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Article

Solvability of the Boussinesq Approximation for Water Polymer Solutions

by
Mikhail A. Artemov
and
Evgenii S. Baranovskii
*
Department of Applied Mathematics, Informatics and Mechanics, Voronezh State University, 394018 Voronezh, Russia
*
Author to whom correspondence should be addressed.
Mathematics 2019, 7(7), 611; https://doi.org/10.3390/math7070611
Submission received: 22 June 2019 / Revised: 4 July 2019 / Accepted: 5 July 2019 / Published: 10 July 2019

Abstract

:
We consider nonlinear Boussinesq-type equations that model the heat transfer and steady viscous flows of weakly concentrated water solutions of polymers in a bounded three-dimensional domain with a heat source. On the boundary of the flow domain, the impermeability condition and a slip condition are provided. For the temperature field, we use a Robin boundary condition corresponding to the classical Newton law of cooling. By using the Galerkin method with special total sequences in suitable function spaces, we prove the existence of a weak solution to this boundary-value problem, assuming that the heat source intensity is bounded. Moreover, some estimates are established for weak solutions.

1. Introduction and Problem Formulation

In this work, we examine the solvability of a boundary-value problem for the Boussinesq approximation describing steady-state flows of weakly concentrated water polymer solutions [1,2] in a sufficiently regular bounded domain Ω R 3 with a heat source, under the assumption that on solid walls of Ω the impermeability condition, a vorticity-slip condition and a Robin-type temperature boundary condition are valid:
i = 1 3 u i u x i ν Δ u α i = 1 3 u i Δ u x i + grad p = T g in Ω ,
div u = 0 in Ω ,
i = 1 3 u i T x i k Δ T = ψ ( x , T ) in Ω ,
u · n | Ω = 0 , ( curl u ) × n | Ω = 0 , T n + β T | Ω = 0 .
Let us briefly describe the various terms in this system: the symbols u and p stand for the velocity and the pressure, respectively, T denotes the temperature field, the parameter ν > 0 represents the viscosity, α > 0 is the relaxation viscosity, ψ denotes the heat source intensity, g = ( 0 , 0 , g ) is the gravitational acceleration, k > 0 is the thermal conductivity, β > 0 is the Robin coefficient, and n is the unit outward normal to the surface Ω . The divergence, the gradient and the Laplacian Δ are taken with respect to the Cartesian coordinates x 1 , x 2 , x 3 .
Notice that Equations (1) and (2) without the temperature term T represent simplified equations of a stationary isothermal flow of the second grade fluid [3] (see also the book [4] for more details).
Obviously, in the case when α = 0 , we formally recover the stationary Navier–Stokes–Boussinesq system with a heat source, but, in what follows, we always assume that α > 0 . As shown in [5,6,7], the parameter α must be non-negative, in view of thermodynamic restrictions.
It is worth pointing out that there is a vast amount of literature on the model of weakly concentrated water polymer solutions and its various modifications, including the so-called Kelvin–Voigt equations that describe viscous fluid flows in which, after the instantaneous removal of stresses, the velocity does not vanish instantaneously but decays exponentially. Starting with the pioneering series of works by A.P. Oskolkov [8,9,10,11,12,13,14], there is an ever growing list of contributions. An interested reader can see the papers [15,16,17,18,19,20,21,22,23,24,25,26,27,28]; this list is by no means exhaustive, but gives a number of current mathematical results obtained for these types of viscoelastic fluids.
In the majority of works, isothermal flows are investigated, although from the point of view of applications in engineering, the analysis of heat transfer in polymer flows is no less important than the studying of hydrodynamic fields. Motivated by this, we consider problem (1)–(4). The present paper continues the investigations initiated in the articles [10,29], where the thermal convection is studied for a simplified version of the model of water polymer solutions. Namely, the authors of these papers focus on the Kelvin–Voigt–Boussinesq equations, which have a lower order (for partial derivatives with respect to the space variables) compared with the equations considered herein.
Under the assumption that the intensity of the heat source is bounded, by the Galerkin method with special total sequences in suitable function spaces, we show the existence of a weak solution to boundary-value problem (1)–(4) and derive some estimates for the norms of the velocity and temperature fields.

