Abstract
We study a class of non-clamped dynamical problems for visco-elastic materials, the contact condition is modeled by a normal compliance, with friction, damage and heat exchange. The weak formulation leads to a general system defined by a second-order quasi-variational evolution inequality on the displacement field coupled with a nonlinear evolutional inequality on temperature field and a parabolic variational inequality on the damage field. We present and establish an existence and uniqueness result of different fields, by using general results on evolution variational inequalities, with monotone operators and fixed point methods. Then, we present a fully discrete numerical scheme of approximation and derive an error estimate. Finally, various numerical computations are developed.
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1 Introduction
Problems involving contact between deformable bodies abound in industry and everyday life. For this reason, a considerable engineering and mathematical literature is devoted to dynamic and quasi-static frictional contact problems, including mathematical modeling, mathematical analysis, numerical analysis and numerical simulations. The study of contact problems for elastic–visco-elastic materials within the mathematical analysis framework was introduced in the early reference works [5, 8,9,10]. In these works, numerous types of frictional contact models with nonlinear visco-elastic or elasto-plastic materials were widely studied, in the framework of linearized infinitesimal deformations, using abstract variational inequalities, with monotonicity and convexity.
Further extensions to non-convex contact conditions with non-monotone and possible multi-valued constitutive laws led to the active domain of non-smooth mechanic within the framework of the so-called hemivariational inequalities, for a mathematical as well as mechanical treatment, we refer to [11].
This paper is a continuation work of the results obtained in [3], p. 251. In [3], the authors studied a problem for the quasi-static contact between an elastic–visco-plastic body and an obstacle, the contact was clamped on some part of the boundary and was frictionless, and it was defined by a normal compliance condition with damage. An existence and uniqueness result on displacement and damage fields has been established, and also some numerical approximations and simulations have been presented.
In this work, we study a class of dynamic contact problems with normal compliance condition and damage, with Coulomb’s friction and thermal effects, for visco-elastic material. The novelty here is that we investigate a general long memory material law, depending on time, on the temperature and the damage. Moreover, the evolution of the temperature is described by a general nonlinear equation, involving the gradient of temperature and the velocity of deformation, and the associated boundary condition is defined by an inclusion of sub-differential type in a non-convex framework. Also, the usual clamped condition has been deleted, so that Korn’s inequality cannot be applied any more. The problem appears then semi-coercive and strongly nonlinear due to the frictions. Semi-coercive problems were first studied in [5] for Coulomb’s friction models, where the inertial term of the dynamic process has been used in order to compensate the loss of coerciveness in the a priori estimates. The variational formulation of the mechanical problem leads to a new non-standard model of system defined by a second-order quasi-variational inequality on the displacement field, coupled with one nonlinear inequality for the temperature field and with a variational inequality on the damage field. Then, by using classical results on evolution variational inequalities, with monotone operators and adopting fixed point methods frequently used in [2], we prove an existence and uniqueness of solution on the displacement, damage, and temperature fields.
The paper is organized as follows. In Section 2, we describe the mechanical problem and specify the assumptions on the data to derive the variational formulation, and then we state our main existence and uniqueness result. In Section 3, we give the proof of the claimed result. In Section 4, we introduce a fully discrete approximation scheme and derive an order error estimate under solution regularity assumptions. In Section 5, we present some numerical simulations in order to show the evolution of deformation, of the Von Mise’s norm, of the temperature and the damage in the body.
2 The Contact Problem
In this section, we study a class of thermal contact problems with non-clamped frictional normal compliance condition, for visco-elastic materials. We describe the mechanical problems, list the assumptions on the data, and derive the corresponding variational formulations. Then, we state an existence and uniqueness result on displacement and temperature fields, which we will prove in the next section.
The physical setting is as follows. A visco-elastic body occupies a bounded domain \(\varOmega \subset \mathbb {R}^d \) (d = 2, 3) with a Lipschitz boundary Γ that is partitioned into two disjoint measurable parts, Γ F and Γ c. Let [0, T] be the time interval of interest, where T > 0. We assume that a volume force of density f 0 acts in Ω × (0, T) and that surface tractions of density f F apply on Γ F × (0, T). The body may come in contact with an obstacle, the foundation, over the potential contact surface Γ C. The model of the contact is specified by a general sub-differential boundary condition, where thermal effects may occur in the frictional contact with the foundation. Our aim is to describe the dynamic evolution of the body.
