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A Mixed Finite Element Method for Coupled Plates

  • Jun Hu , Zhen Liu , Rui Ma EMAIL logo and Ruishu Wang
Published/Copyright: April 30, 2025

Abstract

This paper introduces a mixed finite element method for the problem of two coupled plates with mixed boundary conditions and rigid junction conditions. By introducing the union of stresses and moments as an independent variable, which is of significant interest in practical applications, a mixed formulation is developed and its well-posedness is established. To avoid complications with the direct use of trace operators, the theory of densely defined operators in Hilbert spaces is employed to determine a suitable space that incorporates boundary and junction conditions for this variable. Based on the mixed formulation, a mixed finite element method is presented along with an illustrative example. The discrete stability and the a priori analysis for the mixed finite element method are proved under some assumptions. Numerical tests demonstrate the theoretical results.

MSC 2020: 65N30

1 Introduction

Elastic structures consisting of coupled plates are extensively utilized in automotive and aerospace engineering applications, see, e.g., [41, 7]. This paper focuses on the problem of two coupled plates. The mathematical model for two coupled plates can be formulated by combining two individual plate models, coupled through junction conditions. Specifically, the model for a single plate consists of a plane elasticity model along the longitudinal direction and a Kirchhoff plate model along the transverse direction, with rigid junction conditions considered in this paper. For more descriptions of the mathematical model, readers can refer to [8, 15, 16].

Finite element methods for two coupled plates based on the displacement formulation are well studied, see, e.g., [19, 28, 30, 8, 42, 43, 32, 33, 29]. Nevertheless, there are several motivations for exploring mixed formulations. First, conforming finite element methods for discretizing the deflection require C 1 -continuous elements, which are difficult to construct. Second, stresses and moments are often of greater interest in practical applications, but these quantities cannot be directly obtained from the displacement formulation. Third, junction conditions involve continuity of stresses and moments, see [8, 42, 43]. The displacement formulation treats these continuity conditions as natural junction conditions, which may lead to inaccuracy.

To address these issues, this paper introduces a mixed variational formulation for two coupled plates by introducing the union of stresses and moments as an independent variable. The mixed formulation for two coupled plates can be regarded as an extension of mixed formulations for a single plate. For the plane elasticity model, the Hellinger–Reissner variational principle [5] is employed, which seeks displacements in L 2 ( 2 ) and stresses in H ( div , 𝕊 ) consisting of symmetric tensors with L 2 -components whose divergence is in L 2 ( 2 ) . For the Kirchhoff plate model, a mixed formulation in [36, 4] is utilized, which seeks the transverse displacement in L 2 and moments in H ( divDiv , 𝕊 ) consisting of symmetric tensors with L 2 -components whose divDiv is in L 2 . These two mixed formulations are plausible for preserving the junction conditions of stresses and moments.

However, the generalization of mixed formulations for a single plate to two coupled plates is not straightforward. The main challenge lies in providing an appropriate Sobolev space that incorporates both boundary conditions and junction conditions, which are defined on parts of the boundary for stresses and moments. Since traces of functions in H ( div , 𝕊 ) and H ( divDiv , 𝕊 ) are defined in negative spaces on the boundary, they cannot be simply restricted to parts of the boundary [9, 18]. Furthermore, continuity conditions on the junction involve the coupling of stresses and moments, which need to deal with the coupling of traces of different spaces. In [31, 39], the authors reconsidered the mixed Hellan–Herrmann–Johnson (HHJ) method for the Kirchhoff plate, which seeks moments in H - 1 ( divDiv , 𝕊 ) consisting of symmetric tensors with L 2 -components whose divDiv is in H - 1 , under mixed boundary conditions by duality arguments. This approach avoids the technical complexities associated with directly using trace operators in nonstandard Sobolev spaces. Similar results can be found in tangential-displacement normal-normal stress (TDNNS) method [38, 37] for the plane elasticity model.

This paper employs duality arguments to establish the proper space for the union of stresses and moments of two coupled plates with mixed boundary and rigid junction conditions. Specifically, this paper defines the differential operator B which acts on the space with respect to displacements in the displacement formulation and maps to the space with respect to stresses and moments in L 2 ( 𝕊 ) × L 2 ( 𝕊 ) . The definition of domain of B belongs to H 1 ( 2 ) × H 2 but associated with L 2 ( 2 ) × L 2 norm within it. Then the adjoint operator B * and its definition of domain Σ are derived from the theory of densely defined operators in Hilbert spaces. It is shown that Σ is a subspace of H ( div , 𝕊 ) × H ( divDiv , 𝕊 ) , incorporating the continuity conditions for stresses and moments across the junction. Based on the operator B * and the space Σ, a mixed variational formulation is established. The well-posedness of the mixed variational formulation is proven by utilizing the equivalence to the displacement formulation [8, 42]. Additionally, sufficient and necessary continuity conditions for sufficiently smooth functions in Σ are provided, aligning with continuity conditions of smooth stresses and moments across the junction in [8, 29]. There are some mixed formulations that partially maintain continuity conditions for shell problems, such as the normal-normal components of moments in TDNNS [35, 34] and in HHJ [40].

A conforming mixed finite element method based on the mixed formulation is provided in this paper. The discrete stability and the a priori analysis are shown for this mixed finite element method under some reasonable assumptions regarding the choice of the discrete spaces. Various conforming mixed finite elements satisfying these assumptions can be employed. For finite elements of H ( div , 𝕊 ) , see [25, 5] on triangular meshes and [2, 20, 14] on rectangular meshes. For finite elements of H ( divDiv , 𝕊 ) , see [23, 44, 11] on triangular meshes and [17] on rectangular meshes. Mixed finite elements in higher dimensions can be found in [21, 26, 27, 24, 20, 1, 3, 6] of H ( div , 𝕊 ) and in [23, 12, 22, 13] of H ( divDiv , 𝕊 ) . To demonstrate the mixed finite element method and facilitate the implementation of the continuity conditions, this paper employs the H ( div , 𝕊 ) conforming elements [25] and the H ( divDiv , 𝕊 ) conforming elements [11] to approximate stresses and moments, respectively. Numerical experiments are conducted to validate the theoretical results.

Organization of the Paper.

Section 2 revisits the plane elasticity model and the Kirchhoff plate model, presenting the variational formulation for two coupled plates based on displacements and providing its well-posedness. Section 3 introduces the mixed variational formulation and constructs the nonstandard Sobolev space Σ for two coupled plates. The well-posedness of the mixed formulation is proven. Section 4 presents the conforming mixed finite element method and an illustrative example. Numerical experiments are performed to validate the theory.

2 Preliminaries

This section presents the model assumptions and notation conventions in this paper. A single plate model is shown to define some notations. Then the model of two coupled plates with a rigid junction is provided.

2.1 Hypotheses and Notations

Let H m ( D ; X ) denote the Sobolev space of functions of L 2 ( D ; X ) within domain D, taking values in space X, whose distributional derivatives up to the order m also belong to L 2 ( D ; X ) . Let C m ( D ; X ) denote the space of m-times continuously differentiable functions and P l ( D ; X ) denote the set of all the polynomials with the total degree no greater than l. In this paper, X could be , 2 or 𝕊 , where 𝕊 denotes the set of all symmetric 2 × 2 matrices. If X = , then H m ( D ) abbreviates H m ( D ; X ) , similarly for C m ( D ) and P l ( D ) . The standard Sobolev norm m , D will be taken. When m = 0 , H 0 ( D ; X ) is exactly L 2 ( D ; X ) . The L 2 inner product is denoted by ( , ) D for the scalar, vector-valued, and tensor-valued L 2 spaces over D. In particular, for the tensor-valued L 2 space,

( 𝝈 , 𝝉 ) D D 𝝈 : 𝝉 d x = D i , j = 1 2 σ i j τ i j d x for all  𝝈 , 𝝉 L 2 ( D ; 𝕊 ) .

For scalar functions v, vector-valued functions 𝝍 , and matrix-valued functions 𝝉 , the first-order differential operators v , 𝝍 , s 𝝍 , div 𝝍 and Div 𝝉 are defined by

v ( 1 v 2 v ) , 𝝍 ( 1 ψ 1 2 ψ 1 1 ψ 2 2 ψ 2 ) , s 𝝍 1 2 ( 𝝍 + 𝝍 T ) ,
div 𝝍 1 ψ 1 + 2 ψ 2 , Div 𝝉 ( 1 τ 11 + 2 τ 12 1 τ 21 + 2 τ 22 ) .

Define the following spaces:

H ( div , D ; 2 ) { 𝝍 L 2 ( D ; 2 ) : div 𝝍 L 2 ( D ) } ,
H ( Div , D ; 𝕊 ) { 𝝉 L 2 ( D ; 𝕊 ) : Div 𝝉 L 2 ( D ; 2 ) } ,
H ( divDiv , D ; 𝕊 ) { 𝝉 L 2 ( D ; 𝕊 ) : divDiv 𝝉 L 2 ( D ) } .

