrm{\Gamma }}_T.\end{array} $$

Thumbnail: Fig. 2 Refer to the following caption and surrounding text. Fig. 2

Schematic for single well in an infinite confined aquifer problem.

Table 1

Parameters for single well in an infinite confined acquifer problem.

The Biot parameter is non-zero only inside the pay-zone and zero outside the pay-zone and formally given as α = { 0.8 in   Ω 1 0 in   Ω 2 . Mathematical equation: $$ \alpha =\left\{\begin{array}{cc}0.8& \mathrm{in}\enspace {\mathrm{\Omega }}_1\\ 0& \mathrm{in}\enspace {\mathrm{\Omega }}_2.\end{array}\right. $$

Since for this computational example the term q Mathematical equation: $ q$ represents a well and is not in L ( L 2 ( Ω ) ) Mathematical equation: $ {L}^{\mathrm{\infty }}({L}^2(\mathrm{\Omega }))$, we compute estimates in L ( L 2 ( Ω * ) ) Mathematical equation: $ {L}^{\mathrm{\infty }}({L}^2({\mathrm{\Omega }}^{\mathrm{*}}))$ where Ω * = Ω - B R Mathematical equation: $ {\mathrm{\Omega }}^{\mathrm{*}}=\mathrm{\Omega }-{\mathcal{B}}_R$. Here B R Mathematical equation: $ {\mathcal{B}}_R$ is a cylinder of radius 92 Mathematical equation: $ 92$ m (which is 1 / 10 Mathematical equation: $ 1/10$ times the areal size of the domain) and height of the pay-zone. The error norm for the pore pressure in the pay-zone is computed using the midpoint quadrature rule: | | p - p h | | L 2 ( Ω * ) | | p | | L 2 ( Ω * ) L max 0 < τ T ( E T h Ω * | E | ( p ( τ , m e ) - p h ( τ , m e ) ) 2 E T h Ω * | E | ( p ( τ , m e ) ) 2 ) 1 2 , Mathematical equation: $$ {\Vert \frac{{||p-{p}_h||}_{{L}^2\left({\mathrm{\Omega }}^{\mathrm{*}}\right)}}{{||p||}_{{L}^2\left({\mathrm{\Omega }}^{\mathrm{*}}\right)}}\Vert }_{{L}^{\mathrm{\infty }}}\equiv \underset{0<\tau \le T}{\mathrm{max}}{\left(\frac{\sum_{E\in {\mathcal{T}}_h\cap {\mathrm{\Omega }}^{\mathrm{*}}} |E|(p(\tau,{m}_e)-{p}_h(\tau,{m}_e){)}^2}{\sum_{E\in {\mathcal{T}}_h\cap {\mathrm{\Omega }}^{\mathrm{*}}} |E|(p(\tau,{m}_e){)}^2}\right)}^{\frac{1}{2}}, $$(112)where m e is the center of mass of element E, τ is time, p(τ, m e ) is the analytical solution for pore pressure at time τ and position m e , p h (τ, m e ) is the numerical solution for pore pressure at m e and T is the total time. As shown in Tables 2 and 3, we observe first order convergence for the pore pressure. The simulation was performed using the in-house reservoir simulator IPARS (http://csm.ices.utexas.edu/IparsWeb/index.html) on the bevo3 supercomputer at the Institute for Computational Engineering and Sciences at the University of Texas at Austin. The flow system is solved using a multipoint flux mixed finite element method (Ingram et al. [47]) and the poromechanics system is solved using a conforming Galerkin method. The solver for both the flow and poromechanics systems is the parallel high performance preconditioners library called Hypre (Falgout and Yang [48]). The convergence tolerance is 1 × 10−8. The code takes 1–3 coupling iterations to convergence at every time step.

Table 2

Order of convergence of pore pressure solution with time step of 0.01 day.

Table 3

Order of convergence of pore pressure solution with time step of 0.005 day.

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All Tables

Table 1

Parameters for single well in an infinite confined acquifer problem.

Table 2

Order of convergence of pore pressure solution with time step of 0.01 day.

Table 3

Order of convergence of pore pressure solution with time step of 0.005 day.

All Figures

Thumbnail: Fig. 1 Refer to the following caption and surrounding text. Fig. 1

Pay-zone with surrounding rock.

In the text
Thumbnail: Fig. 2 Refer to the following caption and surrounding text. Fig. 2

Schematic for single well in an infinite confined aquifer problem.

In the text

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