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Article

On the Crossing Bridge between Two Kirchhoff–Love Plates

by
Alexander Khludnev
1,2
1
Institute of Hydrodynamics of SB RAS, 630090 Novosibirsk, Russia
2
Sobolev Institute of Mathematics of SB RAS, 630090 Novosibirsk, Russia
Axioms 2023, 12(2), 120; https://doi.org/10.3390/axioms12020120
Submission received: 2 December 2022 / Revised: 13 January 2023 / Accepted: 18 January 2023 / Published: 26 January 2023
(This article belongs to the Special Issue Differential Equations in Applied Mathematics)

Abstract

:
The paper is concerned with equilibrium problems for two elastic plates connected by a crossing elastic bridge. It is assumed that an inequality-type condition is imposed, providing a mutual non-penetration between the plates and the bridge. The existence of solutions is proved, and passages to limits are justified as the rigidity parameter of the bridge tends to infinity and to zero. Limit models are analyzed. The inverse problem is investigated when both the displacement field and the elasticity tensor of the plate are unknown. In this case, additional information concerning a displacement of a given point of the plate is assumed be given. A solution existence of the inverse problem is proved.

1. Introduction

Bridged structures are very popular for solving connecting problems. Such structures may be different in type, and their quality depends on the purposes addressed. In this paper, we analyze the structure consisting of two Kirchhoff–Love elastic plates and a junction (bridge) that is in contact with the plates. To describe the behavior of the bridge, we use the Euler–Bernoulli beam model. The junction has the displacement coinciding with the displacement of the plates at two fixed points. Moreover, an inequality-type restriction is assumed to be imposed for the solution to provide a mutual non-penetration between the plates and the bridge. This approach implies that the problem is formulated as a free boundary one.
During the last years, boundary-value problems in elasticity with inequality-type boundary conditions have been under active study. We can refer the reader to the books [1,2] containing results for crack models with the non-penetration boundary conditions for a wide class of elasticity problems. There are many papers related to thin inclusions incorporated into elastic bodies. In the case of delamination of the surrounding elastic body from the inclusion, one more difficulty appears since we obtain an interfacial crack. We pay attention to the paper [3] where an equilibrium problem for two elastic plates is analyzed in the case of thin incorporated inclusion and Neumann type boundary conditions for the plate. Different properties of solutions in equilibrium problems for elastic bodies with thin rigid, semi-rigid, and elastic inclusions and cracks are analyzed in [4,5,6,7,8,9,10,11,12,13] and many other papers. In [14,15,16], one can find models for the analysis of non-homogeneous elastic bodies. Note that a derivation of models for elastic bodies with thin inclusions usually takes into account changing physical and geometrical parameters [17,18,19]. Contact problems for elastic plates with thin elastic structures were analyzed in [20,21]. We can also mention a number of applied studies related to thin inclusions of different nature in elastic bodies [22,23,24,25,26,27,28,29]. An application of the finite element method for planar mechanical elastic systems can be found in [30]. As for inverse problems in elasticity, the literature in this field is very vast. We will only mention the articles [31,32] and the links in them.
The structure of the paper is as follows. Section 2 addresses variational and differential formulations of the equilibrium problem. Passages to limits, as a rigidity parameter of the bridge tends to infinity and to zero, are investigated in Section 3 and Section 4. We provide a justification of the limit procedure and analyze the limit models. Section 5 is concerned with the analysis of the inverse problem.

