Finite element method with the total stress variable for Biot’s consolidation model
Abstract
In this work, semi-discrete and fully-discrete error estimates are derived for the Biot’s consolidation model described using a three-field finite element formulation. The fields include displacements, total stress and pressure. The model is implemented using a backward Euler discretization in time for the fully-discrete scheme and validated for benchmark examples. Computational experiments presented verifies the convergence orders for the lowest order finite elements with discontinuous and continuous finite element appropriation for the total stress.
keywords:
Biot’s consolidation model, the total stress, error estimate, fully-discrete, lowest finite elements.AMS:
Primary 65N30; Secondary 65N501 Introduction
Biot’s fundamental equations for the soil consolidation process that describes the gradual adaptation of the soil to a load variation have been established in [1]. The mechanism of consolidation phenomenon described using a linear isotropic model is identical with the process of squeezing water out of an elastic porous medium in many cases. This solid-fluid coupling was extended to general anisotropy case in [2]. Such poroelasticity models have a lot applications in many areas including geomechanics [3], medicine [4], biomechanics [5], reservoir engineering [6]. The Biot’s consolidation models have also been used to combine transvascular and interstitial fluid movement with the mechanics of soft tissue in [7], which can be applied to improve drug delivery in solid tumors. Existence, uniqueness, and regularity theory were developed in [8] for poroelasticity and quasi-static problem in thermoelasticity. In [9], experiments with finite element method for the model in [7] have demonstrated the effects of fluid flow on the spatio-temporal patterns of soft-tissue elastic strain under a variety of physiological condition, which emphasized simulations relevant to a quasistatic elasticity imaging for the characterization of fluid flow in solid tumors.
Biot’s consolidation model has been considered by many researchers using finite element methods. In [10], a variational principle and the finite element method for a model with applications to a nonhomogeneous, anisotropic soil were developed. The fully discretization with backward Euler time discrete finite element method has been carried out and the existence and uniqueness were proved in [11]. Moreover, the simplest Taylor-Hood finite elements were employed. The stability and error estimates for the semi-discrete and fully-discrete finite element approximations were derived in [12] and [13]. Decay functions and post processing technique also were employed to improve the pore pressure accuracy. With the displacement and pore pressure fields as unknowns, the short and long time behavior of spatially discrete finite element solutions have been studied in [14]. Asymptotic error estimates have been derived for both stable and unstable combinations of the finite element spaces. For the coupled problem, a least squares mixed finite element method was presented and analyzed in [15] with the unknowns fluid displacement, stress tensor, flux, and pressure. In [16], coupling of mixed and continuous Galerkin finite element methods for pressure and displacements have been formulated deriving the convergence error estimates in time continuous setting. Methods for coupling mixed and discontinuous Galerkin have been presented in [17]. The error estimates for a fully-discrete stabilized discontinuous Galerkin method were obtained with the unknowns pressure and displacement in [18]. In [19], a discretization method in irregular domains with general grids for discontinuous full tensor permeabilities was developed. A new mixed finite element method for Biot’s consolidation problem in four variables was proposed in [20] and later, a three field mixed finite element which was free of pressure oscillations and Poisson locking has been proposed [21]. The priori error estimates that were robust for material parameters were provided in [22] with a four-field mixed method formulation. A three field finite element formulation with nonconforming finite element space for the displacements was considered in [23]. Based on the parameter dependent norms, the parameter-robust stability was established in [24], and parameter robust inf-sup stability and strong mass conservation were derived for three field mixed discontinuous Galerkin discretizations. A stabilized finite element method with equal order elements for the unknowns pressure and displacement was proposed in [25] to reduce the effects of non-physical oscillations. Combining the mixed method with symmetric interior penalty discontinuous Galerkin method obtained a H(div) conforming finite element method in [26]. The method achieved strong mass conservation.