Let us recall now some classical notations, see e.g. [5] for further details. We denote by S d the space of second-order symmetric tensors on \( \mathbb {R}^{d}\), while “⋅” and |⋅| will represent the inner product and the Euclidean norm on S d and \(\mathbb {R}^d\). Let ν denote the unit outer normal on Γ. Everywhere in the sequel, the indices i and j run from 1 to d, summation over repeated indices is implied, and the index that follows a comma represents the partial derivative with respect to the corresponding component of the independent variable. We also use the following notation:
Here, \( \boldsymbol {\varepsilon } : H_{1} \longrightarrow \mathcal {H}\) and \(\mathrm {Div}\, : \mathcal {H}_{1} \longrightarrow H \) are the deformation and the divergence operators, respectively, defined by
The spaces H, \(\mathcal {H}\), H 1, and \(\mathcal {H}_{1}\) are real Hilbert spaces endowed with the canonical inner products given by
We recall that C denotes the class of continuous functions; C m, \(m\in \mathbb {N}^*\) the set of m times continuously differentiable functions; and W m, p, \(m\in \mathbb {N}\), 1 ≤ p ≤ +∞ the classical Sobolev spaces.
Now, we consider a visco-elastic body which occupies a bounded domain Ω ⊂R d (d = 1, 2, 3) with a Lipschitz boundary Γ that is partitioned into two disjoint measurable parts, Γ F and Γ C. Let [0, T] be the time interval of interest, where T > 0. We assume that a volume force of density f 0 acts in Ω × (0, T) and that surface tractions of density f F apply on Γ F × (0, T). The body may come in contact with an obstacle, the foundation, over the potential contact surface Γ C, see figure below.
To continue, the mechanical problem is then formulated as follows.
Problem Q: Find a displacement field \(\boldsymbol {u} :(0,T) \times \varOmega \longrightarrow \mathbb {R}^{d}\), a stress field σ : (0, T) × Ω→S d, a temperature field \(\theta :\,(0,T) \times \varOmega \longrightarrow \mathbb {R}_+\), and a damage field \(\alpha : (0,T) \times \varOmega \rightarrow \mathbb {R}\) such that for a.e. t ∈ (0, T):
Equation (1) is the Kelving Voigt’s long memory thermo-visco-elastic constitutive law of the body including the influence of the damage variable. Here, σ is the stress tensor, \(\mathcal {A}\) denotes the viscosity operator with, \( \mathcal {A}(t)\boldsymbol {\tau } = \mathcal {A}(t,\cdot ,\boldsymbol {\tau })\) is some function defined on Ω, and \(\mathcal {G}\) is the elastic operator depending on the linearized strain tensor ε(u) of infinitesimal deformations and on the damage α, with \( \mathcal {G}(t)(\boldsymbol {\tau }, \alpha ) = \mathcal {G}(t,\cdot ,\boldsymbol {\tau }, \alpha ) \) is some function defined on Ω. For example,
where \(\mathcal {G}^0(t)\boldsymbol {\tau } = \mathcal {G}^0(t,\cdot ,\boldsymbol {\tau }) \) is some time-depending elastic tensor function independent on the damage, defined on Ω, and C da(t) is some time-depending damage tensor. The term \( \mathcal {B}(t)(\boldsymbol {\tau }, \alpha ) = \mathcal {B}(t,\cdot ,\boldsymbol {\tau }, \alpha ) \) represents the relaxation tensor time depending on the linearized strain tensor and the damage, defined on Ω. And the last tensor C e(t, θ) := C e(t, ⋅, θ) denotes the thermal expansion tensor depending on time and temperature, defined on Ω. For example,
where
is some time-depending expansion tensor defined on Ω, with c ij ∈ L ∞((0, T) × Ω).
The model in (2) is the dynamic equation of motion where the mass density ϱ ≡ 1. Equation (3) is the traction boundary condition.
