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Publicly Available Published by De Gruyter November 10, 2016

Stabilized Mixed Finite Element Methods for Linear Elasticity on Simplicial Grids in ℝn

  • Long Chen , Jun Hu and Xuehai Huang EMAIL logo

Abstract

In this paper, we design two classes of stabilized mixed finite element methods for linear elasticity on simplicial grids. In the first class of elements, we use 𝑯(div,Ω;𝕊)-Pk and 𝑳2(Ω;n)-Pk-1 to approximate the stress and displacement spaces, respectively, for 1kn, and employ a stabilization technique in terms of the jump of the discrete displacement over the edges/faces of the triangulation under consideration; in the second class of elements, we use 𝑯01(Ω;n)-Pk to approximate the displacement space for 1kn, and adopt the stabilization technique suggested by Brezzi, Fortin, and Marini [19]. We establish the discrete inf-sup conditions, and consequently present the a priori error analysis for them. The main ingredient for the analysis are two special interpolation operators, which can be constructed using a crucial 𝑯(div) bubble function space of polynomials on each element. The feature of these methods is the low number of global degrees of freedom in the lowest order case. We present some numerical results to demonstrate the theoretical estimates.

1 Introduction

Assume that Ωn is a bounded polytope. Denote by 𝕊 the space of all symmetric n×n tensors. The Hellinger–Reissner mixed formulation of the linear elasticity under the load 𝒇𝑳2(Ω;n) is given as follows: Find (𝝈,𝒖)𝚺×𝑽:=𝑯(div,Ω;𝕊)×𝑳2(Ω;n) such that

(1.1)a(𝝈,𝝉)+b(𝝉,𝒖)=0for all 𝝉𝚺,
(1.2)-b(𝝈,𝒗)=Ω𝒇𝒗dxfor all 𝒗𝑽,

where

a(𝝈,𝝉):=Ω𝒜𝝈:𝝉dx,b(𝝉,𝒗):=Ωdiv𝝉𝒗dx

with 𝒜 being the compliance tensor of fourth order defined by

𝒜𝝈:=12μ(𝝈-λnλ+2μ(tr𝝈)𝜹).

Here 𝜹:=(δij)n×n is the Kronecker tensor, tr is the trace operator, and positive constants λ and μ are the Lamé constants. It is arduous to design 𝑯(div,Ω;𝕊) conforming finite element with polynomial shape functions due to the symmetry requirement of the stress tensor. Hence composite elements were one main choice to approximate the stress in the last century (cf. [7, 30, 46, 56]).

In the early years of this century, Arnold and Winther constructed the first 𝑯(div,Ω;𝕊) conforming mixed finite element with polynomial shape functions in two dimensions in [10], which was extended to tetrahedral grids in three dimensions in [1, 4] and simplicial grids in any dimension in [42]. In those elements, the displacement space is approximated by 𝑳2(Ω;n)-Pk-1 while the stress space is approximated by the space of functions in 𝑯(div,Ω;𝕊)-Pk+n-1 whose divergence is in 𝑳2(Ω;n)-Pk-1 for k2. Recently, Hu and Zhang showed that the more compact pair of 𝑯(div,Ω;𝕊)-Pk and 𝑳2(Ω;n)-Pk-1 spaces is stable on triangular and tetrahedral grids for kn+1 with n=2,3 in [40, 41]. And Hu generalized those stable finite elements to simplicial grids in any dimension for kn+1 in [37]. One key observation there is that the divergence space of the 𝑯(div) bubble function space of polynomials on each element is just the orthogonal complement space of the piecewise rigid motion space with respect to the discrete displacement space. Then the discrete inf-sup condition was proved for kn+1 through controlling the piecewise rigid motion space by 𝑯1(Ω;𝕊)-Pk space. It is, however, troublesome to prove that the pair of 𝑯(div,Ω;𝕊)-Pk and 𝑳2(Ω;n)-Pk-1 is still stable for 1kn. For such a reason, Hu and Zhang enriched the 𝑯(div,Ω;𝕊)-Pk space with 𝑯(div,Ω;𝕊)-Pn+1 face-bubble functions of piecewise polynomials for each n-1 dimensional simplex in [42]. Gong, Wu and Xu constructed two types of interior penalty mixed finite element methods by using nonconforming symmetric stress approximation in [31]. The stability of those nonconforming mixed methods is ensured by 𝑯(div) nonconforming face-bubble spaces. An interior penalty mixed finite element method using Crouzeix–Raviart nonconforming linear element to approximate the stress was studied in [21]. To get rid of the vertex degrees of freedom appeared in the 𝑯(div,Ω;𝕊)-conforming elements and make the resulting mixed finite element methods hybridizable, nonconforming mixed elements on triangular and tetrahedral grids were developed in [11, 5, 32, 57]. On rectangular grids, we refer to [3, 36, 38, 12, 23] for symmetric conforming mixed finite elements and [39, 47, 58, 59] for symmetric nonconforming mixed finite elements. For keeping the symmetry of the discrete stress space and relaxing the continuity across the interior faces of the triangulation, many discontinuous Galerkin methods were proposed in [20, 27, 24, 43, 44, 45], hybridizable discontinuous Galerkin methods in [51, 35], weak Galerkin methods in [55, 22], hybrid high-order method in [29]. For the weakly symmetric mixed finite element methods for linear elasticity, we refer to [2, 6, 53, 48, 8, 15, 49, 26, 34, 50, 33, 28, 9].