Moreover, in [27], the total stress (or the soil pressure) expressed as a combination of the divergence of the velocity and pressure has been introduced coupling the solid and fluid robustly for Biot’s consolidation problem with the unknown displacement, pressure, and volumetric stress. Using a Fredholm argument for a static model, error estimates were derived independently of the Lam constants for both continuous and discrete formulations. A three field formulation of Biot’s model with the total stress variable has also been proposed in [28], which developed a parameter-robust block diagonal preconditioner for the associated discrete systems. Then, in [29], a priori error estimates for semi-discrete scheme has been presented by introducing the total pressure variable for quasi-static multiple-network poroelasticity equations. Our goal in this paper is to emphasize the time dependence of field variables in error estimates, so we choose to consider the fully-discrete scheme. Thus, using the total stress as a new variable for the three field formulation, we give the error estimates for semi-discrete and fully-discrete with backward Euler time discretization schemes.
Let be an open bounded polygonal or polyhedral domain in . Biot’s consolidation model is described as follows: Find the displacement vector and the fluid pressure in
(1) | ||||
(2) | ||||
(3) | ||||
(4) | ||||
(5) |
where and are disjoint closed subsets with and the Dirichlet boundary . Here, is the strain tensor expressed in terms of symmetrized gradient of displacements, is the permeability of the porous solid and parameters , are the elastic Lam constants. The right hand side term in (1) represents the density of the applied body forces, and the source term in (2) represents a forced fluid extraction or injection. The outward unit normal vector on is denoted by .
Next, we introduce the coupling between the solid and fluid using , where is the total stress, is the displacement and is the fluid pressure [27, 28]. This can be rewritten as
(6) |
For , the initial conditions are given by
(7) | ||||
Hence, the initial condition for the total stress is . Denote the spaces and .
Multiplying (1), (6) and (2) by test functions, integrating by parts and applying boundary conditions yield the following weak formulation: Find , , such that
(8) | ||||
In Section 2, we present the semi-discrete and fully-discrete finite element formulation for system (8) with the unknown displacement, total stress and pressure and prove uniqueness of the solution for each of these schemes. Section 3 presents the derivation and analysis of the error estimates for both the semi-discrete and fully-discrete schemes. In Section 4 we present computational experiments on benchmark problems that validate the theoretical convergence rates with respect to mesh size and time step .
In the paper, we denote the arbitrary constants by , where is positive integer and is a constant which is independent of time step and mesh size . Let be the space of polynomials of degree less than or equal to in all variables. Moreover, let be the norm in space and be the norm in space. Denote the space-time space by for a Banach space (see details in [34]).
2 Finite Element Discretization and Uniqueness
Let be a regular and quasi-uniform triangulation of domain into triangular or tetrahedron elements [30, 31]. For each element , is its diameter and is the mesh size of triangulation . We consider the following finite element spaces on ,
where In order to describe the initial conditions of discretization schemes, we define the following two projection operators. Let us define the Stokes projection and by
(9) | ||||
Also the elliptic projection is defined with the following properties,
(10) |
Hence, given a suitable approximation of initial conditions , and , the semi-discrete scheme corresponding to a three field formulation (8) is for all , to seek , , such that
(11) | ||||
To obtain a fully-discrete formulation, we denote time step by , and , where is non-negative integer. Thus, given a suitable approximation of initial conditions , and , the fully-discrete scheme with backward Euler time discretization corresponding to the three field formulation (8) is to find , , such that
(12) | ||||
where and .
Then, we present an inequality, which will be useful in the uniqueness and convergence analysis.
Theorem 2.
For each , the semi-discrete scheme (11) has a unique solution.
Proof.
We need to prove that the homogeneous problem of (11) has only the trivial solution. Taking the time derivative of the second equation in (11), the homogeneous problem is rewritten as seeking , , with , , such that
(14) | ||||
Using the test functions , and in (14) and simplifying, we can derive the following identity
Integrating the above identity over , one finds
Therefore, with the conditions , , , we have
Then, using Korn’s inequality from Lemma 1 when leads to . ∎
Theorem 3.
For , the fully-discrete scheme (12) has a unique solution.
Proof.