Let S be the midsurface of a thin plate which lies in the x-y plane. For simplicity, assume that S is clamped on S 0 S , with nonzero measure, and is free on the complementary part which is denoted as S 1 , i.e., S = S 0 S 1 , S 0 S 1 = . Other boundary conditions can be treated similarly. In this paper, the deformations are assumed to be small and governed by the equations of plane elasticity, and the material is supposed to be homogeneous and isotropic. The load in S is assumed to be a distributed load ( 𝒇 , f 3 ) ( f 1 , f 2 , f 3 ) , which can be decomposed into in-plane and out-of-plane components. Let 𝒏 and 𝒕 denote the unit outer normal vector and the unit counterclockwise tangential vector of S , respectively, and let n ( ) ( ) 𝒏 and t ( ) ( ) 𝒕 .

For the in-plane part, the plane elasticity model is

{ - Div 𝝈 = 𝒇 in  S , 𝒖 = 0 on  S 0 , 𝝈 𝒏 = 0 on  S 1 ,

where 𝒖 = ( u 1 , u 2 ) T is the displacement vector in plane, and 𝝈 is the stress tensor. The constitutive relation reads

(2.1) 𝝈 = 𝝈 ( 𝒖 ) = 𝒞 1 s 𝒖 E t 1 - ν 2 ( ( 1 - ν ) s 𝒖 + ν tr ( s 𝒖 ) 𝐈 ) ,

where 𝐈 is the identity tensor and tr ( ) is the trace operator. Here t , E , and ν denote the thickness of the plate, Young’s modulus, and the Poisson ratio of the material, respectively.

For the out-of-plane part, the Kirchhoff plate model is

{ - divDiv 𝑴 = f 3 in  S , u 3 = 0 , n u 3 = 0 on  S 0 , T = 0 , M n n = 0 on  S 1 , [ [ M n t ] ] x = 0 at  x 𝒱 S 1 ,

where u 3 is the deflection and 𝑴 is the moment tensor. The constitutive relation reads

(2.2) 𝑴 = 𝑴 ( u 3 ) = 𝒞 2 ( - 2 u 3 ) E t 3 12 ( 1 - ν 2 ) ( ( 1 - ν ) ( - 2 u 3 ) + ν tr ( - 2 u 3 ) 𝐈 ) .

The components of 𝑴 and the shear force T on S are denoted by

M n n ( 𝑴 𝒏 ) 𝒏 , M n t ( 𝑴 𝒏 ) 𝒕 , T ( Div 𝑴 ) 𝒏 + t ( M n t ) .

The set 𝒱 S 1 contains all corner points x where exist two adjacent edges e 1 , e 2 S 1 satisfying e 1 e 2 = x . These edges do not meet an angle of π and possess different normal and tangential vectors 𝒏 1 , 𝒕 1 and 𝒏 2 , 𝒕 2 , respectively. For x 𝒱 S 1 with x being the end point of e 1 and the starting point of e 2 , define

(2.3) [ [ M n t ] ] x M n 1 t 1 ( x ) - M n 2 t 2 ( x ) for  x 𝒱 S 1 .

2.2 Two Coupled Plates Model

This subsection presents the model of two coupled plates with midsurfaces denoted by S and ~ S . Throughout this paper, let ( ~ ) denote the quantities related to ~ S with the same physical meaning as those in S without exception. For simplicity, assume that the material parameters t , E , ν and ~ t , ~ E , ~ ν take the same value, respectively.

Suppose that S and ~ S are coupled along a common rectilinear junction Γ S ~ S , see Figure 1. Assume that S is clamped on S 0 S with nonzero measure. Let S 1 and ~ S 1 be the free boundary of S and ~ S , respectively. Then it holds that

S = S 0 S 1 Γ , ~ S = ~ S 1 Γ .

Let 𝒍 = 𝒏 × 𝒕 . It follows that ( 𝒏 , 𝒕 , 𝒍 ) defined on Γ S constitutes a local orthogonal reference system of S. By taking the opposite direction 𝒕 = - 𝒕 on Γ, the local orthogonal reference system of ~ S can be defined by ( ~ 𝒏 , 𝒕 , ~ 𝒍 ) on Γ ~ S . Define the angle θ between two plates by cos θ = 𝒏 ~ 𝒏 . Then

~ 𝒏 = 𝒏 cos θ - 𝒍 sin θ , 𝒕 = - 𝒕 , ~ 𝒍 = - 𝒏 sin θ - 𝒍 cos θ .

When the plates are coplanar, the angle is equal to π, and when the plates coincide, the angle is equal to 0. This paper deals with the case 0 < θ < π .

Assume that two plates are coupled with a rigid junction. Then the equilibrium equations of two coupled plates, see [8, 42] for instance, are

(2.4)

Div 𝝈 + 𝒇 = 0 , divDiv 𝑴 + f 3 = 0  in  S ,
~ Div ~ 𝝈 + ~ 𝒇 = 0 , ~ divDiv ~ 𝑴 + ~ f 3 = 0  in  ~ S ,

with the boundary conditions

(2.5)

(2.5a) 𝒖 = 𝟎 , u 3 = 0 , n u 3 = 0 on  S 0 ,
(2.5b) 𝝈 𝒏 = 𝟎 , T = 0 , M n n = 0 on  S 1 , [ [ M n t ] ] x = 0 for all  x 𝒱 S 1 ,
(2.5c) ~ 𝝈 ~ 𝒏 = 𝟎 , ~ T = 0 , ~ M ~ n ~ n = 0 on  ~ S 1 , [ [ ~ M ~ n ~ t ] ] x = 0 for all  x 𝒱 ~ S 1 ,

and the junction conditions

(2.6)

(2.6a) n u 3 = - ~ n ~ u 3 on  Γ ,
(2.6b) u 1 = ~ u 1 cos θ - ~ u 3 sin θ , u 2 = - ~ u 2 , u 3 = - ~ u 1 sin θ - ~ u 3 cos θ on  Γ ,
(2.6c) ~ M ~ n ~ n = M n n on  Γ ,
(2.6d) ~ σ ~ n ~ n = - σ n n cos θ + T sin θ , ~ σ ~ n ~ t = σ n t , ~ T = σ n n sin θ + T cos θ on  Γ ,
(2.6e) [ [ M n t ] ] x sin θ = 0 , [ [ ~ M ~ n ~ t ] ] x - [ [ M n t ] ] x cos θ = 0 for all  x Γ .

Here Γ denotes the collection of two end points of Γ.

Figure 1

Local orthogonal reference systems of two coupled plates.

2.3 Variational Formulation Based on Displacements

This subsection recalls the variational formulation based on displacements from [8, 42]. Let ϕ ( 𝒖 , u 3 ; ~ 𝒖 , ~ u 3 ) and F ( 𝒇 , f 3 ; ~ 𝒇 , ~ f 3 ) denote the displacement and external distribute force of S ~ S , respectively. Define

(2.7)

W { ψ = ( 𝒗 , v 3 ; ~ 𝒗 , ~ v 3 ) : ( 𝒗 , v 3 ) H 1 ( S ; 2 ) × H 2 ( S ) , ( ~ 𝒗 , ~ v 3 ) H 1 ( ~ S ; 2 ) × H 2 ( ~ S ) ,
ψ  satisfies (2.5a), (2.6a) and (2.6b) }

equipped with the norm

ψ W ( 𝒗 1 , S 2 + v 3 2 , S 2 + ~ 𝒗 1 , ~ S 2 + ~ v 3 2 , ~ S 2 ) 1 2 .

Given ϕ , ψ W , define

(2.8) D ( ϕ , ψ ) S 𝝈 ( 𝒖 ) : s 𝒗 d S + S 𝑴 ( u 3 ) : ( - 2 v 3 ) d S + ~ S ~ 𝝈 ( ~ 𝒖 ) : ~ s ~ 𝒗 d ~ S + ~ S ~ 𝑴 ( ~ u 3 ) : ( - ~ 2 ~ v 3 ) d ~ S .

Introduce the L 2 space

(2.9) V { ψ = ( 𝒗 , v 3 ; ~ 𝒗 , ~ v 3 ) : ( 𝒗 , v 3 ) L 2 ( S ; 2 ) × L 2 ( S ) , ( ~ 𝒗 , ~ v 3 ) L 2 ( ~ S ; 2 ) × L 2 ( ~ S ) } ,

equipped with the norm

(2.10) ψ V ( 𝒗 0 , S 2 + v 3 0 , S 2 + ~ 𝒗 0 , ~ S 2 + ~ v 3 0 , ~ S 2 ) 1 2

and the corresponding L 2 inner product ( , ) V . Then the variational formulation for two coupled plates (2.4)–(2.6e) with an angle θ reads as follows.

Problem 1.

Given F V , find ϕ W such that

D ( ϕ , ψ ) = ( F , ψ ) V for all  ψ W .

Lemma 2.1 (Well-Posedness [42, Lemma 2.2]).

The bilinear form D ( , ) defined in (2.8) is continuous and coercive on W × W . Moreover, the solution ϕ depends continuously on F with a constant C, namely, ϕ W C F V .

3 Mixed Variational Formulation

This section introduces a mixed formulation for two coupled plates. The unisolvence of the mixed variational formulation is established, by showing the equivalence to the displacement variational formulation.