On the contact surface, the general relation (4) represents the normal compliance contact condition, where σ ν denotes the normal stress, u ν is the normal displacement, g is the gap between the contact surface and the foundation, and p ν is some normal compliance function defined on \( (0,T)\times \varGamma _{C} \times \mathbb {R} \) with the convention that p ν(t, r) = p ν(t, ⋅, r) denotes some function defined on Γ C, for a.e. t ∈ (0, T), for all \(r\in \mathbb {R}\). The term u ν − g represents, when it is positive, the penetration of the surface asperities into the foundation.
For example, for a.e. t ∈ (0, T),
In this formula, the normal stress is proportional to the penetration, with some positive coefficient c ν defined on (0, T) × Γ C, which is related to the hardness of the foundation.
Equation (5) represents a general version of Coulomb’s dry friction law, where σ τ is the tangential stress, p τ is the friction bound measuring the maximal frictional resistance defined on \( (0,T)\times \varGamma _{C} \times \mathbb {R} \), and \( \dot {\boldsymbol {u}}_{\tau }\) is the tangential velocity. Recall that p τ(t, r) = p τ(t, ⋅, r) is some function defined on Γ C, for a.e. t ∈ (0, T), for all \(r\in \mathbb {R}\).
For example, for a.e. t ∈ (0, T),
where the friction bound is proportional to the normal stress with some positive coefficient of friction μ τ defined on (0, T) × Γ C.
Following Frémond [6, 7], the damage function α represents the percentage of the safe part or undamaged part, α = 1 means that the body is undamaged, and α = 0 says that the body is completely damaged. The evolution of the microscopic cracks responsible for the damage is described by the parabolic differential inclusion (6) of the damage function α satisfying 0 ≤ α ≤ 1, where γ is a positive constant and ϕ d is a given constitutive function which describes damage source in the system. The inequality (6) means
and
and
Equation (8) represents the homogeneous Neumann boundary condition for the damage field, see e.g. [3], p. 241.
The differential equation (9) provides the evolution of the temperature field. There \( \mathcal {K}_c(t,\nabla \theta ) := \mathcal {K}_c(t,\cdot ,\nabla \theta )\) is some nonlinear time-depending function of the temperature gradient ∇θ, which is defined on Ω. For example, denote by
the thermal conductivity tensor defined on Ω, we could consider
In the second member, q(t) denotes the density of volume heat sources, whereas
is the deformation-viscosity heat, which is a nonlinear function defined on Ω and which represents the heat generated by the velocity of deformation (viscosity) and may depend on the temperature.
Example 1
Example 2
with some coefficient \( d_{e} \in L^\infty ((0,T)\times \varOmega . \mathbb {R}^+)\);
Example 3
By assuming the variation of θ(t) small enough, then the heat function \(D_{e}(t, \boldsymbol {\varepsilon }(\dot {\boldsymbol {u}}(t)), \theta (t) )\) may be considered as a formula which is independent of the temperature.
The associated temperature boundary condition is given by (10) and (11), where Ξ and φ are some functions defined on \( (0,T) \times \varGamma _{C} \times \mathbb {R}\). Here,
denotes the sub-differential on the third variable of φ in the locally Lipschitz framework.
We recall that for a locally Lipschitz function \( G\,:\, \mathbb {R} \longrightarrow \mathbb {R}\), at any point \(a \in \mathbb {R}\) and for any vector \(d \in \mathbb {R}\), we can define the following directional derivative with respect to d:
We have for all \(a,\, d \in \mathbb {R}\), for all ξ ∈ ∂G(a):
and
where
In the case where G is convex on \( \mathbb {R}\), we have
and
where \( G^{\prime }_r\) and \(G^{\prime }_l\) denote the right side and left side derivatives, respectively.
In the sequel, for a.e. (t, x) ∈ (0, T) × Γ c, for all \( (r,s)\in \mathbb {R}^2\), we use the notation
and
Taking the previous example for \( \mathcal {K}_c\), we have
Let us consider, for example,
where θ R is the temperature of the foundation, and k e is the heat exchange coefficient between the body and the obstacle. We obtain
Finally, the data in u 0, v 0, α 0, and θ 0 in (12) represent the initial displacement, velocity, damage, and temperature, respectively.
In view to derive the variational formulation of the mechanical problems (1)–(12), let us first precise the functional framework. Let
be the admissible displacement space, endowed with the inner product given by
and let ∥⋅∥V be the associated norm, i.e.