2. Setting the Problem

Let Ω 1 , Ω 2 R 2 be bounded domains with Lipschitz boundaries Γ 1 , Γ 2 , respectively, such that Ω ¯ 1 Ω ¯ 2 = . Assume that Γ i is divided into two smooth parts Γ N i and Γ D i , meas Γ D i > 0 , i = 1 , 2 . We set b = ( 2 , 2 ) × { 0 } , b 1 = ( 2 , 1 ) × { 0 } , b 2 = ( 1 , 2 ) × { 0 } , b 0 = ( 1 , 1 ) × { 0 } . Moreover, we assume that b i Ω i , and b crosses Γ N i , b 0 Ω i = , i = 1 , 2 , see Figure 1. Denote by ν = ( 0 , 1 ) , n = ( n 1 , n 2 ) unit normal vectors to b , Γ i , respectively, and set Ω = Ω 1 Ω 2 ,   Ω b = Ω \ b ¯ .
The set Ω corresponds to two elastic plates, and b fits to a thin elastic crossing bridge between two plates. We describe b in the frame of the Euler–Bernoulli beam model. In what follows, the crossing bridge b will be characterized by a rigidity parameter α > 0 . At the first step, this parameter is fixed being equal to 1, and in the sequel we analyze passages to the limit as α goes to infinity and to zero.
Let w be a scalar-valued function. We use the notations w n = w n , w ν = w ν . If M = { M i j } , i , j = 1 , 2 , then M = M i j , i j . We also put w = { w , i j } , i , j = 1 , 2 . Summation convention over repeated indices is used; all functions with two lower indices are assumed to be symmetric in those indices.
In the domains Ω 1 , Ω 2 , elasticity tensors A = { a i j k l } , B = { b i j k l } , i , j , k , l = 1 , 2 , are considered with the usual properties of symmetry and positive definiteness,
a i j k l L ( Ω 1 ) , A ξ · ξ c 0 | ξ | 2 ξ = { ξ i j } , ξ j i = ξ i j , c 0 = c o n s t > 0 .
Similar properties are fulfilled for the tensor B on Ω 2 .
We introduce notations for a bending moment M n and a transverse force T n = T n ( M ) on the boundaries of the plates,
M n = M i j n j n i ; T n = M i j , j n i M i j , k τ k τ j n i , ( τ 1 , τ 2 ) = ( n 2 , n 1 ) .
In this case, for smooth functions w , M = { M i j } , i , j = 1 , 2 , the following Green’s formula holds, see [2], Section 1.2.3,
Ω i M · w = Ω i w M + Γ i M n w n Γ i T n w , i = 1 , 2 .
Since the domain Ω b with the cut b 1 b 2 is a union of the domains Ω 1 \ b 1 and Ω 2 \ b 2 , the above Green’s formula allows us to write Green’s formula for Ω b ,
Ω b M · w = Ω b w M b 1 b 2 [ M ν ] w ν + b 1 b 2 [ T ν ] w + Γ 1 Γ 2 M n w n Γ 1 Γ 2 T n w ,
where [ h ] = h + h is a jump of a function h on b i ;   h ± are the traces of h on the crack faces b i ± , i = 1 , 2 . The signs ± fit to positive and negative directions of ν ; the values M ν , T ν with the normal vector ν are defined on b similar to (2).
In view of the above notations, an equilibrium problem for the plates Ω 1 , Ω 2 and the crossing bridge b is formulated as follows. Given external forces f L 2 ( Ω ) , g L 2 ( b ) acting on the plates and the crossing bridge, respectively, we have to find a displacement of the plates w ; a moment tensor M = { M i j } , i , j = 1 , 2 , defined in Ω , Ω b , respectively; and a crossing bridge displacement v defined on b such that
M + f = 0 in Ω b ,
M + E w = 0 in Ω b ,
v , 1111 = g on b 0 ; v , 1111 = [ T ν ] + g on b 1 b 2 ,
w = w n = 0 on Γ D 1 Γ D 2 ; M n = T n = 0 on Γ N 1 Γ N 2 ,
w ( ± 2 , 0 ) = 0 ; v = v , 11 = 0 as x 1 = 2 , 2 ,
v w 0 , [ T ν ] 0 , ( v w ) [ T ν ] = 0 on b 1 b 2 ,
[ w ] = [ w ν ] = 0 , [ M ν ] = 0 on b 1 b 2 ,