3.1 Spaces and Operators

By introducing the union of the stresses and moments

Φ ( 𝝈 , 𝑴 ; ~ 𝝈 , ~ 𝑴 )

in (2.4) as an independent variable, this section provides a mixed formulation for two coupled plates. Note that, for a single plate S, the mixed formulation based on H ( div , 𝕊 ) × L 2 ( 2 ) is considered for plane elasticity and the mixed formulation based on H ( divDiv , 𝕊 ) × L 2 is considered for the Kirchhoff plate. Readers can refer to [25, 5, 2, 14, 21, 26, 27, 24, 20, 1, 3, 6] and [23, 44, 11, 13, 17, 12, 22] for these two formulations with corresponding mixed finite element methods, respectively. The mixed formulation for two coupled plates can be regarded as an extension of mixed formulations for a single plate.

The generalization of mixed formulations for a single plate to two coupled plates is not straightforward. The main challenge lies in providing an appropriate Sobolev space that incorporates both free boundary conditions (2.5b)–(2.5c) and junction conditions (2.6c)–(2.6e), which are defined on parts of the boundary for stresses and moments. For example, given a stress tensor 𝝈 H ( div , S ; 𝕊 ) , the restriction of 𝝈 𝒏 on S belongs to H - 1 / 2 ( S ) . Since H - 1 / 2 ( S ) is defined as a dual space, 𝝈 𝒏 cannot be simply restricted on S 1 [10, Section 2.5]. Similar considerations apply to functions in H ( divDiv , 𝕊 ) [18]. Furthermore, recall the continuity conditions (2.6d) on the junction as

~ σ ~ n ~ n = - σ n n cos θ + T sin θ , ~ σ ~ n ~ t = σ n t , ~ T = σ n n sin θ + T cos θ on  Γ .

These conditions involve the coupling of stresses and moments, which need to deal with the coupling of traces of H ( div , 𝕊 ) and H ( divDiv , 𝕊 ) .

In this paper, instead of directly tackling the free boundary and rigid junction conditions, a nonstandard Sobolev space is proposed through the application of duality arguments. This approach avoids the direct use of trace operators in nonstandard Sobolev spaces, which would be technically rather involved. Similar results can be found in [39, 38, 37] to deal with H - 1 ( divDiv , 𝕊 ) . Introduce the L 2 space

(3.1) V s { Ψ = ( 𝝉 , 𝜿 ; ~ 𝝉 , ~ 𝜿 ) : ( 𝝉 , 𝜿 ) L 2 ( S ; 𝕊 ) × L 2 ( S ; 𝕊 ) , ( ~ 𝝉 , ~ 𝜿 ) L 2 ( ~ S ; 𝕊 ) × L 2 ( ~ S ; 𝕊 ) }

equipped with the norm

Ψ V s ( 𝝉 0 , S 2 + 𝜿 0 , S 2 + ~ 𝝉 0 , ~ S 2 + ~ 𝜿 0 , ~ S 2 ) 1 2

and the corresponding L 2 inner product ( , ) V s . Define the operator

(3.2) B ( - s , 2 ; - ~ s , ~ 2 )

on W in (2.7). Note that the first and the second differential operators are defined in the context of classical weak derivatives. It can be observed that B W V s .

Let X be a Hilbert space such that W is dense in X, which will be specified later. Introduce the operator B * : D ( B * ) V s X * , where D ( B * ) is the domain of definition of B * , as follows: y D ( B * ) if and only if y V s and there exists a linear functional G X * such that

( B x , y ) V s = G , x X * × X for all  x W .

Define B * y = G . Note that B * y , x is well-defined for x X and y D ( B * ) , and

B * y , x X * × X = ( B x , y ) V s for all  x W , y D ( B * ) .

The domain D ( B * ) is a Hilbert space with the graph norm

y D ( B * ) ( y V s 2 + B * y X * 2 ) 1 2 .

Note that the displacement formulation in Problem 1 can be viewed as the case X = W . This paper considers the case X = V with V from (2.9). Obviously, W V and W is dense in V. The operator B is then a densely defined linear operator. It follows from (2.10) that V * = V and , V * × V = ( , ) V . Define a subspace of V s as follows:

(3.3) H s { Ψ = ( 𝝉 , 𝜿 ; ~ 𝝉 , ~ 𝜿 ) : ( 𝝉 , 𝜿 ) H ( Div , S ; 𝕊 ) × H ( divDiv , S ; 𝕊 ) , ( ~ 𝝉 , ~ 𝜿 ) H ( ~ Div , ~ S ; 𝕊 ) × H ( ~ divDiv , ~ S ; 𝕊 ) } .

According to the definition of B * , Φ D ( B * ) if and only if Φ V s and there exists a linear functional G V such that

(3.4) ( B ψ , Φ ) V s = ( G , ψ ) V for all  ψ W .

Note that C 0 ( S ; 2 ) × C 0 ( S ) × C 0 ( ~ S ; 2 ) × C 0 ( ~ S ) is contained in W and is dense in V. This, (3.3) and (3.4) show that Φ H s for any Φ D ( B * ) and

(3.5) B * = ( Div , divDiv ; ~ Div , ~ divDiv ) .

Let Σ D ( B * ) be the space for the introduced independent variable. Then the following equality holds:

(3.6) ( B * Φ , ψ ) V = ( B ψ , Φ ) V s for all  ψ W , Φ Σ .

The nonstandard Sobolev space Σ can be explicitly given by

(3.7) Σ = { Φ H s : there exists  C > 0  such that  | ( B ψ , Φ ) V s | C ψ V  for all  ψ W }

equipped with the norm Φ Σ ( Φ V s 2 + B * Φ V 2 ) 1 / 2 , i.e.,

Φ Σ = ( Φ V s 2 + Div 𝝈 0 2 + divDiv 𝑴 0 2 + ~ Div ~ 𝝈 0 2 + ~ divDiv ~ 𝑴 0 2 ) 1 / 2 .

3.2 Mixed Formulation and Its Well-Posedness

The results in the previous subsection of densely defined operator B and its adjoint B * together with their definition of domain motivate the mixed formulation as follows. Recall the definition of 𝒞 1 in (2.1) and 𝒞 2 in (2.2). Define 𝒞 ( 𝒞 1 , 𝒞 2 ; 𝒞 1 , 𝒞 2 ) by

𝒞 Ψ ( 𝒞 1 𝝉 , 𝒞 2 𝜿 ; 𝒞 1 ~ 𝝉 , 𝒞 2 ~ 𝜿 ) for all  Ψ = ( 𝝉 , 𝜿 ; ~ 𝝉 , ~ 𝜿 ) .

Problem 2.

Given F V , find ( Φ , ϕ ) Σ × V such that

( Φ , Ψ ) 𝒞 - 1 + ( B * Ψ , ϕ ) V = 0 for all  Ψ Σ ,
( B * Φ , ψ ) V = - ( F , ψ ) V for all  ψ V

with

( Φ , Ψ ) 𝒞 - 1 ( 𝒞 1 - 1 𝝈 , 𝝉 ) S + ( 𝒞 2 - 1 𝑴 , 𝜿 ) S + ( 𝒞 1 - 1 ~ 𝝈 , ~ 𝝉 ) ~ S + ( 𝒞 2 - 1 ~ 𝑴 , ~ 𝜿 ) ~ S .

It is easy to verify that ( Φ , Ψ ) 𝒞 - 1 is a symmetric, nonnegative bilinear form. Brezzi’s theory (see, e.g., [10]) shows that the well-posedness of Problem 2 holds if the following conditions are satisfied:

  1. ( Φ , Ψ ) 𝒞 - 1 is bounded: There exists a constant a > 0 such that

    | ( Φ , Ψ ) 𝒞 - 1 | a Φ Σ Ψ Σ for all  Φ , Ψ Σ .

  2. ( B * Ψ , ψ ) V is bounded: There exists a constant b > 0 such that

    | ( B * Ψ , ψ ) V | b Ψ Σ ψ V for all  Ψ Σ , ψ V .

  3. ( Ψ , Ψ ) 𝒞 - 1 is coercive on the kernel of B: There exists a constant α > 0 such that

    ( Ψ , Ψ ) 𝒞 - 1 α Ψ Σ 2 for all  Ψ Ker B ,

    with

    Ker B = { Ψ Σ : ( B * Ψ , ψ ) V = 0  for all  ψ V } .

  4. ( B * Ψ , ψ ) V satisfies the inf-sup condition: There exists a constant β > 0 such that

    inf 0 ψ V sup 0 Ψ Σ ( B * Ψ , ψ ) V Ψ Σ ψ V β .

These conditions are known as Brezzi’s conditions with constants a , b , α , and β.

The following theorems follow directly from the construction of the space Σ. For completeness, the detailed deductions are provided here. The theorem below shows that the solution of Problem 1 is also a solution of Problem 2, which can be utilized to prove the inf-sup condition of Problem 2.

Theorem 3.1.

Let ϕ W be the solution of Problem 1 for F V . Then Φ = - C B ϕ Σ and ( Φ , ϕ ) solves Problem 2.

Proof.