2. Preliminaries: Notations and Function Spaces

For Banach spaces E 1 and E 2 , by L ( E 1 , E 2 ) , we denote the space of all linear and continuous operators from E 1 to E 2 . The space L ( E 1 , E 2 ) is equipped with the norm
A L ( E 1 , E 2 ) = def sup w E 1 0 A ( w ) E 2 w E 1 .
As usual, C ( Ω ¯ ) denotes the space of all continuous functions w : Ω ¯ R .
We shall use the classical notation and results [30] for the Lebesgue spaces L q ( Ω ) , q 1 , and the Sobolev spaces: H m ( Ω ) = def W m , 2 ( Ω ) , m { 1 , 2 , } . By bold face letters, we denote the corresponding spaces of vector functions, e.g., L q ( Ω ) = def L q ( Ω ) 3 , H 1 ( Ω ) = def H 1 ( Ω ) 3 , etc.
Let us introduce the following divergence-free subspaces:
J n 1 ( Ω ) = def { v H 1 ( Ω ) : div v = 0 , v · n | Ω = 0 } , J n , curl 2 ( Ω ) = def { v H 2 ( Ω ) : div v = 0 , v · n | Ω = 0 , ( curl u ) × n | Ω = 0 } , J n , curl 3 ( Ω ) = def { v H 3 ( Ω ) : div v = 0 , v · n | Ω = Δ v · n | Ω = 0 , ( curl u ) × n | Ω = 0 } .
By X α ( Ω ) denote the space consisting of vector functions from J n , curl 2 ( Ω ) with scalar product defined according to the relation
( v , w ) X α ( Ω ) = def Ω curl v · curl w d x + α Ω Δ v · Δ w d x .
It follows from ([16] § 2) that the scalar product ( · , · ) X α ( Ω ) is well defined and the associated norm · X α ( Ω ) = def ( · , · ) X α ( Ω ) 1 / 2 is equivalent to the standard H 2 -norm.
Finally, by Y β ( Ω ) denote the space consisting of functions from H 1 ( Ω ) with the following scalar product and norm:
( S , Q ) Y β ( Ω ) = def Ω grad S · grad Q d x + β Ω S Q d σ , S Y β ( Ω ) = def ( S , S ) Y β ( Ω ) 1 / 2 .
It can easily be checked that the scalar product ( · , · ) Y β ( Ω ) is well defined and the norm · Y β ( Ω ) is equivalent to the standard H 1 -norm.

3. Weak Formulation of Problem (1)–(4) and Main Results

We propose the problem of determining the velocity field u X α ( Ω ) and the temperature T Y β ( Ω ) that satisfy the system of equations:
i = 1 3 Ω u i u · v x i d x ν Ω Δ u · v d x + α i = 1 3 Ω u i Δ u · v x i d x = Ω T g · v d x ,
i = 1 3 Ω u i T x i S d x + k Ω grad T · grad S d x + k β Ω T S d σ = Ω ψ ( x , T ) S d x ,
for any pair ( v , S ) from the space J n 1 ( Ω ) × H 1 ( Ω ) .
Definition 1.
A solution ( u , T ) X α ( Ω ) × Y β ( Ω ) to system (5) and (6) is called a weak solution of boundary value problem (1)–(4).
The following theorem gives the main result of this paper.
Theorem 1.
Let us assume that
(i)
the function ψ ( · , ξ ) : Ω R is measurable for every ξ R ;
(ii)
the function ψ ( x , · ) : R R is continuous for almost every x Ω ;
(iii)
there exists a positive constant ψ 0 such that | ψ ( x , ξ ) | ψ 0 for almost every x Ω and every ξ R .
Then, boundary value problem(1)–(4) has at least one weak solution ( u , T ) such that
u X α ( Ω ) g ψ 0 M 2 2 ( Ω , β ) M 1 ( Ω , α ) + α 1 / 2 meas ( Ω ) 1 / 2 k ν ,
T Y β ( Ω ) ψ 0 M 2 ( Ω , β ) meas ( Ω ) 1 / 2 k ,
with
M 1 ( Ω , α ) = def I α L ( X α ( Ω ) , L 2 ( Ω ) ) , M 2 ( Ω , β ) = def I β L ( Y β ( Ω ) , L 2 ( Ω ) ) ,
where I α : X α ( Ω ) L 2 ( Ω ) and I β : Y β ( Ω ) L 2 ( Ω ) are embedding operators.