[ v ( ± 1 ) ] = [ v , 1 ( ± 1 ) ] = 0 , [ v , 11 ( ± 1 ) ] = [ v , 111 ( ± 1 ) ] = 0 .
Here, [ h ( a ) ] = h ( a + 0 ) h ( a 0 ) ; w , 1 = w x 1 , ( x 1 , x 2 ) Ω . The tensor E is equal to A , B in Ω 1 , Ω 2 , respectively. Functions defined on b we identify with functions of the variable x 1 .
Relations (4) and (5) are the equilibrium equations for the Kirchhoff–Love elastic plates Ω 1 , Ω 2 and the constitutive law; (6) is the Euler–Bernoulli equilibrium equations for the crossing bridge parts b i , see [1,2]. The right-hand side [ T ν ] in (6) describes forces acting on b 1 b 2 from the elastic plates. The first inequality in (9) provides a non-penetration between the plates and the bridge. Relation (11) provides glue conditions at the points where the bridge b crosses the external boundaries of the elastic plates. Note that, by (9), the contact set between the plates and the bridge is unknown.
We can provide a variational formulation of the problem (4)–(11). Introduce the space
W = H 2 , 0 ( b ) × H D 2 , 0 ( Ω )
with the norm
( v , w ) W 2 = v H 2 , 0 ( b ) 2 + w H D 2 , 0 ( Ω ) 2 ,
where H 2 , 0 ( b ) , H D 2 , 0 ( Ω ) are the usual Sobolev spaces,
H D 2 , 0 ( Ω ) = { w H 2 ( Ω ) | w = w n = 0 on Γ D 1 Γ D 2 ; w ( ± 2 , 0 ) = 0 } , H 2 , 0 ( b ) = { v H 2 ( b ) | v ( ± 2 ) = 0 } ,
and consider the energy functional Π : W R ,
Π ( v , w ) = 1 2 C ( w , w ) Ω f w + 1 2 b v , 11 2 b g v .
Here,
C ( w , w ¯ ) = Ω 1 a i j k l w , k l w ¯ , i j + Ω 2 b i j k l w , k l w ¯ , i j .
Denote by S the set of admissible displacements,
S = { ( v , w ) W | v w 0 on b 1 b 2 }
and consider the problem:
Find ( v , w ) S such that Π ( v , w ) = inf S Π .
This minimization problem has a unique solution since the functional Π is weakly lower semicontinuous and coercive. The coercivity of the functional Π follows from the Dirichlet boundary conditions on the sets Γ D i for the function w and conditions v ( ± 2 ) = 0 . The set S is weakly closed. The solution of the problem satisfies the following variational inequality
( v , w ) S ,
C ( w , w ¯ w ) Ω f ( w ¯ w ) + b v , 11 ( v ¯ , 11 v , 11 ) b g ( v ¯ v ) 0 ( v ¯ , w ¯ ) S .
Theorem 1. 
Problem formulations (4)–(13) are equivalent for smooth solutions.
Proof. 
Assume that (12) and (13) hold. We can substitute in (13) test functions of the form ( v ¯ , w ¯ ) = ( v , w ) ± ( 0 , φ ) , φ C 0 ( Ω b ) . This provides the equilibrium Equation (4) fulfilled in the distributional sense. Next, test functions of the form ( v ¯ , w ¯ ) = ( v , w + φ ) can be substituted in (13), where φ C 0 ( Ω ) , φ 0 on b 1 b 2 ; φ ( ± 2 , 0 ) = 0 . Taking into account the equilibrium Equation (4) and Green Formula (3), we obtain
b 1 b 2 [ M ν ] φ ν + b 1 b 2 [ T ν ] φ 0 .
From here, it follows
[ M ν ] = 0 , [ T ν ] 0 on b 1 b 2 .
Now, test functions of the form ( v ¯ , w ¯ ) = ( v + ψ , w + φ ) are substituted in (13), ( ψ , φ ) S , supp ψ ( b 1 b 2 ) . This gives
C ( w , φ ) Ω f φ + b v , 11 ψ , 11 b g ψ 0 .
Consequently, by using the Green Formula (3), in view of (4), (14), we derive
b 1 b 2 [ T ν ] φ + b v , 1111 ψ b g ψ 0 .
Choosing the above inequality ψ = φ on b 1 b 2 , the following equation
v , 1111 = [ T ν ] + g on b 1 b 2
is derived. To proceed, take test functions of the form ( v ¯ , w ¯ ) = ( v ± ψ , w ) in (3), supp ψ b 0 . The following relation is obtained:
b 0 v , 11 ψ , 11 b 0 g ψ = 0 .
Thus,
v , 1111 = g on b 0 .
Now, we are aiming to derive the last relation of (9). Assume that the inequality v ( x 0 ) w ( x 0 ) > 0 holds at a point x 0 b 1 b 2 . In this case, we can take ( v ¯ , w ¯ ) = ( v , w ) ± ε ( ψ , φ ) as a test function in (13), where the support of ψ belongs to a small neighborhood of x 0 ; the support of φ belongs to a small neighborhood of the point ( x 0 , 0 ) , and ε is small. This implies
C ( w , φ ) Ω f φ + b v , 11 ψ , 11 b g ψ = 0 .
By (3), (4), and (14), we obtain the relation
b 1 b 2 [ T ν ] φ + b v , 1111 ψ b g ψ = 0 .
In particular, this provides
[ T ν ] = 0 in   a   neighborhood   of   the   point x 0 .
This means that
( v w ) [ T ν ] = 0 on b 1 b 2 .
The next step of our reasoning is to derive boundary conditions for v at the points ± 1 , ± 2 and the last condition of (7). To this end, we take test function in (13) of the form ( v ¯ , w ¯ ) = ( v , w ) ± ( ψ , φ ) , ( ψ , φ ) W , φ = ψ on b 1 b 2 . It provides the equality
C ( w , φ ) Ω f φ + b 0 v , 11 ψ , 11 + b 1 b 2 v , 11 ψ , 11 b g ψ = 0 .
Applying the Green Formula (3), this relation implies
Ω b M · φ Ω b f φ + b 0 v , 1111 ψ + b 1 b 2 v , 1111 ψ b 1 b 2 [ M ν ] φ ν + b 1 b 2 [ T ν ] φ + Γ 1 Γ 2 M n φ n Γ 1 Γ 2 T n φ b 0 g ψ b 1 b 2 g ψ v , 111 ψ | x 1 = 1 x 1 = 1 + v , 11 ψ , 1 | x 1 = 1 x 1 = 1 v , 111 ψ | x 1 = 1 + v , 11 ψ , 1 | x 1 = 2 x 1 = 1 v , 111 ψ | x 1 = 1 + v , 11 ψ , 1 | x 1 = 1 x 1 = 2 = 0 .
From here, it follows that
M n = T n = 0 o n Γ N 1 Γ N 2 .
Taking into account (4), (14)–(16), from (17) we obtain
v , 11 ψ , 1 ( 2 ) + v , 11 ψ , 1 ( 2 ) [ v , 11 ( 1 ) ] ψ , 1 ( 1 ) + [ v , 111 ( 1 ) ] ψ ( 1 ) [ v , 11 ( 1 ) ] ψ , 1 ( 1 ) + [ v , 111 ( 1 ) ] ψ ( 1 ) = 0 .
Consequently,
v , 11 ( ± 2 ) = 0 , [ v , 11 ( ± 1 ) ] = [ v , 111 ( ± 1 ) ] = 0 .
Hence, we derived all relations (4)–(11) from (12) and (13).
Let us prove the converse. Assume that (4)–(11) are fulfilled. Then, we have for all ( v ¯ , w ¯ ) S ,
Ω b ( M + f ) ( w ¯ w ) + b 0 ( v , 1111 g ) ( v ¯ v ) + b 1 b 2 ( v , 1111 + [ T ν ] g ) ( v ¯ v ) = 0 .
Integrating by parts in the second and the third integrals of (20) and using the Formula (3), it follows that
Ω b M ( w ¯ w ) Ω b f ( w ¯ w ) + b 0 v , 11 ( v ¯ , 11 v , 11 ) b g ( v ¯ v ) + b 1 b 2 v , 11 ( v ¯ , 11 v , 11 ) + b 1 b 2 [ M ν ] ( w ¯ ν w ν ) b 1 b 2 [ T ν ] ( w ¯ w ) Γ 1 Γ 2 M n ( w ¯ n w n ) + Γ 1 Γ 2 T n ( w ¯ w ) + b 1 b 2 [ T ν ] ( v ¯ v ) + v , 111 ( v ¯ v ) | x 1 = 1 x 1 = 1 v , 11 ( v ¯ , 1 v , 1 ) | x 1 = 1 x 1 = 1 + v , 111 ( v ¯ v ) | x 1 = 2 x 1 = 1 v , 11 ( v ¯ , 1 v , 1 ) | x 1 = 2 x 1 = 1 + v , 111 ( v ¯ v ) | x 1 = 1 x 1 = 2 v , 11 ( v ¯ , 1 v , 1 ) | x 1 = 1 x 1 = 2 = 0 .
We can change the integration over Ω b by integration over Ω in the first two integrals of (21) and use boundary conditions for w , w ¯ , M n , T n . To derive the variational inequality (12) and (13) from (21), it suffices to check that
b 1 b 2 [ T ν ] ( w ¯ w ) + b 1 b 2 [ T ν ] ( v ¯ v ) + v , 111 ( v ¯ v ) | x 1 = 1 x 1 = 1 v , 11 ( v ¯ , 1 v , 1 ) | x 1 = 1 x 1 = 1 + v , 111 ( v ¯ v ) | x 1 = 1 v , 11 ( v ¯ , 1 v , 1 ) | x 1 = 1 + v , 111 ( v ¯ v ) | x 1 = 1 v , 11 ( v ¯ , 1 v , 1 ) | x 1 = 1 0 .
However, the inequality (22) easily follows from (6)–(11). Hence, we proved that (4)–(11) imply (12) and (13). Theorem 1 is proved. □