In this paper, we intend to design stable mixed finite element methods for the linear elasticity using as few global degrees of freedom as possible. To this end, two classes of stabilized mixed finite element methods on simplicial grids in any dimension are proposed. In the first one, we use the pair of 𝑯(div,Ω;𝕊)-Pk and 𝑳2(Ω;n)-Pk-1 constructed in [37] to approximate the stress and displacement for 1kn. To simplify the notation, we shall use superscript ()div for 𝑯(div,Ω;𝕊) conforming elements, ()-1 for discontinuous elements, and ()0 for 𝑯1(Ω;n) or 𝑯1(Ω;𝕊) continuous elements. Instead of enriching Pkdiv elements with face bubble functions of piecewise polynomials as in [42, 31], we include a jump stabilization term into the Hellinger–Reissner mixed formulation to make the discrete method stable, inspired by the discontinuous Galerkin methods constructed in [24] for the linear elasticity problem. The discrete inf-sup condition in a compact form is established with the help of a partial inf-sup condition (2.1) estabilished in [37, 40, 41] and a well-tailored interpolation operator for the stress. Then we show the a priori error analysis for the resulting stabilized Pkdiv-Pk-1-1 elements.

In the second class of stabilized mixed finite element methods, we adopt the stabilization technique suggested in [19] and use 𝑯01(Ω;n)-Pk to approximate the displacement space. The merit of this stabilization technique is that the coercivity condition for the bilinear form related to the stress holds automatically, thus we only need to focus on the discrete inf-sup condition. To recover the inf-sup condition, we first employ 𝑯1(Ω;𝕊)-Pk enriched with (k+1)-st order 𝑯(div) bubble function space of polynomials on each element to approximate the stress space. The discrete inf-sup condition is established by using another special interpolation operator for the stress. The a priori error estimate for the (Pk0+Bk+1div)-Pk0 is then derived by the standard theory of mixed finite element methods. The rate of convergence for the displacement in 𝑳2(Ω;n) norm is, however, suboptimal due to the coupling of stress error measured in 𝑯(div)-norm. To remedy this, we use 𝑯(div,Ω;𝕊)-Pk+1 to approximate the stress space instead. The resulting stable finite element pair is the Hood–Taylor type Pk+1div-Pk0. It was mentioned in [19] that it is not known if the Hood–Taylor element in [54, 13, 14] is stable for the linear elasticity. We solve this problem by enriching the Hood–Taylor element space Pk+10 for the stress with the same degree of 𝑯(div) bubble function space of polynomials on each element.

Note that the key component in constructing the previous two interpolation operators is the 𝑯(div) bubble function space of polynomials on each element. We would like to mention that for the stress we obtain the optimal error estimates in 𝑯(div,Ω;𝕊) norm, whereas these error estimates in 𝑳2(Ω;𝕊) norm are suboptimal. To the best of our knowledge, the global degrees of freedom of our methods for the lowest order case k=1 are fewer than those of any existing mixed-type symmetric finite element method for the linear elasticity in the literature. To be specific, the global degrees of freedom for the stress and the displacement for the stabilized mixed finite element methods (3.1)–(3.2), (4.1)–(4.2) and (4.9)–(4.10) with k=1 are, respectively,

n(n+1)2|𝒱|+n|𝒯|,n(n+1)2(|𝒱|+|𝒯|)+n|𝒱|,n(n+1)2|𝒱|+(n-1)(n+2)2||+n(n+1)2|𝒯|+n|𝒱|.

Here |𝒱|,||,|𝒯| are the numbers of vertices, edges and elements of the triangulation.

When adopting the same degree of polynomial spaces for displacement, the Hood–Taylor type elements Pk+1div-Pk0 and the stabilized elements Pk+1div-Pk-1 share the same convergence rate, which is one order higher than the stabilized elements (Pk0+Bk+1div)-Pk0. It is worth mentioning that to keep the same convergence rate, the stabilized elements Pk+1div-Pk-1 need larger global degrees of freedom than the Hood–Taylor type elements Pk+1div-Pk0.

The rest of this article is organized as follows. We present some notations and definitions in Section 2 for later uses. In Section 3, a stabilized mixed finite element method with discontinuous displacement for the linear elasticity is designed and analyzed. Then we propose a second class of stabilized mixed finite element methods with continuous displacement for the linear elasticity in Section 4. In Section 5, some numerical experiments are given to demonstrate the theoretical results.

2 Preliminaries

Given a bounded domain Gn and a non-negative integer m, let Hm(G) be the usual Sobolev space of functions on G, and 𝑯m(G;𝕏) the usual Sobolev space of functions taking values in the finite-dimensional vector space 𝕏 for 𝕏 being 𝕊 or n. The corresponding norm and seminorm are denoted respectively by m,G and ||m,G. If G is Ω, we abbreviate them by m and ||m, respectively. Let 𝑯0m(G;n) be the closure of 𝑪0(G;n) with respect to the norm m,G. Denote by 𝑯(div,G;𝕊) the Sobolev space of square-integrable symmetric tensor fields with square-integrable divergence. For any 𝝉𝑯(div,Ω;𝕊), we equip the norm

𝝉𝑯(div,𝒜)2:=a(𝝉,𝝉)+div𝝉02.

When 𝝉𝑯(div,Ω;𝕊) satisfying Ωtr𝝉dx=0, it follows from [16, Proposition 9.1.1] that there exists a constant C>0 such that

𝝉0C𝝉𝑯(div,𝒜),

which means 𝝉𝑯(div,𝒜) and 𝝉𝑯(div) are equivalent uniformly with respect to the Lamé constant λ. Hence the norm 𝑯(div,𝒜) presented in all of the estimates in this paper can be replaced by the norm 𝑯(div).