Recall the L 2 space V s in (3.1). It follows from ϕ W that Φ = - 𝒞 B ϕ V s . Note that ϕ is the solution of Problem 1. Then it holds

( B ψ , Φ ) V s = - S s 𝒗 : 𝝈 d S + S 2 v 3 : 𝑴 d S - ~ S ~ s ~ 𝒗 : ~ 𝝈 d ~ S + ~ S ~ 2 ~ v 3 : ~ 𝑴 d ~ S
= - ( S s 𝒗 : 𝝈 d S + S ( - 2 v 3 ) : 𝑴 d S + ~ S ~ s ~ 𝒗 : ~ 𝝈 d ~ S + ~ S ( - ~ 2 ~ v 3 ) : ~ 𝑴 d ~ S )
= - D ( ϕ , ψ ) = - ( F , ψ ) V for all  ψ = ( 𝒗 , v 3 ; ~ 𝒗 , ~ v 3 ) W .

Since F V , this implies that Φ Σ by the definition of Σ in (3.7), and that the second equation of Problem 2 is satisfied by noting that W is dense in V.

For any Ψ = ( 𝝉 , 𝜿 ; ~ 𝝉 , ~ 𝜿 ) Σ , it follows from (3.6) that

( B * Ψ , ϕ ) V = ( B ϕ , Ψ ) V s
= - S s 𝒖 : 𝝉 d S + S 2 u 3 : 𝜿 d S - ~ S ~ s ~ 𝒖 : ~ 𝝉 d ~ S + ~ S ~ 2 ~ u 3 : ~ 𝜿 d ~ S
= - S 𝒞 1 - 1 𝝈 : 𝝉 d S - S 𝒞 2 - 1 𝑴 : 𝜿 d S - ~ S 𝒞 1 - 1 ~ 𝝈 : ~ 𝝉 d ~ S - ~ S 𝒞 2 - 1 ~ 𝑴 : ~ 𝜿 d ~ S
= - ( Φ , Ψ ) 𝒞 - 1 .

This proves the first equation of Problem 2 and completes the proof. ∎

Theorem 3.2.

Brezzi’s conditions (1)–(4) hold for Problem 2.

Proof.

Define λ min ( 𝒞 i ) and λ max ( 𝒞 i ) as the minimum and the maximum eigenvalue of 𝒞 i for i = 1 , 2 , respectively. Let

λ min ( 𝒞 ) min { λ min ( 𝒞 1 ) , λ min ( 𝒞 2 ) } , λ max ( 𝒞 ) max { λ max ( 𝒞 1 ) , λ max ( 𝒞 2 ) } .

The verification of Brezzi’s conditions (1)–(3) is straightforward by assigning constants a = 1 / λ min ( 𝒞 ) , b = 1 and α = 1 / λ max ( 𝒞 ) . To prove the inf-sup condition (4), let ϕ ψ be the solution of Problem 1 with the right-hand side F ψ = - ψ V for a fixed but arbitrary ψ V . Theorem 3.1 shows that Φ ψ = - 𝒞 B ϕ ψ Σ , and ( Φ ψ , ϕ ψ ) is a solution of Problem 2. It follows from the second equation of Problem 2 that

(3.8) ( B * Φ ψ , ψ ) V = - ( F ψ , ψ ) V = ( ψ , ψ ) V = ψ V 2

and B * Φ ψ V = ψ V . Additionally, one can obtain

Φ ψ V s 2 = 𝒞 1 s 𝒖 ψ 0 , S 2 + 𝒞 2 2 u 3 ψ 0 , S 2 + 𝒞 1 ~ s ~ 𝒖 ψ 0 , ~ S 2 + 𝒞 2 ~ 2 ~ u 3 ψ 0 , ~ S 2
λ max ( 𝒞 ) D ( ϕ ψ , ϕ ψ ) = λ max ( 𝒞 ) ( F ψ , ϕ ψ ) V .

Lemma 2.1 shows ϕ ψ W C F ψ V . Then

Φ ψ V s 2 C λ max ( 𝒞 ) F ψ V 2 = C λ max ( 𝒞 ) ψ V 2 .

Hence,

(3.9) Φ ψ Σ 2 = Φ ψ V s 2 + B * Φ ψ V 2 ( 1 + C λ max ( 𝒞 ) ) ψ V 2 .

The combination of (3.8) and (3.9) gives

sup 0 Ψ Σ ( B * Ψ , ψ ) V Ψ Σ ( B * Φ ψ , ψ ) V Φ ψ Σ ( 1 + C λ max ( 𝒞 ) ) - 1 2 ψ V ,

which completes the proof with β = ( 1 + C λ max ( 𝒞 ) ) - 1 2 . ∎

Theorem 3.3.

For F V , Problem 1 and Problem 2 are equivalent in the following sense: If ϕ solves Problem 1, then Φ = - C B ϕ Σ and ( Φ , ϕ ) solves Problem 2. Conversely, if ( Φ , ϕ ) solves Problem 2, then ϕ W and solves Problem 1.

Proof.

Both Problem 1 and 2 are uniquely solvable due to Lemma 2.1 and Theorem 3.2. Thus, it suffices to demonstrate that the solution of one of the problems is also a solution of the other, which is already proven in Theorem 3.1. ∎

3.3 Continuity Conditions

For the finite element discretization of Σ, a characterization of the boundary and continuity conditions of smooth functions in Σ is provided. Introduce the space

C s { Ψ = ( 𝝉 , 𝜿 ; ~ 𝝉 , ~ 𝜿 ) : ( 𝝉 , 𝜿 ) C 0 ( S ¯ ; 𝕊 ) × C 1 ( S ¯ ; 𝕊 ) , ( ~ 𝝉 , ~ 𝜿 ) C 0 ( ~ S ¯ ; 𝕊 ) × C 1 ( ~ S ¯ ; 𝕊 ) } .

Here S ¯ denotes the closure of S. The following theorem shows that the natural conditions in Problem 1 become essential conditions in Problem 2, which are hidden within the definition of Σ in (3.7) and can be explicitly extracted for smooth enough functions Φ. Let 𝒱 S denote the set that contains all corner points x where exist two adjacent edges e 1 , e 2 S and [ [ M n t ] ] x be defined similarly as in (2.3) for x S .

Theorem 3.4.

Let Φ C s . Then Φ Σ if and only if Φ satisfies the free boundary conditions (2.5b)–(2.5c) and the junction conditions (2.6c)–(2.6e).

Proof.

For Φ C s , define the linear functional G acting on ψ = ( 𝒗 , v 3 ; ~ 𝒗 , ~ v 3 ) W as

(3.10) ( G , ψ ) V ( B ψ , Φ ) V .

It follows from the definition of B in (3.2) that

(3.11) ( B ψ , Φ ) V = I S + I ~ S ( - S 𝝈 : s 𝒗 d S + S 𝑴 : 2 v 3 d S ) + ( - ~ S ~ 𝝈 : ~ s ~ 𝒗 d ~ S + ~ S ~ 𝑴 : ~ 2 ~ v 3 d ~ S ) .

An integration by parts and Φ C s show

(3.12)

- S 𝝈 : s 𝒗 d S = S Div 𝝈 𝒗 d S - S 𝝈 𝒏 𝒗 d s ,
S 𝑴 : 2 v 3 d S = S divDiv 𝑴 v 3 d S - S Div 𝑴 𝒏 v 3 d s
+ S M n n n v 3 d s - S t M n t v 3 d s + x 𝒱 S [ [ M n t ] ] x v 3 ( x ) .

Note that S = S 0 S 1 Γ and recall W in (2.7). Substituting (3.12) into I S in (3.11) gives

(3.13) I S = S Div 𝝈 𝒗 d S + S divDiv 𝑴 v 3 d S + I 1 + I 2 + I 3 + I 4

with

(3.14)

I 1 - S 𝝈 𝒏 𝒗 d s = - S 1 𝝈 𝒏 𝒗 d s - Γ 𝝈 𝒏 𝒗 d s ,
I 2 S M n n n v 3 d s = S 1 M n n n v 3 d s + Γ M n n n v 3 d s ,
I 3 - S T v 3 d s = - S 1 T v 3 d s - Γ T v 3 d s ,
I 4 x 𝒱 S [ [ M n t ] ] x v 3 ( x ) = x 𝒱 S 1 [ [ M n t ] ] x v 3 ( x ) + x Γ [ [ M n t ] ] x v 3 ( x ) .

Similarly, due to ~ S = ~ S 1 Γ , it holds

(3.15) I ~ S = ~ S ~ Div ~ 𝝈 ~ 𝒗 d ~ S + ~ S ~ divDiv ~ 𝑴 ~ v 3 d ~ S + ~ I 1 + ~ I 2 + ~ I 3 + ~ I 4

with

~ I 1 - ~ S 1 ~ 𝝈 ~ 𝒏 ~ 𝒗 d ~ s - Γ ~ 𝝈 ~ 𝒏 ~ 𝒗 d ~ s , ~ I 2 ~ S 1 ~ M ~ n ~ n ~ ~ n ~ v 3 d ~ s + Γ ~ M ~ n ~ n ~ ~ n ~ v 3 d ~ s ,
~ I 3 - ~ S 1 ~ T ~ v 3 d ~ s - Γ ~ T ~ v 3 d ~ s , ~ I 4 x 𝒱 ~ S 1 [ [ ~ M ~ n ~ t ] ] x ~ v 3 ( x ) + x Γ [ [ ~ M ~ n ~ t ] ] x ~ v 3 ( x ) .