3. Convergence of Rigidity Parameter α to Infinity

In this section, we introduce a positive bridge rigidity parameter α into the model (12) and (13) and analyze a passage to the limit as α . Our aim is to justify this passage to the limit and investigate the limit model. Instead of (12) and (13), for any α > 0 , consider the following problem
( v α , w α ) S ,
C ( w α , w ¯ w α ) Ω f ( w ¯ w α ) + α b v , 11 α ( v ¯ , 11 v , 11 α ) b g ( v ¯ v α ) 0 ( v ¯ , w ¯ ) S .
The solution ( v α , w α ) of this problem is supplied with the index α . Note that we can write an equivalent differential formulation of the problem (23) and (24) similar to (4)–(11). In this case, instead of (6) we have the following equations for the crossing bridge
α v , 1111 α = g on b 0 ; α v , 1111 α = [ T ν ] + g on b 1 b 2 .
In what follows, we justify a passage to the limit as α in (23) and (24). At the first step, a priori estimates of the solutions are derived.
From (23) and (24), the following relation is obtained:
C ( w α , w α ) Ω f w α + α b ( v , 11 α ) 2 b g v α = 0 .
From (25), we derive the estimate being uniform in α α 0 > 0 ,
( v α , w α ) W c ,
moreover, the relation (25) implies
b ( v , 11 α ) 2 c α .
By estimates (26) and (27), we can assume that as α
( v α , w α ) ( v , w ) weakly in W ,
v ( x 1 ) = a 0 + a 1 x 1 , x 1 ( 2 , 2 ) ; a 0 , a 1 R .
On the other hand, since v H 2 , 0 ( b ) , consequently, v = 0 on b.
Then introduce the set of admissible displacements for the limit problem,
S = { w H D 2 , 0 ( Ω ) | w 0 on b 1 b 2 } .
We take any element w ˜ S . Then, ( 0 , w ˜ ) S . Substitute this function in (24). By (28) and (29), it is possible to pass to the limit in (23) and (24) as α . The limit relations are of the form
w S ,
C ( w , w ˜ w ) Ω f ( w ˜ w ) 0 w ˜ S .
Thus, we have shown the following result.
Theorem 2. 
As α , the solutions of the problem (23) and (24) converge in the sense (28) and (29) to the solution of (30) and (31).
To conclude this section, we provide a differential formulation of the problem (30) and (31): find functions w ,   M = { M i j } , i , j = 1 , 2 , defined in Ω , Ω b , respectively, such that
M + f = 0 in Ω b ,
M + E w = 0 in Ω b ,
w = w n = 0 on Γ D 1 Γ D 2 ; M n = T n = 0 on Γ N 1 Γ N 2 ,
w 0 , [ T ν ] 0 , w [ T ν ] = 0 on b 1 b 2 ,
[ w ] = [ w ν ] = 0 , [ M ν ] = 0 on b 1 b 2 ; w ( ± 2 , 0 ) = 0 .
The following statement takes place providing a connection between problems (30)–(36).
Theorem 3. 
Problem formulations (30)–(36) are equivalent provided that the solutions are smooth.
Proof. 
Let (32)–(36) be fulfilled. Then, we have
Ω b ( M + f ) ( w ¯ w ) = 0 , w ¯ S .
From this relation, by (3), it follows that
Ω M ( w ¯ w ) + b 1 b 2 [ T ν ] ( w ¯ w ) + Ω f ( w ¯ w ) = 0 .
In so doing, we changed the integration domain Ω b by Ω since [ M ν ] = 0 , [ w ] = [ w ν ] = 0 on b 1 b 2 . Thus, to obtain (30) and (31) from (37) it suffices to check that
b 1 b 2 [ T ν ] ( w ¯ w ) 0 .
However, the inequality (38) easily follows from (35).
Conversely, assume that (30) and (31) hold. We take a test function of the form w ˜ = w + φ , φ C 0 ( Ω b ) and substitute it in (31). This implies the equilibrium Equation (32). The other arguments are reminiscent of those used in the proof of Theorem 1, and we omit them. Theorem 3 is proved. □