Suppose the domain Ω is subdivided by a family of shape regular simplicial grids 𝒯h (cf. [17, 25]) with h:=maxK𝒯hhK and hK:=diam(K). Let h be the union of all n-1 dimensional faces of 𝒯h. For any Fh, denote by hF its diameter. Let Pm(G) stand for the set of all polynomials in G with the total degree no more than m, and 𝑷m(G;𝕏) denote the tensor or vector version of Pm(G) for 𝕏 being 𝕊 or n, respectively. Throughout this paper, we also use “” to mean that “C”, where C is a generic positive constant independent of h and the Lamé constant λ, which may take different values at different appearances.

Consider two adjacent simplices K+ and K- sharing an interior face F. Denote by 𝝂+ and 𝝂- the unit outward normals to the common face F of the simplices K+ and K-, respectively. For a vector-valued function 𝒘, write 𝒘+:=𝒘|K+ and 𝒘-:=𝒘|K-. Then define a matrix-valued jump as

𝒘:=12(𝒘+(𝝂+)T+𝝂+(𝒘+)T+𝒘-(𝝂-)T+𝝂-(𝒘-)T).

On a face F lying on the boundary Ω, the above term is defined by

𝒘:=12(𝒘𝝂T+𝝂𝒘T).

For each K𝒯h, define an 𝑯(div,K;𝕊) bubble function space of polynomials of degree k as

𝑩K,k:={𝝉𝑷k(K;𝕊):𝝉𝝂|K=}.

It is easy to check that 𝑩K,1 is merely the zero space. Denote the vertices of simplex K by 𝒙0,,𝒙n. For any edge 𝒙i𝒙j (ij) of element K, let 𝒕i,j be the associated tangent vectors and

𝑻i,j:=𝒕i,j𝒕i,jT,0i<jn.

It follows from [37] that, for k2,

𝑩K,k=0i<jnλiλjPk-2(K)𝑻i,j,

where λi are the associated barycentric coordinates corresponding to 𝒙i for i=0,,n. Some global finite element spaces are given by

𝑩k,h:={𝝉𝑯(div,Ω;𝕊):𝝉|K𝑩K,k for all K𝒯h},
𝚺~k,h:={𝝉𝑯1(Ω;𝕊):𝝉|K𝑷k(K;𝕊) for all K𝒯h},
𝚺k,h:=𝚺~k,h+𝑩k,h,
𝑽k-1,h:={𝒗𝑳2(Ω;n):𝒗|K𝑷k-1(K;n) for all K𝒯h},

with integer k1. It follows from [37, 40, 41] that

(2.1)𝑹(K)=div𝑩K,kfor all K𝒯h,

where the local rigid motion space and its orthogonal complement space with respect to 𝑷k-1(K;n) on each simplex K𝒯h are defined as (cf. [37])

𝑹(K):={𝒗𝑯1(K;n):𝜺(𝒗)=},
𝑹(K):={𝒗𝑷k-1(K;n):K𝒗𝒘dx=0 for all 𝒘𝑹(K)},

with 𝜺(𝒗):=(𝒗+(𝒗)T)/2 being the linearized strain tensor.

To introduce an elementwise 𝑯(div) bubble function interpolation operator, we first present the degrees of freedom for 𝚺k,h which are slightly different from those given in [37]. For the ease of notation, we understand Pk= for negative integers k.

Lemma 2.1

A matrix field 𝛕𝐏k(K;S) can be uniquely determined by the following degrees of freedom:

  1. for each dimensional simplex Δ of K, 0n-1, with linearly independent tangential vectors 𝒕1,,𝒕, and n- linearly independent normal vectors 𝝂1,,𝝂n-, the mean moments of degree at most k--1 over Δ, of 𝒕lT𝝉𝝂i, 𝝂iT𝝉𝝂j, l=1,,, i,j=1,,n-;

  2. the values K𝝉:𝝇dx for any 𝝇𝑷k-2(K;𝕊).

Proof.

This lemma can be proved by applying the arguments used in [37, Theorems 2.1, 2.2]. ∎

It is easy to see that we have the same first set of degrees of freedom as those in [37], whereas the second set of degrees of freedom is different.

Now we present an elementwise 𝑯(div) bubble function interpolation operator. Given 𝝉𝑳2(Ω;𝕊), define 𝑰k,hb𝝉𝚺k,h as follows: on each simplex K𝒯h,

  1. for any degree of freedom D in the first set of degrees of freedom in Lemma 2.1,

    D(𝑰k,hb𝝉)=0,
  2. for any 𝝇𝑷k-2(K;𝕊),

    (2.2)K𝑰k,hb𝝉:𝝇dx=K𝝉:𝝇dx.

Since the first set of degrees of freedom in Lemma 2.1 completely determines 𝝉𝝂 on K for any 𝝉𝑷k(K;𝕊) (cf. [37, Theorem 2.1]), thus 𝑰k,hb𝝉𝑩k,h. Applying a scaling argument, we have, for any 𝝉𝑳2(Ω;𝕊),

(2.3)𝑰k,hb𝝉0,K𝝉0,Kfor all K𝒯h.

3 A Stabilized Mixed Finite Element Method with Discontinuous Displacement

In this section, we devise a stabilized mixed finite element method for linear elasticity. In [37], the pair of 𝑯(div,Ω;𝕊)-Pk and 𝑳2(Ω;n)-Pk-1 is shown to be stable for kn+1. Here we consider the range 1kn.