It should be emphasized that the integral directions on Γ for S and ~ S are opposite, as dictated by the definition of local coordinate systems in Section 2.1. Recall that ψ W satisfies

(3.16) n v 3 + ~ ~ n ~ v 3 = 0 , v 1 = ~ v 1 cos θ - ~ v 3 sin θ , v 2 = - ~ v 2 , v 3 = - ~ v 1 sin θ - ~ v 3 cos θ .

The substitution of (3.13) and (3.15) into (3.11) combined with (3.16) lead to

(3.17)

( G , ψ ) V = I d + I b + I j + I c ,

with

I d S Div 𝝈 𝒗 d S + S divDiv 𝑴 v 3 d S + ~ S ~ Div ~ 𝝈 ~ 𝒗 d ~ S + ~ S ~ divDiv ~ 𝑴 ~ v 3 d ~ S ,
I b - S 1 𝝈 𝒏 𝒗 d s + S 1 M n n n v 3 d s - S 1 T v 3 d s + x 𝒱 S 1 [ [ M n t ] ] x v 3 ( x )
- ~ S 1 ~ 𝝈 ~ 𝒏 ~ 𝒗 d ~ s + ~ S 1 ~ M ~ n ~ n ~ ~ n ~ v 3 d ~ s - ~ S 1 ~ T ~ v 3 d ~ s + x 𝒱 ~ S 1 [ [ ~ M ~ n ~ t ] ] x ~ v 3 ( x ) ,
I j Γ ( - σ n n cos θ - ~ σ ~ n ~ n + T sin θ ) ~ v 1 d s + Γ ( σ n t - ~ σ ~ n ~ t ) ~ v 2 d s
+ Γ ( σ n n sin θ + T cos θ - ~ T ) ~ v 3 d s + Γ ( M n n - ~ M ~ n ~ n ) ~ ~ n ~ v 3 d s ,
I c x Γ [ [ M n t ] ] x ~ v 1 ( x ) sin θ + x Γ ( [ [ M n t ] ] x - [ [ ~ M ~ n ~ t ] ] x cos θ ) ~ v 3 ( x ) .

The only if implications follow immediately from (3.17). To be specific, assume that Φ satisfies the boundary conditions (2.5b)–(2.5c) and junction conditions (2.6c)–(2.6e). Then it follows that

( G , ψ ) V = I d = ( B * Φ , ψ ) V B * Φ V ψ V for all  ψ W .

Hence, G is a linear bounded functional on V and Φ Σ .

For the if implications, assume Φ Σ , then the functional G given by (3.10) is bounded with respect to the V-norm, for all ψ W . Introduce the space

W ¯ = { Ψ = ( 𝒗 , v 3 ; ~ 𝒗 , ~ v 3 ) : Ψ W  and  𝒗 , v 3 , n v 3 = 0  on  S  and  ~ 𝒗 , ~ v 3 , ~ n ~ v 3 = 0  on  ~ S } .

It is easy to verify that W ¯ W and W ¯ is dense in W with respect to the V-norm. For ψ W ¯ , it follows from (3.17) that

(3.18) ( G , ψ ) V = I d for all  ψ W ¯ .

Then one can obtain that (3.18) holds for ψ W . This together with (3.17) imply that

I b + I j + I c = 0 for all  ψ W .

This and standard arguments lead to (2.5b)–(2.5c) and (2.6c)–(2.6e). ∎

4 Mixed Finite Element Method

This section presents a conforming mixed finite element method for Problem 2. The discrete stability and error estimates of the mixed finite element method are provided under reasonable assumptions. An illustrative example is given. Numerical examples are provided to verify the theoretical results.

4.1 Mixed Finite Element Method

Let 𝒯 h and ~ 𝒯 h be a shape regular triangulation of S and ~ S , respectively, which satisfy the compatibility conditions on Γ. Let h be the maximum of the diameters of all the elements K 𝒯 h and ~ K ~ 𝒯 h . Denote by ( K ) the set of all edges of K and 𝒱 ( K ) the set of all vertices of K. Let Σ h 1 × V h 1 H ( div , S ; 𝕊 ) × L 2 ( S ; 2 ) and Σ h 2 × V h 2 H ( divDiv , S ; 𝕊 ) × L 2 ( S ) be two conforming finite element spaces for S. Let ~ Σ h 1 × ~ V h 1 H ( div , ~ S ; 𝕊 ) × L 2 ( ~ S ; 2 ) and ~ Σ h 2 × ~ V h 2 H ( divDiv , ~ S ; 𝕊 ) × L 2 ( ~ S ) be defined in a similar way except that these spaces are defined on ~ S . Recall the definitions of V in (2.9) and H s in (3.3). Then the discrete spaces for two coupled plates can be given by

(4.1)

Σ h { Ψ h = ( 𝝉 h , 𝜿 h ; ~ 𝝉 h , ~ 𝜿 h ) H s : ( 𝝉 h , 𝜿 h ) Σ h 1 × Σ h 2 , ( ~ 𝝉 h , ~ 𝜿 h ) ~ Σ h 1 × ~ Σ h 2 ,
Ψ h  satisfies the conditions in Theorem 3.4 }

and

(4.2) V h { ψ h = ( 𝒗 h , v 3 h ; ~ 𝒗 h , ~ v 3 h ) V : ( 𝒗 h , v 3 h ) V h 1 × V h 2 , ( ~ 𝒗 h , ~ v 3 h ) ~ V h 1 × ~ V h 2 } .

The discrete mixed formulation for Problem 2 is as follows.

Problem 3.

Given F V , find Φ h ( 𝝈 h , 𝑴 h ; ~ 𝝈 h , ~ 𝑴 h ) Σ h and ϕ h ( 𝒖 h , u 3 h ; ~ 𝒖 h , ~ u 3 h ) V h such that

( Φ h , Ψ h ) 𝒞 - 1 + ( B * Ψ h , ϕ h ) V = 0 for all  Ψ h Σ h ,
( B * Φ h , ψ h ) V = - ( F , ψ h ) V for all  ψ h V h .

The following assumptions are proposed for the discrete stability of Problem 3.

Assumption (A1).

For all ψ h V h , there exists a Φ Σ ~ Σ equipped with the norm Σ ~ with extra regularity compared to Σ such that B * Φ = ψ h .

Assumption (A2).

There exists a Fortin operator Π h : Σ ~ Σ h such that

Q h B * Φ = B * Π h Φ ,

where Q h is the L 2 projection from V to V h , namely,

( B * Φ , ψ h ) V = ( B * Π h Φ , ψ h ) V for all  ψ h V h .

The stability Π h Φ Σ C Φ Σ ~ holds with a constant C.

Theorem 4.1.

Problem 3 is well-posed under Assumptions (A1)(A2).

Proof.

It is easy to verify that ( Φ h , Ψ h ) 𝒞 - 1 is a symmetric, nonnegative bilinear form. It remains to show that Brezzi’s conditions hold for Problem 3, which can be derived from the continuous counterpart with the help of a Fortin operator, e.g., [10]. The proof is completed by Theorem 3.2 and Assumptions (A1)(A2). ∎

Following the standard procedures in [10], the well-posedness of Problem 3 allows the following error estimate.

Theorem 4.2.

Let ( Φ , ϕ ) ( Σ , V ) be the solution of Problem 2 and let ( Φ h , ϕ h ) ( Σ h , V h ) be the solution of Problem 3. Then there exists a constant C independent of mesh-size h such that

Φ - Φ h Σ + ϕ - ϕ h V C inf Ψ h Σ h , ψ h V h ( Φ - Ψ h Σ + ϕ - ψ h V ) .

4.2 An Example

This subsection provides a specific example of Σ h and V h . Under some regularity Assumption (A1), Assumption (A2) is proved. With a slight abuse of notation, introduce the following symbols in this subsection

T ( ) Div ( ) 𝒏 + t ( ( ( ) 𝒏 ) 𝒕 ) , ( ) n n ( ( ) 𝒏 ) 𝒏 , ( ) n t ( ( ) 𝒏 ) 𝒕 .

Recall the continuity conditions (2.6c)–(2.6e) in Theorem 3.4 as follows:

~ M ~ n ~ n = M n n on  Γ , ~ σ ~ n ~ n = - σ n n cos θ + T sin θ , ~ σ ~ n ~ t = σ n t , ~ T = σ n n sin θ + T cos θ on  Γ .
[ [ M n t ] ] x sin θ = 0 , [ [ ~ M ~ n ~ t ] ] x - [ [ M n t ] ] x cos θ = 0 for all  x Γ .

It can be observed that the junction conditions contain the terms σ n n , σ n t , M n n , T , M n t . For ease of programming implementation, the conforming H ( div , 𝕊 ) × L 2 ( 2 ) mixed elements in [25] and the conforming H ( divDiv , 𝕊 ) × L 2 mixed elements in [11], containing degrees of freedom of these terms, are chosen for S and ~ S in this subsection. The spaces defined on S with similar notations for ~ S are detailed here.