4. Convergence of Rigidity Parameter of b 0 to Zero

In this section, we assume that g = 0 on b 0 . A convergence to zero of the rigidity parameter α will be analyzed when assuming that a change of this parameter happens at b 0 . In this case, the rigidity parameter at b 1 , b 2 is fixed and is equal to 1.
We first provide a formulation of the equilibrium problem such as (4)–(11) for this case: find functions w α , M = { M i j } , i , j = 1 , 2 , defined in Ω , Ω b , respectively, and functions v α defined on b such that
M + f = 0 in Ω b ,
M + E w α = 0 in Ω b ,
α v , 1111 α = 0 on b 0 ; v , 1111 α = [ T ν ] + g on b 1 b 2 ,
w α = w n α = 0 on Γ D 1 Γ D 2 ; M n = T n = 0 on Γ N 1 Γ N 2 ,
v α = v , 11 α = 0 as x 1 = 2 , 2 ; w ( ± 2 , 0 ) = 0 ,
[ w α ] = [ w ν α ] = 0 , [ M ν ] = 0 on b 1 b 2 ,
v α w α 0 , [ T ν ] 0 , ( v α w α ) [ T ν ] = 0 on b 1 b 2 ,
[ v α ( ± 1 ) ] = [ v , 1 α ( ± 1 ) ] = 0 , v , 11 α ( ± 1 ± 0 ) = α v , 11 α ( ± 1 0 ) ,
v , 111 α ( ± 1 ± 0 ) = α v , 111 α ( ± 1 0 ) .
In relations (46) and (47), we should simultaneously take upper or lower signs.
The problem (39)–(47) can be formulated in a variational form. Indeed, consider the energy functional π α : W R ,
π α ( v , w ) = 1 2 C ( w , w ) Ω f w + α 2 b 0 v , 11 2 + 1 2 b 1 b 2 v , 11 2 b 1 b 2 g v .
Then, the problem
find ( v α , w α ) S such that π α ( v α , w α ) = inf S π α
has a solution satisfying the variational inequality
( v α , w α ) S , C ( w α , w ¯ w α ) Ω f ( w ¯ w α )
+ α b 0 v , 11 α ( v ¯ , 11 v , 11 α ) + b 1 b 2 v , 11 α ( v ¯ , 11 v , 11 α ) b 1 b 2 g ( v ¯ v α ) 0 ( v ¯ , w ¯ ) S .
In what follows, we aim to justify a passage to the limit in (48) and (49) as α 0 . From (48) and (49), the following relation is obtained:
C ( w α , w α ) Ω f w α + α b 0 ( v , 11 α ) 2 + b 1 b 2 ( v , 11 α ) 2 b 1 b 2 g v α = 0 .
This relation provides the following estimate being uniform in α
v α H 2 ( b 1 b 2 ) 2 + w α H D 2 , 0 ( Ω ) 2 c ,
moreover, the relation (50) implies
α b 0 ( v , 11 α ) 2 c .
By estimates (51) and (52), we can assume that, as α 0 ,
v α v weakly in H 2 ( b 1 b 2 ) , w α w weakly in H D 2 , 0 ( Ω ) .
From (51) it follows that uniformly in α ,
v α ( ± 1 ± 0 ) , v , 1 α ( ± 1 ± 0 ) are bounded .
Here, and in (55) below, we should take upper or below signs simultaneously. Taking into account the conditions
[ v α ] = [ v , 1 α ] = 0 as x 1 = ± 1
we obtain for small α that
α v α ( ± 1 0 ) , α v , 1 α ( ± 1 0 ) are bounded .
Consequently, relations (52), (55) imply for small α that
α v α are bounded in H 2 ( b 0 ) .
Thus, we can assume that as α 0 ,
α v α v ˜ weakly in H 2 ( b 0 ) .
Now, introduce the set of admissible displacements for the limit problem