With previous preparation, a stabilized mixed finite element method for linear elasticity is defined as follows: Find (𝝈h,𝒖h)𝚺k,h×𝑽k-1,h such that

(3.1)a(𝝈h,𝝉h)+b(𝝉h,𝒖h)=0for all 𝝉h𝚺k,h,
(3.2)-b(𝝈h,𝒗h)+c(𝒖h,𝒗h)=Ω𝒇𝒗hdxfor all 𝒗h𝑽k-1,h,

where the jump stabilization term for the displacement is

c(𝒖h,𝒗h):=FhhFF𝒖h:𝒗hds.

With this jump stabilization term, a jump seminorm for 𝑽k-1,h+𝑯1(Ω;n) is defined as

𝒗hc2:=c(𝒗h,𝒗h)for all 𝒗h𝑽k-1,h+𝑯1(Ω;n).

We also define the following two norms:

𝝉a2:=a(𝝉,𝝉)for all 𝝉𝑳2(Ω;𝕊),
𝒗h0,c2:=𝒗h02+𝒗hc2for all 𝒗h𝑽k-1,h+𝑯1(Ω;n).

Let 𝑸h be the L2 orthogonal projection from 𝑳2(Ω;n) onto 𝑽k-1,h. The following error estimate holds (cf. [25, 17]):

𝒗-𝑸h𝒗0,K+hK1/2𝒗-𝑸h𝒗0,KhKmin{k,m}|𝒗|m,Kfor all 𝒗𝑯m(Ω;n)

with integer m1. Let 𝑰hSZ be a tensorial or vectorial Scott–Zhang interpolation operator designed in [52], which possesses the following error estimate:

(3.3)K𝒯hhK-2𝝉-𝑰hSZ𝝉0,K2+|𝝉-𝑰hSZ𝝉|12h2min{k,m-1}𝝉m2

for any 𝝉𝑯m(Ω;𝕊) with integer m1. Then for each 𝝉𝑯1(Ω;𝕊), define

𝑰h𝝉:=𝑰hSZ𝝉+𝑰k,hb(𝝉-𝑰hSZ𝝉).

Apparently we have 𝑰h𝝉𝚺k,h. And it follows from (2.2) that

(3.4)K(𝑰h𝝉-𝝉):𝝇dx=0for all 𝝇𝑷k-2(K;𝕊) and K𝒯h.
Lemma 3.1

Given integers m,k1, we have, for any 𝛕𝐇m(Ω;S),

(3.5)K𝒯hhK-2(𝝉-𝑰h𝝉0,K2+hK𝝉-𝑰h𝝉0,K2)h2min{k,m-1}𝝉m2.

Proof.

According to the triangle inequality and (2.3), it holds

𝝉-𝑰h𝝉0,K𝝉-𝑰hSZ𝝉0,K+𝑰k,hb(𝝉-𝑰hSZ𝝉)0,K𝝉-𝑰hSZ𝝉0,K.

Analogously, from the triangle inequality, the inverse inequality, the trace inequality and (2.3) we obtain

hK1/2𝝉-𝑰h𝝉0,KhK1/2𝝉-𝑰hSZ𝝉0,K+hK1/2𝑰k,hb(𝝉-𝑰hSZ𝝉)0,K
hK1/2𝝉-𝑰hSZ𝝉0,K+𝑰k,hb(𝝉-𝑰hSZ𝝉)0,K
𝝉-𝑰hSZ𝝉0,K+hK|𝝉-𝑰hSZ𝝉|1,K.

Thus the combination of the last two inequalities and (3.3) implies (3.5). ∎

To derive a discrete inf-sup condition for the stabilized mixed finite element method (3.1)–(3.2), we rewrite it in a compact way: Find (𝝈h,𝒖h)𝚺k,h×𝑽k-1,h such that

(3.6)(𝝈h,𝒖h;𝝉h,𝒗h)=Ω𝒇𝒗hdxfor all (𝝉h,𝒗h)𝚺k,h×𝑽k-1,h,

where

(𝝈h,𝒖h;𝝉h,𝒗h):=a(𝝈h,𝝉h)+b(𝝉h,𝒖h)-b(𝝈h,𝒗h)+c(𝒖h,𝒗h).

Similarly, problem (1.1)–(1.2) can be rewritten as

(3.7)(𝝈,𝒖;𝝉,𝒗)=Ω𝒇𝒗dxfor all (𝝉,𝒗)𝚺×𝑽.

Obviously the bilinear form is continuous with respect to the norm 𝑯(div,𝒜)+0,c. Now we present the following inf-sup condition for (3.6).

Lemma 3.2

For any (𝛔~h,𝐮~h)Σk,h×𝐕k-1,h, it follows

(3.8)𝝈~h𝑯(div,𝒜)+𝒖~h0,csup(𝝉h,𝒗h)𝚺k,h×𝑽k-1,h(𝝈~h,𝒖~h;𝝉h,𝒗h)𝝉h𝑯(div,𝒜)+𝒗h0,c.

Proof.

It is sufficient to prove that for a given pair (𝝈~h,𝒖~h)𝚺k,h×𝑽k-1,h, there exists (𝝉h,𝒗h)𝚺k,h×𝑽k-1,h such that

(3.9)𝝈~h𝑯(div,𝒜)2+𝒖~h0,c2B(𝝈~h,𝒖~h;𝝉h,𝒗h),
(3.10)𝝉h𝑯(div,𝒜)+𝒗h0,c𝝈~h𝑯(div,𝒜)+𝒖~h0,c.