Let Σ h 1 × V h 1 H ( div , S ; 𝕊 ) × L 2 ( S ; 2 ) denote the mixed finite element space in [25]. For k 2 ,

V h 1 = { 𝒗 h L 2 ( S ; 2 ) : 𝒗 h | K P k ( K ; 2 )  for all  K 𝒯 h } .

The degrees of freedom of 𝝉 Σ h 1 defined on element K are

(4.3)

(4.3a) 𝝉 ( x ) for all  x 𝒱 ( K ) ,
(4.3b) ( 𝝉 𝒏 , 𝒒 ) e for all  𝒒 P k - 1 ( e ; 2 ) , e ( K ) ,
(4.3c) ( 𝝉 , 𝝇 ) K for all  𝝇 P k - 2 ( K ; 𝕊 )  with  𝝇 𝒏  vanish on  K .

Then the space is given by

Σ h 1 = { 𝝉 h H ( div , S ; 𝕊 ) : 𝝉 h | K P k + 1 ( K ; 𝕊 )  for all  K 𝒯 h ,
all the degrees of the freedom (4.3a)–(4.3b) are single-valued } .

Let Σ h 2 × V h 2 H ( divDiv , S ; 𝕊 ) × L 2 ( S ) denote the mixed finite element space in [11]. For k 2 ,

V h 2 = { v 3 h L 2 ( S ) : v 3 h | K P k ( K )  for all  K 𝒯 h } .

The degrees of freedom of 𝜿 Σ h 2 defined on element K are

(4.4)

(4.4a) 𝜿 ( x ) for all  x 𝒱 ( K ) ,
(4.4b) ( 𝜿 n n , q ) e for all  q P k ( e ) , e ( K ) ,
(4.4c) ( T ( 𝜿 ) , q ) e for all  q P k + 1 ( e ) , e ( K ) ,
(4.4d) ( 𝜿 , 𝝇 ) K for all  𝝇 2 P k ( K ) sym ( x P k ( K ; 2 ) ) ,

where sym ( ) denotes the symmetric part of a tensor and x = ( x 1 , x 2 ) = ( - x 2 , x 1 ) . Then the space is given by

Σ h 2 = { 𝜿 h H ( divDiv , S ; 𝕊 ) : 𝜿 h | K P k + 2 ( K ; 𝕊 )  for all  K 𝒯 h ,
all the degrees of the freedom (4.4a)–(4.4c) are single-valued } .

According to Theorem 4.1, the discrete stability of the mixed finite elements of Σ h × V h defined on (4.1)–(4.2) can be derived by Assumptions (A1)(A2). Introduce the following space with extra regularities compared to Σ as

Σ ~ = { Ψ = ( 𝝉 , 𝜿 ; ~ 𝝉 , ~ 𝜿 ) Σ : ( 𝝉 , 𝜿 ) H 1 ( S ; 𝕊 ) × H 2 ( S ; 𝕊 ) , ( ~ 𝝉 , ~ 𝜿 ) H 1 ( ~ S ; 𝕊 ) × H 2 ( ~ S ; 𝕊 ) }

equipped with the norm

Ψ Σ ~ = ( 𝝉 1 , S 2 + 𝜿 2 , S 2 + ~ 𝝉 1 , ~ S 2 + ~ 𝜿 2 , ~ S 2 ) 1 2 .

Assume that for any ψ h V h , there exists a Φ Σ ~ satisfying Assumption (A1). It remains to construct an appropriate interpolation operator satisfying Assumption (A2). Introduce the interpolation operator Π 1 in [21, Remark 3.1] for Σ h 1 . Given 𝝈 H 1 ( S ; 𝕊 ) , note that Π 1 𝝈 ( x ) is defined as an average value on an edge at the vertex x. To satisfy the zero boundary condition 𝝈 𝒏 = 0 on S 1 and continuity conditions (2.6d) in Theorem 3.4, modify Π 1 related to degrees of freedom (4.3a) for any K 𝒯 h by

Π 1 𝝈 ( x ) = 0 for all  x 𝒱 ( K ) ( Γ S 1 ) .

Let Q k be the L 2 projection onto piecewise P k polynomials. The modified operator Π 1 does satisfy the commuting property

(4.5) div Π 1 𝝈 = Q k div 𝝈 .

Introduce Π 2 in [11, Section 3.3] for Σ h 2 , which is defined as the nodal interpolation operator based on the degrees of freedom (4.4a)-(4.4d). Corresponding to the modifications of Π 1 , to satisfy the continuity conditions (2.6d), modify Π 2 related to degrees of freedom (4.4c) for any K 𝒯 h by

(4.6)

(4.6a) T ( Π 2 𝑴 ) ( x ) = 0 for all  x 𝒱 ( K ) Γ ,
(4.6b) ( T ( Π 2 𝑴 ) , q ) e = ( T ( 𝑴 ) , q ) e for all  q P k - 1 ( e ) , e ( K ) Γ .

Lemma 4.3.

There exists a stable interpolation operator Π ^ 2 : H 2 ( S ; S ) Σ h 2 such that

divDiv ( Π ^ 2 𝑴 ) = Q k divDiv ( 𝑴 ) for all  𝑴 H 2 ( S ; 𝕊 ) ,

and Π ^ 2 𝐌 0 , S C 𝐌 2 , S with a positive constant C.

Proof.

Given any K 𝒯 h , Green’s formula in [11, Lemma 2.1] shows that

(4.7) K divDiv ( 𝑴 - Π 2 𝑴 ) q d x = K T ( 𝑴 - Π 2 𝑴 ) q d x - K ( 𝑴 - Π 2 𝑴 ) n n q n d x + x 𝒱 ( K ) [ [ ( 𝑴 - Π 2 𝑴 ) n t ] ] x q ( x )

holds for any q P 1 ( K ) . The combination of (4.4a)–(4.4b) shows that the last two terms in (4.7) vanish. This and (4.6b) show

divDiv ( 𝑴 - Π 2 𝑴 ) P k ( K ) / P 1 ( K ) .

Let Σ b , K denote the space

Σ b , K { 𝜿 P k + 2 ( K ; 𝕊 ) : all degrees of freedom (4.4a)–(4.4c) vanish } .

Since divDiv Σ b , K = P k ( K ) / P 1 ( K ) [11, (24)], one can select 𝜿 1 Σ b , K by

𝜿 1 0 , K = min { 𝜿 0 , K , divDiv 𝜿 = divDiv ( 𝑴 - Π 2 𝑴 ) } .

The proof is concluded by defining ( Π ^ 2 𝑴 ) | K ( Π 2 𝑴 ) | K + 𝜿 1 . ∎

Let ~ Π 1 and ~ Π ^ 2 be defined for ~ S in a similar way. Define

Π h Φ ( Π 1 𝝈 , Π ^ 2 𝑴 ; ~ Π 1 ~ 𝝈 , ~ Π ^ 2 ~ 𝑴 ) .

The combination of (4.5) and Lemma 4.3 shows that Π h satisfies the commuting property in Assumption (A2), and the stability inequality

Π h Φ Σ C Φ Σ ~

with a constant C. This concludes the proof of the discrete stability for these pairs Σ h × V h with k 2 .

4.3 Numerical Tests

This subsection gives two numerical experiments to verify the theoretical results established in Theorem 4.2. The conforming mixed finite elements with k = 2 in the last subsection will be used.

As shown on the left of Figure 2, the degrees of freedom defined in (4.3) are indicated by black points, double arrows, and nine H ( div , 𝕊 ) -bubble functions, respectively. On the left of Figure 3, the degrees of freedom defined in (4.4) are indicated by black points at three vertices, black points in the interior of each edge, arrows, and fifteen H ( divDiv , 𝕊 ) -bubble functions, respectively. For each midsurface S and ~ S , the implementation follows the similar procedures of mixed finite element methods for a single plate. As mentioned in Theorem 3.4, the only difference is to deal with the junction conditions (2.6c)–(2.6e). For the junction condition (2.6c), i.e., M n n = ~ M ~ n ~ n on Γ. The restriction of these functions to Γ are polynomials of degree four in one variable. Thus, it suffices to satisfy (2.6c) at the three points inside the edge together with two endpoints. For the junction condition (2.6d), similarly, it suffices to satisfy these conditions at the points related to the degrees of freedom.

Figure 2

Left and Right are degrees of freedom for a P 3 - H ( div , 𝕊 ) element and a discontinuous vectorial P 2 element, respectively.

Figure 3

Left and Right are degrees of freedom for a P 4 - H ( divDiv , 𝕊 ) element and a discontinuous P 2 element, respectively.

Example 4.4.