S 0 = { ( v , w ) H 2 ( b 1 b 2 ) × H D 2 , 0 ( Ω ) | v w 0 on b 1 b 2 ; v ( ± 2 ) = 0 } .
Take ( v ¯ , w ¯ ) S 0 and extend the function v ¯ to b 0 assuming that the extension belongs to the space H 2 , 0 ( b ) . In this case ( v ¯ , w ¯ ) S , and we can substitute ( v ¯ , w ¯ ) in (48) and (49) as a test function. Passing to the limit as α 0 , by (53), (56), the following variational inequality is obtained:
( v , w ) S 0 ,
C ( w , w ¯ w ) Ω f ( w ¯ w ) + b 1 b 2 v , 11 ( v ¯ , 11 v , 11 ) b 1 b 2 g ( v ¯ v ) 0 ( v ¯ , w ¯ ) S 0 .
Thus, the following statement is proved.
Theorem 4. 
As α 0 , the solutions of the problem (48) and (49) converge in the sense (53) to the solution of (57) and (58).
To conclude the section, we provide a differential formulation of the problem (57) and (58): find a displacement of the elastic plates w , a moment tensor M = { M i j } , i , j = 1 , 2 , defined in Ω , Ω b , respectively, and a function v defined on b 1 b 2 such that
M + f = 0 in Ω b ,
M + E w = 0 in Ω b ,
v , 1111 = [ T ν ] + g on b 1 b 2 ,
w = w n = 0 on Γ D 1 Γ D 2 ; M n = T n = 0 on Γ N 1 Γ N 2 ,
w ( ± 2 , 0 ) = 0 ; v = v , 11 = 0 as x 1 = 2 , 2 ,
v w 0 , [ T ν ] 0 , ( v w ) [ T ν ] = 0 on b 1 b 2 ,
= [ w ν ] = 0 , [ M ν ] = 0 on b 1 b 2 ,
v , 11 ( ± 1 ) = v , 111 ( ± 1 ) = 0 .
The following statement is valid.
Theorem 5. 
Problem formulations (57)–(59) and (66) are equivalent provided that the solutions are smooth.
We omit the proof of this theorem since it is reminiscent of that of Theorem 1. The only step we have to take is to provide a proof that from (57) and (58) the boundary conditions (66) follow. Indeed, take in (57) and (58) test functions of the form ( v ¯ , w ¯ ) = ( v , w ) ± ( v ˜ , w ˜ ) , ( v ˜ , w ˜ ) S 0 , v ˜ = w ˜ on b 1 b 2 . This gives
C ( w , w ˜ ) Ω f w ˜ + b 1 b 2 v , 11 v ˜ , 11 b 1 b 2 g v ˜ = 0 .
Since
C ( w , w ¯ ) = Ω M i j ( w ) w ¯ , i j ,
we can integrate by parts in the third term of (67) and use Green’s Formula (3). This implies
Ω b M · w ˜ Ω b f w ˜ + b 1 b 2 v , 1111 v ˜ b 1 b 2 [ M ν ] w ˜ ν + b 1 b 2 [ T ν ] w ˜ + Γ 1 Γ 2 M n w ˜ n Γ 1 Γ 2 T n w ˜ b 1 b 2 g v ˜ v , 111 v ˜ | x 1 = 1 + v , 11 v ˜ , 1 | x 1 = 1 v , 111 v ˜ | x 1 = 1 + v , 11 v ˜ , 1 | x 1 = 1 = 0 .
Since the equilibrium equations (59), (61) hold, and since [ M ν ] = 0 on b 1 b 2 , the relation (68) implies boundary conditions (66) and the second group of boundary conditions (62).
Theorem 5 is proved.
To conclude this section, we note that the problems (59) and (66) describe an equilibrium state for two plates occupying the domains Ω 1 , Ω 2 . In fact, we have two independent problems (for each plate) since there is no connection between the plates.