Let 𝒖~h𝑳2(Ω;n) such that 𝒖~h|K is the L2-projection of 𝒖~h|K onto 𝑹(K) for each K𝒯h. By (2.1), there exists 𝝉1𝑩k,h such that (cf. [41, Lemma 3.3] and [37, Lemma 3.1])

(3.11)div𝝉1=𝒖~h,𝝉1H(div,K)𝒖~h0,K.

By the definition of 𝝉1, it holds

(𝝈~h,𝒖~h;𝝉1,)=a(𝝈~h,𝝉1)+b(𝝉1,𝒖~h)=a(𝝈~h,𝝉1)+(𝒖~h,𝒖~h)=a(𝝈~h,𝝉1)+𝒖~h02.

Thus by (3.11), there exists a constant C1>0 such that

(𝝈~h,𝒖~h;𝝉1,0)-𝝈~ha𝝉1a+𝒖~h02-C1𝝈~ha𝒖~h0+𝒖~h02
(3.12)-C122𝝈~ha2+12𝒖~h02.

On the other hand, there exists 𝝉2𝑯01(Ω;𝕊) such that (cf. [10, 4])

(3.13)div𝝉2=𝒖~h-𝒖~hand𝝉21𝒖~h-𝒖~h0.

Thanks to (3.4), integration by parts leads to

b(𝑰h𝝉2,𝒖~h)=b(𝑰h𝝉2-𝝉2,𝒖~h)+b(𝝉2,𝒖~h)
=FhF(𝑰h𝝉2-𝝉2):𝒖~hds+Ω(𝒖~h-𝒖~h)𝒖~hdx
=FhF(𝑰h𝝉2-𝝉2):𝒖~hds+𝒖~h-𝒖~h02+Ω(𝒖~h-𝒖~h)𝒖~hdx.

Together with (3.5) and (3.13), there exists a constant C2>0 such that

(𝝈~h,𝒖~h;𝑰h𝝉2,0)=a(𝝈~h,𝑰h𝝉2)+b(𝑰h𝝉2,𝒖~h)
𝒖~h-𝒖~h02-C2𝒖~h-𝒖~h0(𝝈~ha+𝒖~hc+𝒖~h0)
(3.14)12𝒖~h-𝒖~h02-32C22(𝝈~ha2+𝒖~hc2+𝒖~h02).

Due to the inverse inequality, there exists a constant C3>0 such that

div𝝈~hcC3div𝝈~h0.

Then from the Cauchy–Schwarz inequality we get

(𝝈~h,𝒖~h;,-div𝝈~h)=div𝝈~h02-c(𝒖~h,div𝝈~h)div𝝈~h02-𝒖~hcdiv𝝈~hc
(3.15)div𝝈~h02-C3𝒖~hcdiv𝝈~h012div𝝈~h02-C322𝒖~hc2.

Now take 𝝉h=𝝈~h+γ1𝝉1+γ2𝑰h𝝉2 and 𝒗h=𝒖~h-γ3div𝝈~h where γ1, γ2 and γ3 are three to-be-determined positive constants. Then from (3.12), (3.14) and (3.15) we get

(𝝈~h,𝒖~h;𝝉h,𝒗h)=B(𝝈~h,𝒖~h;𝝈~h,𝒖~h)+γ1B(𝝈~h,𝒖~h;𝝉1,0)
+γ2B(𝝈~h,𝒖~h;𝑰h𝝉2,0)+γ3B(𝝈~h,𝒖~h;,-div𝝈~h)
=𝝈~ha2+𝒖~hc2+γ1B(𝝈~h,𝒖~h;𝝉1,0)
+γ2B(𝝈~h,𝒖~h;𝑰h𝝉2,0)+γ3B(𝝈~h,𝒖~h;,-div𝝈~h)
(1-γ1C122-γ23C222)𝝈~ha2+γ32div𝝈~h02+γ22𝒖~h-𝒖~h02
+(γ12-γ23C222)𝒖~h02+(1-γ23C222-γ3C322)𝒖~hc2.

Hence we acquire (3.9) by choosing

γ1=23C12,γ2=min{29C22,γ11+3C22},γ3=23C32.

Estimate (3.10) follows immediately from the definitions of 𝝉h and 𝒗h. ∎

The unique solvability of the stabilized mixed finite element method (3.1)–(3.2) is the immediate result of the inf-sup condition (3.8).

Next we show the a priori error analysis for the stabilized mixed finite element method (3.1)–(3.2). Subtracting (3.6) from (3.7), we have the following error equation from the definition of 𝑸h:

(3.16)(𝑰h𝝈-𝝈h,𝑸h𝒖-𝒖h;𝝉h,𝒗h)=a(𝑰h𝝈-𝝈,𝝉h)+b(𝝈-𝑰h𝝈,𝒗h)+c(𝑸h𝒖,𝒗h)

for any (𝝉h,𝒗h)𝚺k,h×𝑽k-1,h.

Theorem 3.3

Let (𝛔,𝐮) be the exact solution of problem (1.1)–(1.2) and (𝛔h,𝐮h) the discrete solution of the stabilized mixed finite element method (3.1)–(3.2) using Pkdiv-Pk-1-1 elements. Assume that 𝛔𝐇k+1(Ω;S) and 𝐮𝐇k(Ω;Rn), then

𝝈-𝝈h𝑯(div,𝒜)+𝒖-𝒖h0,chk(𝝈k+1+𝒖k).

Proof.