Similar to the semi-discrete, with , and , we rewrite the second equation of (12) and consider the homogeneous problem for fully-discrete scheme (12) is to find , , such that
(15) | ||||
Choosing , and , equation (15) can be simplified to
Here, we have used the inequality
Summing over from to , it follows that
Note that the assumptions , , , and using Korn’s inequality (13) from Lemma 1, we have , and . ∎
3 Error Estimates
In order to derive the error estimates, we first show the inf-sup condition for space pair with . Denote . For each , there exists satisfying and . Thus, we can deduce that for [35, 27]
Since not all the discrete finite element spaces meet the inf-sup condition, we assume that the space pair satisfy the inf-sup condition, i.e. there exists a positive constant such that for
(16) |
3.1 Error estimate for the semi-discrete scheme
For the semi-discrete scheme, we denote the error in displacement by , where and . Similarly, we decompose the errors of the total stress and pressure into two parts, respectively, i.e. and .
Theorem 4.
Proof.
Subtracting (11) from (8), and taking the derivative of the second equation with respect to time , we get
With the use of the definitions of projections (9) and (10), it follows
(19) | ||||
Taking , and , then we can deduce that
Next, integrating over , since and , we have
Using the Gronwall Lemma [34], one finds
(20) |
Now, to estimate , we deduce from the first equation of (19), for each
Thus, using the inf-sup condition (16), it follows that
(21) |
On the other hand, differentiating the first equation of (19) with respect to , it follows
Taking in the above identity and , in (19), we have
So we rewrite the above inequality as following
Integrating on , we have
(22) |
The proof is completed combining (20), (21), (22) with the definitions of errors. ∎
3.2 Error estimate for the fully-discrete scheme
Denote the error in displacement at time by . We define and in a similar fashion as .
Theorem 6.
Proof.
For each , using the definition of Stokes projection (9), we have
Combining the above identity with the first equation of (12) yields
(25) |
For each , taking into account the derivative of the second equation in (8) with respect to time and (9), one obtains
Rewriting the second term of (12) as and substituting it into the above identity lead to
(26) | ||||
For each , the definition of elliptic projection (10) and third equation of (8) imply that
Therefore, by employing the third equation of (12), one finds
(27) | ||||
To proceed our analysis, taking , and in (25), (26) and (27) respectively, we have
Note that, using Cauchy–Schwarz inequality and Poincar inequality, it follows
where are positive constants. Here, we take into account the following inequalities,
Choosing , , then we can reformulate the above inequality as
where we use the estimate
Then, adding from to , we get
Using discrete Gronwall Lemma [34], we deduce
(28) | ||||
Note that follows from (26) and (16), therefore, it leads to the error estimates (23).
3.3 Applying to lower-order finite elements
In this subsection, we discuss two lowest order finite element approximation by considering the finite element space for the total stress to be continuous and discontinuous, then we present the error estimates of them.
3.3.1 Finite elements with discontinuous total stress for ,
Consider the spaces,
The inf-sup condtition (16) for the space pair is known [36]. With the use of the properties of Stokes projection (see Lemma 3.1 in [14]), it follows
Hence, combining the above inequality with properties of elliptic projection [34], the error estimates of semi-discrete scheme in Theorem 4 with elements can be rewritten as follows.
Theorem 7.
Similarly, we rewrite the error estimates of the fully-discrete scheme in Theorem 6 with elements.
3.3.2 Lowest Taylor-Hood elements with the continuous total stress are chosen for
Consider the spaces,
It is well known that the space pair satisfies the inf-sup condition (16) (see [35]). With the use of the properties of stoke projection (see Lemma 3.1 in [14]), it follows
The convergence orders for the fully-discrete scheme with elements will be verified in numerical examples. Theorem 6 is rewritten as follows.
Theorem 9.
Remark 1.
Remark 2.
The results for the lowest Taylor-Hood finite elements in Theorem 9 can be extended to higher orders elements directly with the properties of the stokes projection and elliptic projection. In general, the convergence in Theorem 8 and Theorem 9 can be extended to many finite elements spaces pairs which satisfy the inf-sup conditions (16) with the properties of projections.
4 Numerical experiments
The numerical examples are presented to confirm our convergence orders with respect to mesh size and time step for elements and elements for the benchmark problems. Let us define the linear Lagrange interpolation for pressure by . For simplicity, we still denote the error between linear Lagrange interpolation and numerical solutions by in the following tables. The error estimates are divided into two parts, i.e.
Note that, we can obtain the convergence orders for as based on the properties of Lagrange interpolation [34]. The errors for and are defined in a similar way. We denote the error in energy norm for the displacement by . For the square domain, the uniform triangular mesh is employed, and Figure 1 shows the computational grid with the meshes.