4. Proof of Theorem 1

To construct a weak solution of problem (1)–(4), we shall use the Galerkin method. Let us take a sequence { w j } j = 1 from the space J n , curl 3 ( Ω ) such that { w j } j = 1 is total in J n , curl 3 ( Ω ) and
( w i , w j ) X α ( Ω ) = δ i j ,
where δ i j is the Kronecker symbol. In addition, fix a sequence { S j } j = 1 that is an orthonormal basis of Y β ( Ω ) .
For an arbitrary fixed number N { 1 , 2 , } , we consider the 2 N -dimensional auxiliary problem:
Find a vector h λ N = ( a N 1 , , a N N , b N 1 , , b N N ) R 2 N such that
λ i = 1 3 Ω u i N u N · ( w j α Δ w j ) x i d x ν Ω Δ u N · ( w j α Δ w j ) d x + λ α i = 1 3 Ω u i N Δ u N · ( w j α Δ w j ) x i d x = λ Ω T N g · ( w j α Δ w j ) d x , j = 1 , , N ,
λ i = 1 3 Ω u i N T N x i S j d x + k Ω grad T N · grad S j d x + k β Ω T N S j d σ = λ Ω ψ ( x , T N ) S j d x , j = 1 , , N ,
u N ( x ) = def j = 1 N a N j w j ( x ) , T N ( x ) = def j = 1 N b N j S j ( x ) ,
where λ is a parameter, λ [ 0 , 1 ] .
Our immediate goal is to obtain a priori estimates for solutions to problem (9)–(11). Let a vector h λ N = ( a N 1 , , a N N , b N 1 , , b N N ) be a solution of problem (9)–(11) under a fixed parameter λ [ 0 , 1 ] . It is easy to see that
| h λ N | 2 = j = 1 N a N j 2 + j = 1 N b N j 2 = u N X α ( Ω ) 2 + T N Y β ( Ω ) 2 .
Therefore, we wish to find estimates for the norms u N X α ( Ω ) and T N Y β ( Ω ) .
Let us multiply Equation (9) by a N j and add the results for j = 1 , , N . Then, we get
λ i = 1 3 Ω u i N u N · ( u N α Δ u N ) x i d x ν Ω Δ u N · ( u N α Δ u N ) d x + λ α i = 1 3 Ω u i N Δ u N · ( u N α Δ u N ) x i d x = λ Ω T N g · ( u N α Δ u N ) d x .
This equality can be rewritten as follows:
λ i = 1 3 Ω u i N ( u N α Δ u N ) · ( u N α Δ u N ) x i d x Q 1 ν Ω Δ u N · ( u N α Δ u N ) d x = λ Ω T N g · ( u N α Δ u N ) d x .
Note that the term Q 1 vanishes. Indeed, using integration by parts, we find that
Q 1 = 1 2 i = 1 3 Ω u i N x i | u N α Δ u N | 2 d x = 1 2 i = 1 3 Ω u i N n i | u N α Δ u N | 2 d σ 1 2 i = 1 3 Ω u i N x i | u N α Δ u N | 2 d x = 1 2 Ω ( u N · n ) | u N α Δ u N | 2 d σ 1 2 Ω ( div u N ) | u N α Δ u N | 2 d x = 0 .
Therefore, we have
ν Ω Δ u N · ( u N α Δ u N ) d x = λ Ω T N g · ( u N α Δ u N ) d x .
Taking into account the relation
Ω Δ v · w d x = Ω curl v · curl w d x , v J n , curl 2 ( Ω ) , w H 1 ( Ω ) ,
we can rewrite (13) as
ν Ω | curl u N | 2 d x + ν α Ω | Δ u N | 2 d x = λ Ω T N g · u N d x λ α Ω T N g · Δ u N d x .
It follows from this equality that
ν u N X α ( Ω ) 2 = ν Ω | curl u N | 2 d x + ν α Ω | Δ u N | 2 d x = λ Ω T N g · u N d x λ α Ω T N g · Δ u N d x ,
whence, using the Cauchy–Bunyakovsky–Schwarz inequality, the estimates 0 λ 1 and
u N L 2 ( Ω ) M 1 ( Ω , α ) u N X α ( Ω ) , T N L 2 ( Ω ) M 2 ( Ω , β ) T N Y β ( Ω ) ,
we derive
ν u N X α ( Ω ) 2 g Ω | T N | 2 d x 1 / 2 Ω | u N | 2 d x 1 / 2 + g α 1 / 2 Ω | T N | 2 d x 1 / 2 α Ω | Δ u N | 2 d x 1 / 2 = g T N L 2 ( Ω ) u N L 2 ( Ω ) + g α 1 / 2 T N L 2 ( Ω ) α 1 / 2 Δ u N L 2 ( Ω ) g M 2 ( Ω , β ) M 1 ( Ω , α ) + α 1 / 2 T N Y β ( Ω ) u N X α ( Ω )