Set 𝝈~h=𝑰h𝝈-𝝈h and 𝒖~h=𝑸h𝒖-𝒖h in Lemma 3.2. From the error equation (3.16) we have

𝑰h𝝈-𝝈h𝑯(div,𝒜)+𝑸h𝒖-𝒖h0,csup(𝝉h,𝒗h)𝚺k,h×𝑽k-1,hB(𝑰h𝝈-𝝈h,𝑸h𝒖-𝒖h;𝝉h,𝒗h)𝝉h𝑯(div,𝒜)+𝒗h0,c
=sup(𝝉h,𝒗h)𝚺k,h×𝑽k-1,ha(𝑰h𝝈-𝝈,𝝉h)+b(𝝈-𝑰h𝝈,𝒗h)+c(𝑸h𝒖-𝒖,𝒗h)𝝉h𝑯(div,𝒜)+𝒗h0,c
𝝈-𝑰h𝝈𝑯(div,𝒜)+𝒖-𝑸h𝒖c.

Hence we can finish the proof by using the triangle inequality and the interpolation error estimates. ∎

4 Two Stabilized Mixed Finite Element Methods with Continuous Displacement

In this section, we will present another class of stabilized mixed finite element methods by a different stabilization mechanism suggested in [19]. To pursue a small number of global degrees of freedom, the displacement will be approximated by Lagrange elements. To be specific, we adopt the following finite element spaces for stress and displacement:

𝚺k,h:=𝚺~k,h+𝑩k+1,h,𝑾k,h:=𝑽k,h𝑯01(Ω;n).

Recurring to the stabilization technique in [19], we devise a stabilized mixed finite element method for linear elasticity as follows: Find (𝝈h,𝒖h)𝚺k,h×𝑾k,h such that

(4.1)a(𝝈h,𝝉h)+b(𝝉h,𝒖h)=-Ω𝒇div𝝉hdxfor all 𝝉h𝚺k,h,
(4.2)-b(𝝈h,𝒗h)=Ω𝒇𝒗hdxfor all 𝒗h𝑾k,h,

where

a(𝝈h,𝝉h):=a(𝝈h,𝝉h)+Ωdiv𝝈hdiv𝝉hdx.

The benefit of this stabilization technique is that the coercivity condition on 𝑯(div,Ω;𝕊) with norm 𝑯(div,𝒜) for the bilinear form a(,) holds automatically.

We are now in the position to prove the discrete inf-sup condition for the stabilized mixed finite element method (4.1)–(4.2). For this, define an interpolation operator 𝑰h:𝑯1(Ω;𝕊)𝚺k,h in the following way: for each 𝝉𝑯1(Ω;𝕊), let

𝑰h𝝉:=𝑰hSZ𝝉+𝑰k+1,hb(𝝉-𝑰hSZ𝝉).

We deduce from (2.2) that

(4.3)K(𝑰h𝝉-𝝉):𝝇dx=0for all 𝝇𝑷k-1(K;𝕊) and K𝒯h.

Similar to Lemma 3.1, we have the following interpolation error estimate.

Lemma 4.1

Given integers m,k1, we have, for any 𝛕𝐇m(Ω;S),

(4.4)K𝒯hhK-2𝝉-𝑰h𝝉0,K2+|𝝉-𝑰h𝝉|12h2min{k,m-1}𝝉m2.

Then using integration by parts and (4.3), we have

(4.5)b(𝑰h𝝉,𝒗h)=b(𝝉,𝒗h)for all 𝝉𝑯1(Ω;𝕊) and 𝒗h𝑾k,h.
Lemma 4.2

The following discrete inf-sup condition holds:

(4.6)𝒗h0sup𝝉h𝚺k,hb(𝝉h,𝒗h)𝝉h𝑯(div,𝒜)for all 𝒗h𝑾k,h.

Proof.

Let 𝒗h𝑾k,h, then there exists a 𝝉𝑯1(Ω;𝕊) such that (cf. [10, 4])

div𝝉=𝒗hand𝝉1𝒗h0.

It follows from (4.5) that

(4.7)b(𝑰h𝝉,𝒗h)=b(𝝉,𝒗h)=𝒗h02.

On the other hand, from (4.4) we get

(4.8)𝑰h𝝉𝑯(div,𝒜)𝝉1𝒗h0.

Hence (4.6) is the immediate result of (4.7) and (4.8). ∎

With the previous preparation, we show the a priori error estimate for the (Pk0+Bk+1div)-Pk0 elements.

Theorem 4.3

Let (𝛔,𝐮) be the exact solution of problem (1.1)–(1.2) and (𝛔h,𝐮h) the discrete solution of the stabilized mixed finite element method (4.1)–(4.2) using the (Pk0+Bk+1div)-Pk0 element. Assume that 𝛔𝐇k+1(Ω;S) and 𝐮𝐇k+1(Ω;Rn), then

𝝈-𝝈h𝑯(div,𝒜)+𝒖-𝒖h0hk(𝝈k+1+h𝒖k+1).

Proof.

The coercivity of the bilinear form a(,) with respect to the norm 𝑯(div,𝒜) is trivial. Together with the discrete inf-sup condition (4.6), we obtain the following error estimate by the standard theory of mixed finite element methods (cf. [18, 16]):

𝝈-𝝈h𝑯(div,𝒜)+𝒖-𝒖h0inf𝝉h𝚺k,h,𝒗h𝑾k,h(𝝈-𝝉h𝑯(div,𝒜)+𝒖-𝒗h0).