Example 1.
Let the domain be and . Then, we choose the Dirichlet boundary and the exact solutions
and
The body force function , the forced fluid , initial conditions and Dirichlet boundary conditions are determined by the exact solutions. We obtain
We set the parameters , and in this example. Table 1 gives the error estimates with respect to for elements. The convergence orders for each variable are consistent with our theory. Table 2 shows the convergence orders with elements, which are in agreements with our results in Theorem 9. Furthermore, the convergence orders with respect to can be observed in Table 3 and Table 4.
Moreover, the convergence orders for the pressure are computed to be in Table 1 and Table 2, so we can obtain convergence results for due to the properties of the linear Lagrange interpolation. A similar argument can be employed for the pressure in norm as well. In particular, the convergence orders of for the displacement and the pressure in norm can be observed in Tables 1 and 2.
h | ||||||||||
---|---|---|---|---|---|---|---|---|---|---|
error | order | error | order | error | order | error | order | error | order | |
1/8 | 1.2572e-02 | 4.1887e-04 | 1.0502e-02 | 7.8321e-02 | 1.6727e-02 | |||||
1/16 | 5.7283e-03 | 1.1340 | 9.7376e-05 | 2.1048 | 2.5910e-03 | 2.0190 | 1.9241e-02 | 2.0252 | 4.1523e-03 | 2.0101 |
1/32 | 2.8055e-03 | 1.0298 | 2.3932e-05 | 2.0246 | 6.4557e-04 | 2.0048 | 4.7886e-03 | 2.0065 | 1.0362e-03 | 2.0026 |
1/64 | 1.3961e-03 | 1.0068 | 5.9561e-06 | 2.0065 | 1.6128e-04 | 2.0010 | 1.1959e-03 | 2.0015 | 2.5896e-04 | 2.0005 |
h | ||||||||||
---|---|---|---|---|---|---|---|---|---|---|
error | order | error | order | error | order | error | order | error | order | |
1/8 | 3.8777e-03 | 3.0217e-04 | 2.8315e-03 | 1.0661e-02 | 2.3541e-03 | |||||
1/16 | 6.8421e-04 | 2.5026 | 7.7262e-05 | 1.9675 | 7.2470e-04 | 1.9661 | 2.6829e-03 | 1.9904 | 6.0092e-04 | 1.9699 |
1/32 | 1.4486e-04 | 2.2397 | 1.9575e-05 | 1.9807 | 1.8225e-04 | 1.9914 | 6.7188e-04 | 1.9975 | 1.5103e-04 | 1.9923 |
1/64 | 3.4293e-05 | 2.0786 | 4.9123e-06 | 1.9945 | 4.5631e-05 | 1.9978 | 1.6804e-04 | 1.9993 | 3.7807e-05 | 1.9981 |
error | order | error | order | error | order | error | order | |||
---|---|---|---|---|---|---|---|---|---|---|
1 | 3.8459e-03 | 2.4103e-03 | 1.5573e-01 | 3.3603e-01 | 1.5887e-01 | |||||
1/2 | 1.9797e-03 | 0.9580 | 1.2156e-03 | 0.9875 | 7.8538e-02 | 0.9875 | 1.6971e-01 | 0.9855 | 8.0238e-02 | 0.9854 |
1/4 | 1.0634e-03 | 0.8965 | 6.0752e-04 | 1.0006 | 3.9277e-02 | 0.9997 | 8.5072e-02 | 0.9963 | 4.0241e-02 | 0.9956 |
1/8 | 6.5722e-04 | 0.6942 | 3.0332e-04 | 1.0020 | 1.9639e-02 | 0.9999 | 4.2737e-02 | 0.9931 | 2.0245e-02 | 0.9911 |
error | order | error | order | error | order | error | order | |||
---|---|---|---|---|---|---|---|---|---|---|
1 | 1.2052e-02 | 1.7118e-03 | 2.9200e-02 | 2.7565e-01 | 2.9310e-02 | |||||
1/2 | 6.0467e-03 | 0.9950 | 8.5831e-04 | 0.9959 | 1.4653e-02 | 0.9947 | 1.3831e-01 | 0.9949 | 1.4713e-02 | 0.9943 |
1/4 | 3.0175e-03 | 1.0027 | 4.2802e-04 | 1.0038 | 7.3185e-03 | 1.0015 | 6.9128e-02 | 1.0005 | 7.3538e-03 | 1.0005 |
1/8 | 1.5027e-03 | 1.0057 | 2.1286e-04 | 1.0077 | 3.6508e-03 | 1.0033 | 3.4532e-02 | 1.0013 | 3.6736e-03 | 1.0012 |
Example 2.