Consider two coupled plates shown in Figure 1 with two local coordinates ( 𝒏 , 𝒕 , 𝒍 ) and ( ~ 𝒏 , ~ 𝒕 , ~ 𝒍 ) located at the middle point of Γ. The domains in local coordinates are S = ( - 1 , 0 ) × ( - 1 , 1 ) , ~ S = ( - 1 , 0 ) × ( - 1 , 1 ) and the angle θ = π / 2 . In this example, E = 3000 , ν = 0 , e = 0.124 . Let the exact solution be chosen as

(4.8)

( 𝒖 , u 3 ) = ( - ( 1 - x 2 ) 2 ( 1 - y 2 ) 2 , ( 1 - x 2 ) 2 ( 1 - y 2 ) 2 , ( 1 - x 2 ) 2 ( 1 - y 2 ) 2 ) ,
( ~ 𝒖 , ~ u 3 ) = ( - ( 1 - ~ x 2 ) 2 ( 1 - ~ y 2 ) 2 , - ( 1 - ~ x 2 ) 2 ( 1 - ~ y 2 ) 2 , ( 1 - ~ x 2 ) 2 ( 1 - ~ y 2 ) 2 ) .

The external force F, the boundary forces, and moments in equations (2.5b)–(2.5c) can be determined through straightforward calculations. It can be verified that the solution (4.8) satisfies the clamped boundary condition (2.5a) on S 0 and junction conditions (2.6a)–(2.6c) on Γ. Nevertheless, this solution fails to satisfy the homogeneous junction condition σ n t - ~ σ ~ n ~ t = 0 on Γ, while it does satisfy σ n t - ~ σ ~ n ~ t = 2 σ n t . Consequently, the junction condition in this example is nonhomogeneous.

Theorem 4.2 shows that the following error estimate result

Φ - Φ h Σ + ϕ - ϕ h V C h 3

holds for the case k = 2 . It is observed from Table 1 that the convergence rates of ( 𝝈 , 𝑴 ) and ( 𝒖 , u 3 ) for the middle surface S are both O ( h 3 ) in the norms of Σ and V, respectively. Moreover, the rates of ( 𝝈 , 𝑴 ) in L 2 norms are O ( h 4 ) and O ( h 5 ) , both of which are optimal. The mesh is uniformly refined. For the middle surface ~ S , the similar conclusion can be derived from Table 2. These numerical results coincide with the theoretical result in Theorem 4.2.

Table 1

Errors on S for Example 4.4.

Mesh 𝝈 - 𝝈 h 0 Order 𝒖 - 𝒖 h 0 Order 𝝈 - 𝝈 h H ( div ) Order
1 3.85439 E + 01 6.31904 E - 02 1.37373 E + 02
2 3.86755 E + 00 3.32 1.02984 E - 02 2.62 2.07569 E + 01 2.73
3 2.69636 E - 01 3.84 1.36836 E - 03 2.91 2.76788 E + 00 2.91
4 1.71509 E - 02 3.97 1.73916 E - 04 2.98 3.51847 E - 01 2.98
5 1.07473 E - 03 4.00 2.18326 E - 05 2.99 4.41676 E - 02 2.99
𝑴 - 𝑴 h 0 Order u 3 - u 3 h 0 Order 𝑴 - 𝑴 h H ( divDiv ) Order
1 1.83015 E - 01 4.27046 E - 02 3.18201 E + 00
2 7.75092 E - 03 4.56 7.24994 E - 03 2.56 4.34361 E - 01 2.87
3 2.70767 E - 04 4.84 9.67331 E - 04 2.91 5.53801 E - 02 2.97
4 8.35573 E - 06 5.02 1.22977 E - 04 2.98 6.95601 E - 03 2.99
5 2.50436 E - 07 5.06 1.54381 E - 05 2.99 8.70545 E - 04 3.00
Table 2

Errors on ~ S for Example 4.4.

Mesh ~ 𝝈 - ~ 𝝈 h 0 Order ~ 𝒖 - ~ 𝒖 h 0 Order ~ 𝝈 - ~ 𝝈 h H ( ~ div ) Order
1 3.04348 E + 01 6.18553 E - 02 2.23788 E + 02
2 3.16175 E + 00 3.27 1.02746 E - 02 2.59 4.34492 E + 01 2.36
3 2.22673 E - 01 3.83 1.36833 E - 03 2.91 6.04352 E + 00 2.85
4 1.42905 E - 02 3.96 1.73919 E - 04 2.98 7.75373 E - 01 2.96
5 8.97872 E - 04 3.99 2.18328 E - 05 2.99 9.75505 E - 02 2.99
~ 𝑴 - ~ 𝑴 h 0 Order ~ u 3 - ~ u 3 h 0 Order ~ 𝑴 - ~ 𝑴 h H ( ~ divDiv ) Order
1 3.88066 E - 01 4.25016 E - 02 3.18201 E + 00
2 1.61729 E - 02 4.58 7.24375 E - 03 2.55 4.34361 E - 01 2.87
3 4.39241 E - 04 5.20 9.67361 E - 04 2.90 5.53801 E - 02 2.97
4 1.18672 E - 05 5.21 1.22980 E - 04 2.98 6.95601 E - 03 2.99
5 3.66826 E - 07 5.02 1.54382 E - 05 2.99 8.70545 E - 04 3.00

Example 4.5.

This example compares different finite element methods for solving two coupled plates with the rigid junction Γ shown in Figure 4. Given the global coordinate ( X , Y , Z ) , the left one S is clamped on S 0 while the right one is loaded along one edge of ~ S 1 by a line density of forces P z = - 1 lb/in in global coordinate. In this example, E = 3 × 10 7 psi, ν = 0 , α = 30 , e = 0.124 in. The length and width of the plates are shown in Figure 4. Calculate the displacements of points A ( 0 , 2.52 cos α ) , B ( 1 / 3 , 2.52 cos α ) , C ( 2 / 3 , 2.52 cos α ) , and D ( 1 , 2.52 cos α ) in the global Z-axis. Figure 5 shows the first mesh and the mesh is uniformly refined.

Figure 4

The coupled plates with the rigid junction of Example 4.5.

Figure 5

The first mesh of Example 4.5.

Table 3

Results obtained by different finite element methods.

Displacement in the Global Z-Axis
Mesh A B C D
Mixed Method 1 - 8.35998E - 4 - 8.38402E - 4 - 8.40832E - 4 - 8.43207E - 4
2 - 8.37679E - 4 - 8.38905E - 4 - 8.40137E - 4 - 8.41361E - 4
3 - 8.38579E - 4 - 8.39198E - 4 - 8.39819E - 4 - 8.40438E - 4
4 - 8.39040E - 4 - 8.39351E - 4 - 8.39663E - 4 - 8.39974E - 4
5 - 8.39273E - 4 - 8.39429E - 4 - 8.39585E - 4 - 8.39741E - 4
Displacement Method 1 - 8.37038E - 4 - 8.37025E - 4 - 8.37024E - 4 - 8.37002E - 4
2 - 8.38927E - 4 - 8.38907E - 4 - 8.38897E - 4 - 8.38889E - 4
3 - 8.39369E - 4 - 8.39359E - 4 - 8.39355E - 4 - 8.39354E - 4
4 - 8.39474E - 4 - 8.39470E - 4 - 8.39469E - 4 - 8.39470E - 4
5 - 8.39499E - 4 - 8.39498E - 4 - 8.39497E - 4 - 8.39498E - 4

Table 3 displays the displacements of four points computed by two different finite element methods. It shows that the displacements calculated using the mixed finite element method, as mentioned at the beginning of this subsection, converge to - 8.395 × 10 - 4 in. Moreover, the displacements obtained by the conforming finite element method based on the displacement formulation, reduced Hermite element and reduced HCT element in [8], converge to -8.395E-4 in. These results demonstrate that the displacements of the cantilever plate computed by the mixed finite element method are in good agreement with the results obtained from the method based on the displacement formulation.

Award Identifier / Grant number: 12288101

Award Identifier / Grant number: 12301466

Funding statement: The first author was supported by the National Natural Science Foundation of China project 12288101. The third author was supported by the National Natural Science Foundation of China project 12301466.

References

[1] S. Adams and B. Cockburn, A mixed finite element method for elasticity in three dimensions, J. Sci. Comput. 25 (2005), no. 3, 515–521. 10.1007/s10915-004-4807-3Search in Google Scholar

[2] D. N. Arnold and G. Awanou, Rectangular mixed finite elements for elasticity, Math. Models Methods Appl. Sci. 15 (2005), no. 9, 1417–1429. 10.1142/S0218202505000741Search in Google Scholar

[3] D. N. Arnold, G. Awanou and R. Winther, Finite elements for symmetric tensors in three dimensions, Math. Comp. 77 (2008), no. 263, 1229–1251. 10.1090/S0025-5718-08-02071-1Search in Google Scholar

[4] D. N. Arnold and K. Hu, Complexes from complexes, Found. Comput. Math. 21 (2021), no. 6, 1739–1774. 10.1007/s10208-021-09498-9Search in Google Scholar

[5] D. N. Arnold and R. Winther, Mixed finite elements for elasticity, Numer. Math. 92 (2002), no. 3, 401–419. 10.1007/s002110100348Search in Google Scholar

[6] G. Awanou, Two remarks on rectangular mixed finite elements for elasticity, J. Sci. Comput. 50 (2012), no. 1, 91–102. 10.1007/s10915-011-9474-6Search in Google Scholar