Therefore, (V, ∥⋅∥V) is a real Hilbert space, where the norm ∥⋅∥V is equivalent to \(\|\cdot \|{ }_{(H^{1}(\varOmega ))^d}\).
Let
be the admissible temperature space, endowed with the canonical inner product of H 1(Ω).
By the Sobolev’s trace theorem, there exists a constant c 0 > 0 depending only on Ω, and Γ C such that
Next, we denote the set of admissible damage fields by
We use here two Gelfand evolution triples (see e.g. [12], pp. 416) given by
where the inclusions are dense and continuous.
In the study of the mechanical problems (1)–(12), we assume that the viscosity operator \( {\mathcal A} \,:\, (0,T)\times \varOmega \times S_d\longrightarrow S_d\) satisfies
Here, recall that for every t ∈ (0, T) and τ ∈ S d, we write by \({\mathcal A}(t) = {\mathcal A}(t,\cdot ,\cdot )\) a functional which is defined on Ω × S d and \({\mathcal A}(t) \, \boldsymbol {\tau } = {\mathcal A}(t,\cdot ,\boldsymbol {\tau })\) some function defined on Ω.
We suppose that the elasticity operator \({\mathcal G} : (0,T)\times \varOmega \times S_d \times \mathbb {R} \longrightarrow S_d \) satisfies
We put again \({\mathcal G}(t)(\boldsymbol {\tau }, \lambda ) = {\mathcal G}(t,\cdot ,\boldsymbol {\tau }, \lambda )\) some function defined on Ω for every t ∈ (0, T), τ ∈ S d, \( \lambda \in \mathbb {R}\).
The relaxation tensor \({\mathcal B}\,:\, (0,T) \times \varOmega \times S_d \times \mathbb {R} \longrightarrow S_d\) satisfies
The body forces and surface tractions satisfy the regularity conditions:
The gap function g : (0, T) × Γ C→R + verifies
The thermal expansion tensor \(C_e \,:\, (0,T) \times \varOmega \times \mathbb {R} \longrightarrow S_d\) verifies
Here, we use the notation C e(t, 𝜗) = C e(t, ⋅, 𝜗) some function defined on Ω, for all t ∈ (0, T) and \( \vartheta \in \mathbb {R} \).
The normal compliance function \( p_\nu \,:\, (0,T) \times \varGamma _{C} \times \mathbb {R} \longrightarrow \mathbb {R}_+\) satisfies
The friction bound function \( p_\tau \,:\, (0,T) \times \varGamma _{C} \times \mathbb {R} \longrightarrow \mathbb {R}_+\) satisfies
The damage source \(\phi _d\,: \, \varOmega \times S_d \times S_d \times [0,1] \longrightarrow \mathbb {R}\) verifies
We assume that the nonlinear function \(\mathcal {K}_c : (0,T)\times \varOmega \times \mathbb {R}^d \longrightarrow \mathbb {R}^d \) satisfies
We suppose that the deformation-viscosity heat function \(D_{e} : (0,T)\times \varOmega \times S_d \times \mathbb {R} \longrightarrow \mathbb {R} \) satisfies
We notice that these conditions are verified in examples (13)–(15).
The heat sources density verifies
We suppose that the nonlinear functions \(\varXi ,\,\varphi : (0,T)\times \varGamma _{C} \times \mathbb {R} \longrightarrow \mathbb {R} \) satisfy
These assumptions are clearly satisfied in example (17).
Finally, we assume that the initial data satisfy the conditions
Using Green’s formula, we obtain the following weak formulation of the mechanical problem Q, defined by a system of second-order quasi-variational evolution inequality coupled with a first-order evolution equation.
Problem QV : Find a displacement field u : [0, T] → V , a damage field \(\alpha : [0,T] \longrightarrow \mathcal {K}_{da}\), and a temperature field θ : [0, T] → E satisfying for a.e. t ∈ (0, T):
Here, the operators and functions A(t) : V →V ′, \( B(t)\, : \, V \times \mathcal {K}_{da} \longrightarrow V'\), C(t) : E→V ′, \( j_{\nu },\, j_{\tau } \, : \, (0,T) \times V^2 \longrightarrow \mathbb {R}^+\), K(t) : E→E′, \(\psi (t,\cdot ;\cdot )\,:\,E\times E \longrightarrow \mathbb {R}\), R(t, ⋅, ⋅) : V × E→E′, f : (0, T)→V ′, and Q : (0, T)→E′ are defined by, for all v ∈ V , w ∈ V , ζ ∈ E, η ∈ E, \( \xi \in \mathcal {K}_{da}\), for a.e. t ∈ (0, T),
We notice that from (31), then the formula ψ(t, ζ;η) is well defined for all ζ ∈ E, η ∈ E, for a.e. t ∈ (0, T).