We consider the problem as in Example 1 with Neumann and Dirichlet boundary conditions. Let the Neumann boundary be and the Dirichlet boundary .
We also set the parameters , and as in Example 1. With the Neumann and Dirichlet boundary conditions, we observe the convergence orders in energy norm of the displacement in Table 5 and Table 6 which are in full agreements with our main results in Theorem 8 and Theorem 9. The convergence orders for the total stress in norm are recorded in Table 5 and Table 6 which confirm our theory.
h | ||||||||||
---|---|---|---|---|---|---|---|---|---|---|
error | order | error | order | error | order | error | order | error | order | |
1/8 | 1.4182e-02 | 1.7411e-03 | 1.2276e-02 | 8.0666e-02 | 1.8625e-02 | |||||
1/16 | 5.9152e-03 | 1.2615 | 4.1226e-04 | 2.0783 | 3.0872e-03 | 1.9914 | 2.0045e-02 | 2.0087 | 4.6735e-03 | 1.9946 |
1/32 | 2.8262e-03 | 1.0655 | 9.9754e-05 | 2.0471 | 7.6655e-04 | 2.0098 | 4.9844e-03 | 2.0077 | 1.1632e-03 | 2.0064 |
1/64 | 1.3985e-03 | 1.0149 | 2.4612e-05 | 2.0190 | 1.9134e-04 | 2.0022 | 1.2446e-03 | 2.0017 | 2.9050e-04 | 2.0014 |
h | ||||||||||
---|---|---|---|---|---|---|---|---|---|---|
error | order | error | order | error | order | error | order | error | order | |
1/8 | 6.0055e-03 | 6.2900e-04 | 2.5456e-03 | 1.5738e-02 | 2.2821e-03 | |||||
1/16 | 1.1116e-03 | 2.4336 | 1.6328e-04 | 1.9457 | 6.5647e-04 | 1.9914 | 3.9863e-03 | 1.9811 | 5.8439e-04 | 1.9653 |
1/32 | 2.2324e-04 | 2.3159 | 4.1244e-05 | 1.9850 | 1.6542e-04 | 2.0098 | 9.9993e-04 | 1.9951 | 1.4701e-04 | 1.9910 |
1/64 | 4.8554e-05 | 2.2009 | 1.0324e-05 | 1.9981 | 4.1437e-05 | 2.0022 | 2.5020e-04 | 1.9987 | 3.6809e-05 | 1.9977 |
Example 3.
Let the domain be and . The Dirichlet boundary satisfy . Then, we choose the exact solutions
and
We choose the body force function , forced fluid , initial conditions and Dirichlet boundary conditions so that the exact solutions satisfy the problems (1) and (2) . Note that , and when the elastic Lam parameters , we have .
We set the parameters , and with nearly incompressible case. We test both and elements to emphasize the efficiency. Thus, Table 7 and Table 8 show the convergence orders for each variable as expected. At the same time, the convergence orders for the total stress are shown in Table 7, and we can observe that the convergence orders of displacement are in Table 8 which is better than expected. Therefore, we can conclude that the finite element method is valid for the nearly incompressible case.