Choose 𝝉h=𝑰h𝝈 and 𝒗h=𝑰hSZ𝒖. Then we can finish the proof by combining the last inequality, (4.4) and (3.3). ∎

To achieve the optimal convergence rate of 𝒖-𝒖h0, we can further enrich the stress finite element space 𝚺k,h to 𝚺k+1,h. The resulting mixed finite element method is: Find (𝝈h,𝒖h)𝚺k+1,h×𝑾k,h such that

(4.9)a(𝝈h,𝝉h)+b(𝝉h,𝒖h)=-Ω𝒇div𝝉hdxfor all 𝝉h𝚺k+1,h,
(4.10)-b(𝝈h,𝒗h)=Ω𝒇𝒗hdxfor all 𝒗h𝑾k,h.

Corollary 4.4

Let (𝛔,𝐮) be the exact solution of problem (1.1)–(1.2) and (𝛔h,𝐮h) the discrete solution of the stabilized mixed finite element method (4.9)–(4.10) using the Pk+1div-Pk0 element. Then under the assumption of 𝛔𝐇k+2(Ω;S) and 𝐮𝐇k+1(Ω;Rn), it follows

(4.11)𝝈-𝝈h𝑯(div,𝒜)+𝒖-𝒖h0hk+1(𝝈k+2+𝒖k+1).
Remark 4.5

The finite element pair 𝚺k+1,h×𝑾k,h is just the Hood–Taylor element in [54, 13, 14] augmented by the elementwise 𝑯(div) bubble function space 𝑩k+1,h. Hence we give a positive answer to the question in [19, Example 3.3] whether the Hood–Taylor element is stable for the linear elasticity.

Remark 4.6

In order to remain the zero right-hand side as in (1.1) and (3.1), we can use the following stabilized mixed finite element method: Find (𝝈h,𝒖h)𝚺k+1,h×𝑾k,h such that

a(𝝈h,𝝉h)+b(𝝉h,𝒖h)=0for all 𝝉h𝚺k+1,h,
-b(𝝈h,𝒗h)=Ω𝒇𝒗hdxfor all 𝒗h𝑾k,h,

where

a(𝝈,𝝉)=Ω𝒜𝝈:𝝉dx+FhhFF[div𝝈][div𝝉]ds.

For any 𝝉h𝚺k+1,h, define the norm

𝝉h2:=𝝉h𝑯(div,𝒜)2+FhhF[div𝝉h]0,F2.

It can be shown that a(,) is coercive on the kernel space

𝑲h:={𝝉h𝚺k+1,h:b(𝝉h,𝒗h)=0 for all 𝒗h𝑾k,h},

i.e.

𝝉h2a(𝝉h,𝝉h)for all 𝝉h𝑲h.

The discrete inf-sup condition can be derived from (4.6) and the inverse inequality.

5 Numerical Results

In this section, we will report some numerical results to assess the accuracy and behavior of the stabilized mixed finite element methods developed in Sections 3 and 4. Let λ=0.3 and μ=0.35. We use the uniform triangulation 𝒯h of Ω.

First we test our stabilized mixed finite element methods for the pure displacement problem on the square Ω=(-1,1)2 in 2D. Take

𝒇(x1,x2)=(-8(x1+x2)((3x1x2-2)(x12+x22)+5(x1x2-1)2-2x12x22)-8(x1-x2)((3x1x2+2)(x12+x22)-5(x1x2+1)2+2x12x22)).

It can be verified that the exact displacement of problem (1.1)–(1.2) is

𝒖(x1,x2)=807(-x2(1-x22)(1-x12)2x1(1-x12)(1-x22)2)-4(x1(1-x12)(1-x22)2x2(1-x22)(1-x12)2).

The exact stress can be computed by 𝝈=2μ𝜺(𝒖)+λ(tr𝜺(𝒖))𝜹.

The element diagram in Figure 1 is mnemonic of the local degrees of freedom of 𝚺2,h in 2D. For the stabilized Pkdiv-Pk-1-1 element, numerical errors 𝝈-𝝈h𝑯(div,𝒜), uhc and 𝒖-𝒖h0 with respect to h for k=1,2 are shown in Tables 1 and 2, from which we can see that all the three errors achieve optimal convergence rates O(hk) numerically. These results agree with the theoretical result in Theorem 3.3. Numerical results for the stabilized mixed finite element method (4.1)–(4.2) with k=1 are listed in Table 3. We find that the convergence rate of 𝝈-𝝈h𝑯(div,𝒜) is O(h), which coincides with Theorem 4.3. It deserves to be mentioned that the convergence rate of 𝒖-𝒖h0 in Table 3 is higher than the theoretical result in Theorem 4.3, but still suboptimal. Numerical results for the stabilized mixed finite element method (4.9)–(4.10) with k=1 are given in Table 4. It can be observed that both convergence rates of 𝝈-𝝈h𝑯(div,𝒜) and 𝒖-𝒖h0 are O(h2), as indicated by (4.11).

Figure 1 Element diagram for 𝚺2,h${\boldsymbol{\Sigma}_{2,h}}$ in 2D.
Figure 1

Element diagram for 𝚺2,h in 2D.