5. Analysis of Inverse Problem

In this section, we analyze an inverse problem related to the equilibrium problem (12) and (13). Elasticity tensors A , B are assumed to be constant. The inverse problem consists in finding displacement fields of the plates and the bridge together with an elasticity tensor A when assuming that additional data are provided by measurement. More precisely, it is assumed that for a given continuous function ξ , a value ξ ( w ( x 0 ) ) is known, where w ( x 0 ) is the displacement of the plate at a given point x 0 Ω 2 , x 0 ( 2 , 0 ) . In particular, we can assume that ξ ( w ( x 0 ) ) = w ( x 0 ) . Note that from a practical standpoint, it is no problem to provide measurements for finding a displacement w ( x 0 ) of the point x 0 ; consequently, ξ ( w ( x 0 ) ) . We first introduce the 6D space with the Euclidean metric,
R s y m = { A = { a i j k l } | a i j k l = a j i k l = a k l i j , i , j , k , l = 1 , 2 ; a i j k l R } .
Let G R s y m be a bounded domain with a smooth boundary whose elements satisfy the inequality (1). Then, for any A G ¯ and the fixed tensor B it is possible to find a solution of the variational inequality
( v A , w A ) S ,
C A ( w A , w ¯ w A ) Ω f ( w ¯ w A ) + b v , 11 A ( v ¯ , 11 v , 11 A ) b g ( v ¯ v A ) 0 ( v ¯ , w ¯ ) S ,
where C A = C with the given tensor A .
Now, we assume that the elasticity tensor A is unknown in the problems (69) and (70). On the other hand, the plate displacement of the point x 0 is known. Namely, w ( x 0 ) is known from a measurement. Then, the precise formulation of the inverse problem is as follows. Let d R be given. We have to find ( v A , w A ) , A G ¯ such that
( v A , w A ) S ,
C A ( w A , w ¯ w A ) Ω f ( w ¯ w A ) + b v , 11 A ( v ¯ , 11 v , 11 A ) b g ( v ¯ v A ) 0 ( v ¯ , w ¯ ) S ,
ξ ( w A ( x 0 ) ) = d .
Below, we prove the existence of a solution of the inverse problem (71)–(73).
Theorem 6. 
d 1 , d 2 R , d 1 d 2 , exist such that for any fixed d [ d 1 , d 2 ] , the inverse problem (71)–(73) has a solution.
Proof. 
We introduce a function L defined on the closed set G ¯ ,
L : G ¯ R , L ( A ) = ξ ( w A ( x 0 ) ) ,
where ( v A , w A ) is the solution of the direct problem (69) and (70) with the given elasticity tensor A. In what follows, we prove that this function is continuous on the set G ¯ . Indeed, let A p G ¯ ,
A p A , A G ¯ , p ,
where we use the convergence in the Euclidean norm | · | . For any p , we can find the unique solution of the problem
( v p , w p ) S ,
C p ( w p , w ¯ w p ) Ω f ( w ¯ w p ) + b v , 11 p ( v ¯ , 11 v , 11 p ) b g ( v ¯ v p ) 0 ( v ¯ , w ¯ ) S ,
where C p fits the elasticity tensor A p . The variational inequality (76) and (77) implies
C p ( w p , w p ) Ω f w p + b ( v , 11 p ) 2 b g v p = 0 .
From (78), by the uniformity of this estimate in p, it follows that
( v p , w p ) W c .
Choosing a subsequence, if necessary, we can assume that as p ,
( v p , w p ) ( v , w ) weakly   in W .
By (75), (80), a passage to the limit in (76) and (77), as p , is possible, and the limit relation reads as follows:
( v , w ) S ,
C A ( w , w ¯ w ) Ω f ( w ¯ w ) + b v , 11 ( v ¯ , 11 v , 11 ) b g ( v ¯ v ) 0 ( v ¯ , w ¯ ) S .
Consequently, we have ( v , w ) = ( v A , w A ) ,
( v A , w A ) S ,
C A ( w A , w ¯ w A ) Ω f ( w ¯ w A ) + b v , 11 A ( v ¯ , 11 v , 11 A ) b g ( v ¯ v A ) 0 ( v ¯ , w ¯ ) S .
Moreover, by (80), we can assume that w p ( x 0 ) w A ( x 0 ) as p ; consequently,
ξ ( w p ( x 0 ) ) ξ ( w A ( x 0 ) ) .
We proved, therefore, that the function L is continuous on the compact set G ¯ . By the Weierstrass extreme value theorem, this means that we can find
d 1 = min A G ¯ L ( A ) , d 2 = max A G ¯ L ( A ) .
Taking into account the intermediate value theorem for continuous functions, we conclude that for any d [ d 1 , d 2 ] A G ¯ exists such that
L ( A ) = d .
This implies that the inverse problems (71) and (73) have a solution. Theorem 6 is proved. □
Note that similar arguments can be used for proving a solution existence to an inverse boundary problem with a different additional information compared to (73). In particular, instead of (73), we can consider
ξ ( v A ( y 0 ) ) = d ,
where y 0 ( 1 , 2 ) is a given point, and v A is the displacement of the bridge.

6. Conclusions

The paper presents a rigorous mathematical analysis of the elastic structure consisting of two Kirchhoff–Love plates and the crossing 1D bridge. An inequality-type restriction is imposed on the solution, which provides a mutual non-penetration between the plates and the bridge. This restriction implies that the boundary-value problem as a whole refers to the problem with unknown set of a contact. The solution existence of the problem is established, and asymptotic analysis is fulfilled with respect to the rigidity parameter of the bridge as this parameter tends to infinity and to zero. Therefore, in the frame of the high-level mathematical model, we provide a correctness of the boundary-value problem and analyze the limit mathematical models. Moreover, the existence of a solution to the inverse problem is proved, which allows us to find both the displacement field and the elasticity tensor of one plate provided that a displacement of the other plate at a given point is known.

Funding

This work was supported by Mathematical Center in Akademgorodok under agreement No. 075-15-2019-1613 with the Ministry of Science and Higher Education of the Russian Federation.

Data Availability Statement

Not applicable.

Conflicts of Interest

The authors declare no conflict of interest.

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Figure 1. Elastic plates Ω 1 , Ω 2 with crossing bridge b.
Figure 1. Elastic plates Ω 1 , Ω 2 with crossing bridge b.
Axioms 12 00120 g001
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Khludnev, A. On the Crossing Bridge between Two Kirchhoff–Love Plates. Axioms 2023, 12, 120. https://doi.org/10.3390/axioms12020120

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