h | ||||||||||
---|---|---|---|---|---|---|---|---|---|---|
error | order | error | order | error | order | error | order | error | order | |
1/8 | 4.8359e-02 | 1.1460e-03 | 1.0101e-02 | 1.0998e-02 | 2.3094e-03 | |||||
1/16 | 1.9701e-02 | 1.2955 | 2.0102e-04 | 2.5111 | 2.6388e-03 | 1.9365 | 2.8017e-03 | 1.9728 | 5.9488e-04 | 1.9568 |
1/32 | 9.7854e-03 | 1.0095 | 4.9100e-05 | 2.0335 | 7.3649e-04 | 1.8411 | 7.0387e-04 | 1.9929 | 1.4987e-04 | 1.9888 |
1/64 | 4.9240e-03 | 0.9908 | 1.2386e-05 | 1.9870 | 2.1109e-04 | 1.8028 | 1.7619e-04 | 1.9981 | 3.7540e-05 | 1.9972 |
h | ||||||||||
---|---|---|---|---|---|---|---|---|---|---|
error | order | error | order | error | order | error | order | error | order | |
1/8 | 3.0635e-02 | 9.8803e-04 | 1.7083e-02 | 1.0998e-02 | 2.3094e-03 | |||||
1/16 | 4.3311e-03 | 2.8223 | 6.9922e-05 | 3.8207 | 3.0093e-03 | 2.5050 | 2.8017e-03 | 1.9728 | 5.9488e-04 | 1.9568 |
1/32 | 5.6515e-04 | 2.9380 | 4.5564e-06 | 3.9397 | 7.0999e-04 | 2.0835 | 7.0388e-04 | 1.9929 | 1.4987e-04 | 1.9888 |
1/64 | 7.1810e-05 | 2.9763 | 2.8910e-07 | 3.9782 | 1.7635e-04 | 2.0093 | 1.7619e-04 | 1.9981 | 3.7540e-05 | 1.9972 |
Example 4.
We consider Example 3 with non-homogeneous Dirichlet boundary conditions. Let the domain be and . The Dirichlet boundary satisfy . Then, we choose the exact solutions
and
Again, we choose the body force function , forced fluid , initial conditions and Dirichlet boundary conditions so that the exact solutions satisfy the problems (1) and (2) . Note that , and when the elastic Lam parameters , we have .
We also set the parameters , and . The results in Table 9 and Table 10 verify our theory for the case with non-homogeneous Dirichlet boundary conditions.
h | ||||||||||
---|---|---|---|---|---|---|---|---|---|---|
error | order | error | order | error | order | error | order | error | order | |
1/8 | 2.5465e-03 | 5.9338e-05 | 1.1059e-03 | . | 1.6621e-04 | 3.6140e-05 | ||||
1/16 | 1.3791e-03 | 0.8847 | 1.7079e-05 | 1.7967 | 3.4468e-04 | 1.6818 | 4.2208e-05 | 1.9774 | 9.2862e-06 | 1.9604 |
1/32 | 7.1729e-04 | 0.9430 | 4.6074e-06 | 1.8901 | 1.0408e-04 | 1.7275 | 1.0556e-05 | 1.9994 | 2.3293e-06 | 1.9951 |
1/64 | 3.6553e-04 | 0.9725 | 1.1977e-06 | 1.9436 | 3.0911e-05 | 1.7515 | 2.6206e-06 | 2.0100 | 5.7865e-07 | 2.0091 |
h | ||||||||||
---|---|---|---|---|---|---|---|---|---|---|
error | order | error | order | error | order | error | order | error | order | |
1/8 | 2.8381e-04 | 9.5582e-06 | 4.3295e-04 | 1.6621e-04 | 3.6141e-05 | |||||
1/16 | 3.8805e-05 | 2.8706 | 6.4511e-07 | 3.8891 | 1.0424e-04 | 2.0542 | 4.2209e-05 | 1.9773 | 9.2864e-06 | 1.9604 |
1/32 | 5.0463e-06 | 2.9429 | 4.1637e-08 | 3.9536 | 2.5944e-05 | 2.0064 | 1.0556e-05 | 1.9994 | 2.3293e-06 | 1.9952 |
1/64 | 6.4255e-07 | 2.9733 | 2.6417e-09 | 3.9783 | 6.4796e-06 | 2.0014 | 2.6206e-06 | 2.0100 | 5.7866e-07 | 2.0091 |
5 Conclusions
For Biot’s consolidation model, we analyze the error estimates for a three field discretization. And the total stress coupling between the solid and fluid variable is as an unknown. Moreover, the convergence of fully-discrete scheme is presented and the results can be extended to many finite element spaces that satisfy the inf-sup conditions.
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