and hence
u N X α ( Ω ) g M 2 ( Ω , β ) M 1 ( Ω , α ) + α 1 / 2 ν T N Y β ( Ω ) .
Next, we multiply Equation (10) by b N j and add the results for j = 1 , , N ; this gives
λ i = 1 3 Ω u i N T N x i T N d x Q 2 + k Ω | grad T N | 2 d x + k β Ω | T N | 2 d σ = λ Ω ψ ( x , T N ) T N d x .
Applying integration by parts, it can easily be checked that the term Q 2 vanishes. Indeed,
Q 2 = 1 2 i = 1 3 Ω u i N x i | T N | 2 d x = 1 2 i = 1 3 Ω u i N n i | T N | 2 d σ 1 2 i = 1 3 Ω u i N x i | T N | 2 d x = Ω ( u N · n ) | T N | 2 d σ 1 2 Ω ( div u N ) | T N | 2 d x = 0 .
Therefore, we arrive at the equality
k Ω | grad T N | 2 d x + k β Ω | T N | 2 d σ = λ Ω ψ ( x , T N ) T N d x ,
whence, using the Cauchy–Bunyakovsky–Schwarz inequality, condition (iii), the second inequality of (14), and 0 λ 1 , we derive
k T N Y β ( Ω ) 2 = λ Ω ψ ( x , T N ) T N d x Ω | ψ ( x , T N ) | 2 d x 1 / 2 Ω | T N | 2 d x 1 / 2 ψ 0 meas ( Ω ) 1 / 2 T N L 2 ( Ω ) ψ 0 meas ( Ω ) 1 / 2 M 2 ( Ω , β ) T N Y β ( Ω ) .
This yields that
T N Y β ( Ω ) ψ 0 M 2 ( Ω , β ) meas ( Ω ) 1 / 2 k .
Combining (15) and (16), we get
u N X α ( Ω ) g ψ 0 meas ( Ω ) 1 / 2 M 2 2 ( Ω , β ) M 1 ( Ω , α ) + α 1 / 2 k ν .
Finally, using (12), (16) and (17), we obtain the following a priori estimate
| h λ N | 2 g 2 ψ 0 2 meas ( Ω ) M 2 4 ( Ω , β ) M 1 ( Ω , α ) + α 1 / 2 2 k 2 ν 2 + ψ 0 2 M 2 2 ( Ω , β ) meas ( Ω ) k 2 ,
which is independent of N as well as λ .
Next, we define the operators A , G λ : R 2 N R 2 N as follows:
  • for each m { 1 , , N } , we set
    A m ( a N 1 , , a N N , b N 1 , , b N N ) = def ν Ω curl u N · curl w m d x + ν α Ω Δ u N · Δ w m d x ,
    G λ m ( a N 1 , , a N N , b N 1 , , b N N ) = def λ i = 1 3 Ω u i N u N · ( w m α Δ w m ) x i d x + λ α i = 1 3 Ω u i N Δ u N · ( w m α Δ w m ) x i d x λ Ω T N g · ( w m α Δ w m ) d x ;
  • for each m { N + 1 , , 2 N } , we set
    A m ( a N 1 , , a N N , b N 1 , , b N N ) = def k Ω grad T N · grad S m N d x + k β Ω T N · S m N d σ ,
    G λ m ( a N 1 , , a N N , b N 1 , , b N N ) = def λ i = 1 3 Ω u i N T N x i S m N d x λ Ω ψ ( x , T N ) S m N d x ,
where ( a N 1 , , a N N , b N 1 , , b N N ) is an arbitrary vector from space R 2 N , while functions u N and T N are defined by (11).
Letting
F ( a N 1 , , a N N , b N 1 , , b N N , λ ) = def A ( a N 1 , , a N N , b N 1 , , b N N ) + G λ ( a N 1 , , a N N , b N 1 , , b N N ) ,
we note that the Galerkin system (9)–(11) is equivalent to the following equation
F ( a N 1 , , a N N , b N 1 , , b N N , λ ) = 0 R 2 N ,
where λ [ 0 , 1 ] .
It is worth pointing out that
F ( a N 1 , , a N N , b N 1 , , b N N , 0 ) = A ( a N 1 , , a N N , b N 1 , , b N N )
and the operator A is an isomorphism due to the relation
A ( a N 1 , , a N N , b N 1 , , b N N ) = ( ν a N 1 , , ν a N N , k b N 1 , , k b N N ) .