The inequality (35) is a consequence of the following equation:
where Ξ(t, r) := Ξ(t, ⋅, r) for \( (t,r)\in (0,T)\times \mathbb {R}\).
In the case when φ(t, x, ⋅) is differentiable for a.e. (t, x) ∈ (0, T) × Γ c, we have
for \( (t,\boldsymbol {x},r)\in (0,T)\times \varGamma _{C} \times \mathbb {R}\).
Then, for all ζ ∈ E and a.e. t ∈ (0, T), the linear functional
will be denoted by
The inequality (35) or Equation (37) can be written as
Our main existence and uniqueness result is the following, which we will prove in the next section.
Theorem 1
Assume that (19)–(32) hold, and under the condition that
then there exists an unique solution {u, α, θ} to problem QV with the regularity:
3 Proof of Theorem 1
The idea is to bring the second-order inequality to a first-order inequality, using monotone operator, convexity, and fixed point arguments, and will be carried out in several steps.
Let us introduce the velocity variable
The system in problem QV is then written as, for a.e. t ∈ (0, T),
with the regularities:
We begin by the following lemma.
Lemma 1
For all η ∈ W 1, 2(0, T;V ′), there exists an unique
satisfying
where
Moreover, if \( L_{\tau } < \frac {m_{\mathcal {A}}}{\sqrt {2}\, T c_0^2} \) , then ∃c > 0 such that ∀η 1, η 2 ∈ W 1, 2(0, T;V ′), ∀t ∈ [0, T]:
Proof
Given η ∈ W 1, 2(0, T;V ′) and x ∈ C(0, T;V ), by using a general result on parabolic variational inequality (see e.g. [1]), we obtain the existence of a unique v η x ∈ C(0, T;H) ∩ L 2(0, T;V ) ∩ W 1, 2(0, T;V ′) satisfying
Now, let us fix η ∈ W 1, 2(0, T;V ′) and consider Λ η : C(0, T;V ) → C(0, T;V ) defined by
We check by algebraic manipulation that for all u 1, u 2, w 1, w 2 ∈ V , a.e. t ∈ (0, T), we have
where \(c_1 = L_\tau \, c_0^2\) is involving c 0, which is defined by (18).
Let x 1, x 2 ∈ C(0, T;V ) be given. Putting in (41) the data x = x 1 with \(\boldsymbol {w} = \boldsymbol {v}_{\eta \,x_2}\) and x = x 2 with \(\boldsymbol {w} = \boldsymbol {v}_{\eta \,x_1}\), adding then the two inequalities, and integrating over (0, T), we obtain, ∀t ∈ [0, T],
Using Gronwall’s inequality (see e.g. [2]), we deduce that
Thus, by Banach’s fixed point principle, we know that Λ η has an unique fixed point denoted by x η. We then verify that
is the unique solution verifying (39).
Now, let η 1, η 2 ∈ W 1, 2(0, T;V ′). Putting in (39) the data η = η 1 with \(\boldsymbol {w} = \boldsymbol {v}_{\eta _2}\) and η = η 2 with \(\boldsymbol {w} = \boldsymbol {v}_{\eta _1}\), adding then the two inequalities and integrating over (0, T), and using the inequality
for all reals a, b, ε > 0, we obtain for all δ > 0, for all t ∈ [0, T]:
Now, verifying that
we have
We deduce (40) from Gronwall’s inequality if
i.e.
where
To conclude, we obtain (40) if ∃ς ∈ ]0, 1[ such that \( L_{\tau } < \frac {m_{\mathcal {A}}}{T c_0^2}\, \sqrt {2\varsigma (1-\varsigma )}\). This last condition is equivalent to
□
Here and below, we denote by c > 0 a generic constant, which value may change from lines to lines.