Table 1

Numerical errors for the stabilized P10-P0-1 element in 2D.

h𝝈-𝝈h𝑯(div,𝒜)order𝒖hcorder𝒖-𝒖h0order
2-11.9436E+01-5.7136E+00-2.8981E+00-
2-21.0703E+010.863.7894E+000.591.6073E+000.85
2-35.7982E+000.882.1600E+000.818.3356E-010.95
2-43.0580E+000.921.1484E+000.914.2521E-010.97
2-51.5780E+000.955.9220E-010.962.1527E-010.98
2-68.0346E-010.973.0101E-010.981.0848E-010.99
2-74.0590E-010.991.5187E-010.995.4494E-020.99
Table 2

Numerical errors for the stabilized P2div-P1-1 element in 2D.

h𝝈-𝝈h𝑯(div,𝒜)order𝒖hcorder𝒖-𝒖h0order
11.1868E+01-5.0478E+00-2.4374E+00-
2-14.6400E+001.351.7436E+001.537.1254E-011.77
2-21.4841E+001.644.6132E-011.921.8285E-011.96
2-34.2227E-011.811.1783E-011.974.6102E-021.99
2-41.1120E-011.922.9546E-022.001.1556E-022.00
2-52.8378E-021.977.3651E-032.002.8912E-032.00
2-67.1562E-031.991.8358E-032.007.2294E-042.00
Table 3

Numerical errors for the stabilized (P10+B2div)-P10 element in 2D.

h𝝈-𝝈h𝑯(div,𝒜)order𝒖-𝒖h0order
2-11.3570E+01-5.9057E+00-
2-27.5576E+000.842.1407E+001.46
2-34.1592E+000.866.2487E-011.78
2-42.2977E+000.861.9626E-011.67
2-51.2391E+000.896.2250E-021.66
2-66.4969E-010.931.9087E-021.71
2-73.3399E-010.965.7719E-031.73
Table 4

Numerical errors for the stabilized P2div-P10 element in 2D.

h𝝈-𝝈h𝑯(div,𝒜)order𝒖-𝒖h0order
11.0966E+01-6.0260E+00-
2-13.5092E+001.641.5579E+001.95
2-29.0380E-011.963.3148E-012.23
2-32.2504E-012.017.2219E-022.20
2-45.5922E-022.011.6506E-022.13
2-51.3981E-022.004.1182E-032.00
2-63.4746E-032.019.5159E-042.11
Table 5

Numerical errors for the stabilized P10-P0-1 element in 3D.

h𝝈-𝝈h𝑯(div,𝒜)order𝒖hcorder𝒖-𝒖h0order
2-14.1723E+00-4.0747E-01-2.4720E-01-
2-22.3595E+000.823.5554E-010.201.7403E-010.51
2-31.2849E+000.882.5527E-010.481.1168E-010.64
2-46.8023E-010.921.5243E-010.746.3889E-020.81
2-53.5167E-010.958.3310E-020.873.4309E-020.90
Table 6

Numerical errors for the stabilized P2div-P1-1 element in 3D.

h𝝈-𝝈h𝑯(div,𝒜)order𝒖hcorder𝒖-𝒖h0order
2-11.4440E+00-1.7738E-01-8.3035E-02-
2-23.8864E-011.895.2337E-021.762.2979E-021.85
2-39.9734E-021.961.3657E-021.945.9084E-031.96
2-42.5160E-021.993.4507E-031.981.4873E-031.99
Table 7

Numerical errors for the stabilized P2div-P10 element in 3D.

h𝝈-𝝈h𝑯(div,𝒜)order𝒖-𝒖h0order
2-11.4391E+00-2.3509E-01-
2-23.8148E-011.925.4959E-022.10
2-39.6524E-021.981.1730E-022.23
2-42.4182E-022.002.6368E-032.15
Table 8

Numerical errors for the stabilized P3div-P20 element in 3D.

h𝝈-𝝈h𝑯(div,𝒜)order𝒖-𝒖h0order
2-12.7531E-01-3.9149E-02-
2-23.7035E-022.895.7416E-032.77
2-34.7120E-032.977.8312E-042.87

Next we take into account the pure displacement problem on the unit cube Ω=(0,1)3 in 3D. The exact solution is given by

𝒖(x1,x2,x3)=(242526)x1(1-x1)x2(1-x2)x3(1-x3).

Then the exact stress 𝝈 and the load function 𝒇 are derived from (1.1)–(1.2). From Tables 5 and 6, it is easy to see that all the convergence rates of the errors 𝝈-𝝈h𝑯(div,𝒜), 𝒖hc and 𝒖-𝒖h0 for the stabilized Pkdiv-Pk-1-1 with k=1,2 are optimal, i.e. O(hk) assured by Theorem 3.3. The numerical convergence rates of the errors 𝝈-𝝈h𝑯(div,𝒜) and 𝒖-𝒖h0 for the stabilized Pk+1div-Pk0 element with k=1,2 are presented in Tables 7 and 8. The numerical results in these two tables confirm the optimal rate of convergence result (4.11).

Award Identifier / Grant number: DMS-1418934

Award Identifier / Grant number: 11625101

Award Identifier / Grant number: 11271035

Award Identifier / Grant number: 91430213

Award Identifier / Grant number: 11421101

Award Identifier / Grant number: 11301396

Award Identifier / Grant number: 11671304

Award Identifier / Grant number: LY17A010010

Award Identifier / Grant number: LY15A010015

Award Identifier / Grant number: LY15A010016

Award Identifier / Grant number: LY14A010020

Funding statement: The first author was supported by NSF (grant DMS-1418934). The work of the second author was supported by the NSFC (projects 11625101, 11271035, 91430213, 11421101). The work of the third author was supported by the NSFC (projects 11301396, 11671304) and the Natural Science Foundation of Zhejiang Province (projects LY17A010010, LY15A010015, LY15A010016, LY14A010020).

Acknowledgements

This work was finished when L. Chen visited Peking University in the fall of 2015. He would like to thank Peking University for the support and hospitality, as well as for their exciting research atmosphere.

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Received: 2016-10-14
Revised: 2016-10-19
Accepted: 2016-10-20
Published Online: 2016-11-10
Published in Print: 2017-1-1

© 2017 by De Gruyter

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