[7] K. J. Bathe, Finite Element Procedures in Engineering Analysis, Prentice-Hall, Englewood Cliffs, 1960. Search in Google Scholar

[8] M. Bernadou, S. Fayolle and F. Léné, Numerical analysis of junctions between plates, Comput. Methods Appl. Mech. Engrg. 74 (1989), no. 3, 307–326. 10.1016/0045-7825(89)90054-6Search in Google Scholar

[9] D. Boffi, F. Brezzi and M. Fortin, Reduced symmetry elements in linear elasticity, Commun. Pure Appl. Anal. 8 (2009), no. 1, 95–121. 10.3934/cpaa.2009.8.95Search in Google Scholar

[10] D. Boffi, F. Brezzi and M. Fortin, Mixed Finite Element Methods and Applications, Springer Ser. Comput. Math. 44, Springer, Heidelberg, 2013. 10.1007/978-3-642-36519-5Search in Google Scholar

[11] L. Chen and X. Huang, Finite elements for divdiv-conforming symmetric tensors, preprint (2021), https://arxiv.org/abs/2005.01271v3. Search in Google Scholar

[12] L. Chen and X. Huang, Finite elements for div div conforming symmetric tensors in three dimensions, Math. Comp. 91 (2022), no. 335, 1107–1142. 10.1090/mcom/3700Search in Google Scholar

[13] L. Chen and X. Huang, A new div - div -conforming symmetric tensor finite element space with applications to the biharmonic equation, Math. Comp. 94 (2025), no. 351, 33–72. 10.1090/mcom/3957Search in Google Scholar

[14] S.-C. Chen and Y.-N. Wang, Conforming rectangular mixed finite elements for elasticity, J. Sci. Comput. 47 (2011), no. 1, 93–108. 10.1007/s10915-010-9422-xSearch in Google Scholar

[15] P. G. Ciarlet, Mathematical Elasticity. Volume II. Theory of Plates, Classics Appl. Math. 85, Society for Industrial and Applied Mathematics, Philadelphia, 2022. Search in Google Scholar

[16] K. Feng and Z.-C. Shi, Mathematical Theory of Elastic Structures, Springer, Berlin, 1996. Search in Google Scholar

[17] T. Führer and N. Heuer, Mixed finite elements for Kirchhoff–Love plate bending, Math. Comp. 94 (2025), no. 353, 1065–1099. 10.1090/mcom/3995Search in Google Scholar

[18] T. Führer, N. Heuer and A. H. Niemi, An ultraweak formulation of the Kirchhoff-Love plate bending model and DPG approximation, Math. Comp. 88 (2019), no. 318, 1587–1619. 10.1090/mcom/3381Search in Google Scholar

[19] L. Guo and J. Huang, Adini- Q 1 - P 3 FEM for general elastic multi-structure problems, Numer. Methods Partial Differential Equations 27 (2011), no. 5, 1092–1112. 10.1002/num.20571Search in Google Scholar

[20] J. Hu, A new family of efficient conforming mixed finite elements on both rectangular and cuboid meshes for linear elasticity in the symmetric formulation, SIAM J. Numer. Anal. 53 (2015), no. 3, 1438–1463. 10.1137/130945272Search in Google Scholar

[21] J. Hu, Finite element approximations of symmetric tensors on simplicial grids in n : the higher order case, J. Comput. Math. 33 (2015), no. 3, 283–296. 10.4208/jcm.1412-m2014-0071Search in Google Scholar

[22] J. Hu, Y. Liang, R. Ma and M. Zhang, A family of conforming finite element divdiv complexes on cuboid meshes, Numer. Math. 156 (2024), 1603–1638. 10.1007/s00211-024-01418-7Search in Google Scholar

[23] J. Hu, R. Ma and M. Zhang, A family of mixed finite elements for the biharmonic equations on triangular and tetrahedral grids, Sci. China Math. 64 (2021), no. 12, 2793–2816. 10.1007/s11425-020-1883-9Search in Google Scholar

[24] J. Hu, H. Man and S. Zhang, A simple conforming mixed finite element for linear elasticity on rectangular grids in any space dimension, J. Sci. Comput. 58 (2014), no. 2, 367–379. 10.1007/s10915-013-9736-6Search in Google Scholar

[25] J. Hu and S. Zhang, A family of symmetric mixed finite elements for linear elasticity on triangular grids, preprint (2015), https://arxiv.org/abs/1406.7457. Search in Google Scholar

[26] J. Hu and S. Zhang, A family of symmetric mixed finite elements for linear elasticity on tetrahedral grids, Sci. China Math. 58 (2015), no. 2, 297–307. 10.1007/s11425-014-4953-5Search in Google Scholar

[27] J. Hu and S. Zhang, Finite element approximations of symmetric tensors on simplicial grids in n : The lower order case, Math. Models Methods Appl. Sci. 26 (2016), no. 9, 1649–1669. 10.1142/S0218202516500408Search in Google Scholar

[28] J. Huang, L. Guo and Z. Shi, A finite element method for investigating general elastic multi-structures, Comput. Math. Appl. 53 (2007), no. 12, 1867–1895. 10.1016/j.camwa.2006.08.048Search in Google Scholar

[29] J. Huang, Z. Shi and Y. Xu, Some studies on mathematical models for general elastic multi-structures, Sci. China Ser. A 48 (2005), no. 7, 986–1007. 10.1007/BF02879079Search in Google Scholar

[30] J. Huang, Z. Shi and Y. Xu, Finite element analysis for general elastic multi-structures, Sci. China Ser. A 49 (2006), no. 1, 109–129. 10.1007/s11425-005-0118-xSearch in Google Scholar

[31] W. Krendl and W. Zulehner, A decomposition result for biharmonic problems and the Hellan–Herrmann–Johnson method, Electron. Trans. Numer. Anal. 45 (2016), 257–282. Search in Google Scholar

[32] J. Lai and J. Huang, A finite element method for vibration analysis of elastic plate-plate structures, Discrete Contin. Dyn. Syst. Ser. B 11 (2009), no. 2, 387–419. 10.3934/dcdsb.2009.11.387Search in Google Scholar

[33] J. Lai, J. Huang and Z. Shi, A lumped mass finite element method for vibration analysis of elastic plate-plate structures, Sci. China Math. 53 (2010), no. 6, 1453–1474. 10.1007/s11425-010-3072-1Search in Google Scholar

[34] M. Neunteufel, Mixed finite element methods for nonlinear continuum mechanics and shells, PhD thesis, Technische Universität Wien, 2021. 10.1016/j.cma.2021.113857Search in Google Scholar

[35] M. Neunteufel and J. Schöberl, The Hellan–Herrmann–Johnson and TDNNS methods for linear and nonlinear shells, Computers & Structures 305 (2024), Article ID 107543. 10.1016/j.compstruc.2024.107543Search in Google Scholar

[36] D. Pauly and W. Zulehner, The divDiv-complex and applications to biharmonic equations, Appl. Anal. 99 (2020), no. 9, 1579–1630. 10.1080/00036811.2018.1542685Search in Google Scholar

[37] A. Pechstein and J. Schöberl, Tangential-displacement and normal-normal-stress continuous mixed finite elements for elasticity, Math. Models Methods Appl. Sci. 21 (2011), no. 8, 1761–1782. 10.1142/S0218202511005568Search in Google Scholar

[38] A. S. Pechstein and J. Schöberl, An analysis of the TDNNS method using natural norms, Numer. Math. 139 (2018), no. 1, 93–120. 10.1007/s00211-017-0933-3Search in Google Scholar PubMed PubMed Central

[39] K. Rafetseder and W. Zulehner, A decomposition result for Kirchhoff plate bending problems and a new discretization approach, SIAM J. Numer. Anal. 56 (2018), no. 3, 1961–1986. 10.1137/17M1118427Search in Google Scholar

[40] K. Rafetseder and W. Zulehner, A new mixed approach to Kirchhoff–Love shells, Comput. Methods Appl. Mech. Engrg. 346 (2019), 440–455. 10.1016/j.cma.2018.11.033Search in Google Scholar

[41] S. P. Timoshenko and S. Woinowsky-Krieger, Theory of Plates and Shells. Vol. 2, McGraw-Hill, New York, 1959. Search in Google Scholar

[42] L. H. Wang, A mathematical model of coupled plates and its finite element method, Comput. Methods Appl. Mech. Engrg. 99 (1992), no. 1, 43–59. 10.1016/0045-7825(92)90122-ZSearch in Google Scholar

[43] L. H. Wang, Mathematical model of coupled plates meeting at an angle 0 < θ < π and its finite element method, Numer. Methods Partial Differential Equations 9 (1993), no. 1, 13–22. 10.1002/num.1690090103Search in Google Scholar

[44] X. Ye and S. Zhang, A family of H-div-div mixed triangular finite elements for the biharmonic equation, Results Appl. Math. 15 (2022), Article ID 100318. 10.1016/j.rinam.2022.100318Search in Google Scholar

Received: 2024-10-30
Accepted: 2025-04-11
Published Online: 2025-04-30
Published in Print: 2025-07-01

© 2025 Institute of Mathematics of the National Academy of Science of Belarus, published by De Gruyter, Berlin/Boston

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