Lemma 2
For all η ∈ W 1, 2(0, T;V ′), there exists a unique
satisfying
Moreover, if \( L_{\tau } < \frac {m_{\mathcal {A}}}{\sqrt {2}\, T c_0^2} \) , then ∃c > 0 such that ∀η 1, η 2 ∈ W 1, 2(0, T;V ′):
Proof
Let us fix η ∈ W 1, 2(0, T;V ′). We verify that Q ∈ L 2(0, T;E′).
Let us consider the operator Ψ η(t) : E→E′ defined for a.e. t ∈ (0, T) by
Then, the problem is to find θ : (0, T)→E verifying
Using the assumptions (28), (29), and (31), Ψ η(t) is strongly monotone for a.e. t ∈ (0, T). Therefore, the existence and uniqueness result verifying (42) follows from classical result on first-order evolution equation (see e.g. [9], pp. 162–164).
Now, for η 1, η 2 ∈ W 1, 2(0, T;V ′), we have, for a.e. t ∈ (0;T),
Then, integrating the last property over (0, t), using the strong monotonicity of K(t) and the Lipschitz continuity of R(t, ⋅, ⋅) : V × E→E′ independently of t ∈ (0, T), we deduce
The inequality (43) follows then from Lemma 1. □
Lemma 3
For all μ ∈ L 2(0, T;L 2(Ω)), there exists an unique
satisfying
Moreover, ∃c > 0 such that ∀μ 1, μ 2 ∈ L 2(0, T;L 2(Ω)):
Proof
The inequality (44) follows from classical result on parabolic evolution variational inequalities, see e.g. [1].
Now, for any μ 1, μ 2 ∈ L 2(0, T;L 2(Ω)), putting in (44) the data μ = μ 1 with \(\xi = \alpha _{\mu _2}\), then μ = μ 2 with \(\xi = \alpha _{\mu _1}\), adding then the two inequalities, and integrating over (0, T), we obtain, ∀t ∈ [0, T],
Thus, the inequality (45) follows from Gronwall’s inequality. □
Consider X := W 1, 2(0, T;V ′) × L 2(0, T;L 2(Ω)), and the operator Λ : X → X is defined by, for all (η, μ) ∈ X,
where
and
Lemma 4
Under the condition that \( L_{\tau } < \frac {m_{\mathcal {A}}}{\sqrt {2}\, T c_0^2} \) , then Λ has a unique fixed point (η ∗, μ ∗).
Proof
First, we check that from the definition of the operator C(⋅) and from hypothesis (24), then there exists c > 0, such that for a.e. t ∈ (0, T), for all ξ 1, ξ 2 ∈ E, we have
Now, let (η 1, μ 1) and (η 2, μ 2) be given in X. We verify that, for a.e. t ∈ (0, T),
Thus,
We deduce from Lemmas 1–3 that if \(L_{\tau } < \frac {m_{\mathcal {A}}}{\sqrt {2} T c_0^2}\), then ∃c > 0 satisfying, for all (η 1, μ 1), (η 2, μ 2) in X and for all t ∈ [0, T],
Then, using again Banach’s fixed point principle, we obtain that Λ has an unique fixed point. □
Proof of Theorem 1
We have now all the ingredients to prove Theorem 1.
We verify then that the functions
are solutions to problem QV with the regularities in (38), the uniqueness follows from the uniqueness in Lemmas 1–3. □
4 Analysis of a Numerical Scheme
In this section, we study a fully discrete numerical approximation scheme of the variational problem QV . For this purpose, let {u, θ} be the unique solution of the problem QV , and introduce the velocity variable
Then,
Here, we make the following additional assumptions on the different data, operators, and solution fields:
and for all \(r, r_1, r_2 \in \mathbb {R}\), a.e. (t, x) ∈ (0, T) × Γ C:
We remark that the example of φ given in (17) satisfies hypothesis (48).
From Theorem 1, {v, θ, α} verify, for all t ∈ [0, T],
Now, let V h ⊂ V , E h ⊂ E, and \(\mathcal {K}_{da}^h\subset \mathcal {K}_{da}\) be a family of finite dimensional subspaces, with h > 0 a discretization parameter. We divide the time interval [0, T] into N equal parts: t n = n k, n = 0, 1, …, N, with the time step k = T∕N.
For a continuous operator or function U ∈ C([0, T];X) with values in a space X, we use the notation U n = U(t n) ∈ X.
Then, from (49)–(52), we introduce the following fully discrete scheme.
Problem P hk
Find \(\boldsymbol {v}^{hk}=\{\boldsymbol {v}^{hk}_n\}_{n=0}^N \subset V^h\), \(\theta ^{hk}=\{\theta ^{hk}_n\}_{n=0}^N \subset E^h\) and \(\alpha ^{hk}=\{\alpha _n^{hk}\}_{n=0}^N \subset \mathcal {K}_{da}^h\) such that
and for n = 1, ⋯ , N,
where for n = 1, ⋯ , N,
Here, \( \boldsymbol {u}^h_0 \in V^h \), \( \boldsymbol {v}^h_0 \in V^h \), \(\theta ^{h}_0 \in E^h\), \(\alpha ^h_0\in \mathcal {K}_{da}^h\), and \( \boldsymbol {\sigma }_{0}^{h} \in \mathcal {H} \) are suitable approximations of the initial values u 0, v 0, θ 0, α 0, and σ 0, respectively.
We verify that for n = 1, ⋯ , N, once \(\boldsymbol {u}_{n-1}^{hk}, \boldsymbol {v}_{n-1}^{hk}, \theta _{n-1}^{hk}, \alpha _{n-1}^{hk}, and \boldsymbol {\sigma }_{n-1}^{hk}\) are known, then we obtain \( \boldsymbol {v}_{n}^{hk} \) by (54), \( \theta _{n}^{hk} \) by (55), \( \alpha _{n}^{hk} \) by (56), \( \boldsymbol {u}_{n}^{hk} \) by (57) (using \( \boldsymbol {u}_{n}^{hk} = \boldsymbol {u}_{n-1}^{hk} + k\,\boldsymbol {v}^{hk}_n\)), and \( \boldsymbol {\sigma }_{n}^{hk} \) by (58).
We now turn to an error analysis of the numerical solution. Here, we use and extend the technique developed in [3], p. 241.
proof
We have to estimate the following numerical solution errors, respectively, for the velocity, temperature, and damage:
First step. Estimate of \(( \alpha _n - \alpha ^{hk}_n)_{ 1\le n\le N}\). Let us fix n = 1, ⋯ , N. Using (51) with t = t n, \( \xi = \alpha ^{hk}_n\) and (56) with \( \xi ^h = \xi ^{h}_n \in \mathcal {K}_{da}^h\) and then adding the two inequalities, we obtain after some algebraic manipulation, for some constant c > 0,
where ε > 0 is a small parameter which will be chosen later and
From (47), we have
and
We deduce that
where by using (47),
From (58), we have for n = 1, ⋯ , N,
Therefore, we arrive to the following error estimate for the damage:
For some constant c > 0 and for n = 1, ⋯ , N,
Second step. Estimate of \((\varepsilon _n := \theta _n-\theta ^{hk}_n)_{ 1\le n\le N}\).
Let us fix n = 1, ⋯ , N and denote shortly \(\varepsilon _j := \theta _j-\theta ^{hk}_j \), 1 ≤ j ≤ N. We take (50), where t = t n and η = −η h, and add to (55), with η h ∈ E h, we have
Taking \( \eta ^h = \eta _n^h - \theta _n + \varepsilon _n \), then we have
From (28), we have
From (29), we have
Then, let us denote
We have
and for 𝜖 1 > 0,
and for 𝜖 > 0,
To continue, by using (48), we obtain
and thus
Consider the quantity for n = 1, ⋯ , N,
We have
Now, we sum Ξ j from j = 1 to j = n.
From (47), we have
Under the condition that
we can choose 𝜖 and 𝜖 1 such that \( \epsilon + \epsilon _1 + D_T + c_0\,c^\varphi < m_{\mathcal {K}_c}\). After some manipulation, we deduce the following error estimate for the temperature.
For some constant c > 0 independent of D V and for n = 1, ⋯ , N,
Here,
Third step. Estimate of \(( \boldsymbol {v}_n-\boldsymbol {v}^{hk}_n )_{ 1\le n\le N}\). The computation of the estimate for the velocity is similar as in [3], p. 241, which we refer for details. We mention only the main steps.
We obtain, for some constant c > 0 and for n = 1, ⋯ , N,
Here, we denote by
and for n = 1, ⋯ , N,
and
and
We have, for n = 1, ⋯ , N,
and
and
Thus, we obtain the following error estimate for the velocity.
For some constant c > 0 and for n = 1, ⋯ , N,
To summarize, adding the three inequalities (59), (61), and (62) and choosing D V and ε small enough, we obtain, for some constant c > 0 and for n = 1, ⋯ , N,
To end, let us recall the discrete version of Gronwall’s inequality, see e.g. [2].
Consider a sequence \( \{ r_n \}_{0\leq n \leq N} \subset \mathbb {R}^+\) and \(a \in \mathbb {R}^+\).
Assume
Then, we have
Now, from Gronwall’s inequality, using estimation (63) and under condition (60), we conclude that for D V small enough, then there exists some constant c > 0:
As a typical example, let us consider \(\varOmega \subset \mathbb {R}^d\), \(d\in \mathbb {N}^*\), a polygonal domain. Let \({\mathcal T}^h\) be a regular finite element partition of Ω. Let V h ⊂ V , E h ⊂ E, and \(\mathcal {K}^h_{da}\subset \mathcal {K}_{da}\) be the finite element spaces consisting of piecewise polynomials of degree ≤ m, with m ≥ 1, according to the partition \({\mathcal T}^h\). Denote by \(\varPi ^h_V\,:\, H^{m +1}(\varOmega )^d \to V^h\), \(\varPi ^h_E\,:\, H^{m +1}(\varOmega )\to E^h\), and \(\varPi ^h_K\,:\, H^{m}(\varOmega )\to \mathcal {K}^h_{da}\) the finite element interpolation operators.
Recall (see e.g. [4]) that
where r = 0 (for which H 0 = L 2) or r = 1.
We assume the following additional data and solution regularities:
Then, we choose in (64) the elements
and
From assumption (65), we have
Using these estimates in (64), we conclude to the following error estimate result.
Theorem 2
We keep the assumptions of Theorem 1 . Under the additional assumptions (47), (48), and (65), and condition (60), then for D V small enough, we obtain the error estimate for the corresponding discrete solution \( \{ ( \boldsymbol {v}_n^{hk}, \, \theta _n^{hk}, \, \alpha _n^{hk}),\ 1\leq n \leq N \} \):
In particular, for m = 1, we have
5 Numerical Computations
In this section, we provide numerical simulations in two-dimensional tests for the variational problem (QV ) by using Matlab computation codes. We refer to the previous numerical scheme and use spaces of continuous piecewise affine functions V h ⊂ V , E h ⊂ E, and \(\mathcal {K}_{da}^{h}\subset \mathcal {K}_{da}\) as families of approximating subspaces.
Here, we consider the following formulas:
In view of the numerical simulations, we consider a rectangular open set, linear elastic, and linear visco-elastic operators, for a.e. t ∈ (0, T):
Here, E Y is the Young’s modulus, r P is the Poisson’s ratio of the material, δ ij denotes the Kronecker symbol, and μ and η are viscosity constants.
For computations, we considered the following data (IS unity), for t ∈ (0, T):
Figure 1 represents the initial configuration.
In Figures 2, 3, and 4, we compute, respectively, the Von Mise norm, which gives a global measure of the stress, the temperature, and the damage at final time in the body at final time, for θ R = 0, respectively, for short and long memory visco-elasticity. In Figure 5, we show the evolution of the damage at the particular point S = (L 1, L 2) (direction of the surface traction). We observe that the distribution of these parameters is changing for long memory, the deformation is more important, as well as for the damage, temperature, and stress in the neighborhood of the point S.
Finally in Figure 6, we show the distribution of the temperature and damage of the body for larger ground temperature. Here, we observe larger deformation, larger damage, and larger temperature in the neighborhood of the contact surface.
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Chau, O., Petrov, A., Heibig, A., Marques, M.M. (2021). A Frictional Dynamic Thermal Contact Problem with Normal Compliance and Damage. In: Rassias, T.M., Pardalos, P.M. (eds) Nonlinear Analysis and Global Optimization. Springer Optimization and Its Applications, vol 167. Springer, Cham. https://doi.org/10.1007/978-3-030-61732-5_4
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