Then, an application of Proposition A1 (see the Appendix A) together with a priori estimate (18) allows us to state that problem (9)–(11) is solvable for any N { 1 , 2 , } and λ [ 0 , 1 ] .
Let { u * N } N = 1 and { T * N } N = 1 be sequences of functions that satisfy (9) and (10) with the parameter λ = 1 , i.e.,
i = 1 3 Ω u * i N u * N · ( w j α Δ w j ) x i d x ν Ω Δ u * N · ( w j α Δ w j ) d x + α i = 1 3 Ω u * i N Δ u * N · ( w j α Δ w j ) x i d x = Ω T * N g · ( w j α Δ w j ) d x , j = 1 , , N ,
i = 1 3 Ω u * i N T * N x i S j d x + k Ω grad T * N · grad S j d x + k β Ω T * N S j d σ = Ω ψ ( x , T * N ) S j d x , j = 1 , , N .
It follows from estimates (16) and (17) that the set { u * N } N = 1 is bounded in the space X α ( Ω ) and the set { T * N } N = 1 is bounded in the space Y β ( Ω ) . Hence, there exists a vector function u 0 from the space X α ( Ω ) and a function T 0 from the space Y β ( Ω ) such that u * N converges to u 0 weakly in X α ( Ω ) and T * N converges to T 0 weakly in Y β ( Ω ) , for some subsequence N . Without loss of generality, we can assume that
lim N u * N = u 0 weakly in X α ( Ω ) ,
lim N T * N = T 0 weakly in Y β ( Ω ) .
Using standard compactness results for the Sobolev spaces (see, e.g., [30] Chap. 6), we derive that the space X α ( Ω ) is compactly imbedded into C ( Ω ¯ ) and the space Y β ( Ω ) is compactly imbedded into L q ( Ω ) when 1 q < 6 . Therefore, it follows from (22) and (23) that
lim N u * N = u 0 strongly in C ( Ω ¯ ) ,
lim N T * N = T 0 strongly in L q ( Ω ) ,
where 1 q < 6 .
Furthermore, by using the theorem of M. A. Krasnoselskii on a superposition operator (see the Appendix A, Proposition A2), we conclude from conditions (i)–(iii) and (25) that
lim N ψ · , T * N ( · ) = ψ · , T 0 ( · ) strongly in L 2 ( Ω ) .
Fix an arbitrary number j { 1 , 2 , } . Then, letting m in (20) and (21), we get
i = 1 3 Ω u 0 i u 0 · ( w j α Δ w j ) x i d x ν Ω Δ u 0 · ( w j α Δ w j ) d x + α i = 1 3 Ω u 0 i Δ u 0 · ( w j α Δ w j ) x i d x = Ω T 0 g · ( w j α Δ w j ) d x ,
i = 1 3 Ω u 0 i T 0 x i S j d x + k Ω grad T 0 · grad S j d x + k β Ω T 0 S j d σ = Ω ψ ( x , T 0 ) S j d x .
Of course, in this passage-to-limit procedure, we used all the convergence results (22)–(26).
It follows from ([16] § 2) that the mapping R α defined by
R α : J n , curl 3 ( Ω ) J n 1 ( Ω ) , R α ( v ) = def v α Δ v
is an isomorphism. Therefore, the sequence { w j α Δ w j } j = 1 is total in the space J n 1 ( Ω ) . This fact is a key tool in our proof. Indeed, due to this property, equality (27) remains valid if we replace w j α Δ w j with an arbitrary vector function v from J n 1 ( Ω ) . In addition, since the set { S j } j = 1 is total in H 1 ( Ω ) , we see that (28) is true with an arbitrary function S from H 1 ( Ω ) instead of S j . Thus, we have established that the pair ( u 0 , T 0 ) is a weak solution of problem (1)–(4).
Moreover, in view of estimates (16) and (17), we obviously have the inequalities (7) and (8) with u = u 0 and T = T 0 . The proof of Theorem 1 is complete.

5. Conclusions

In this paper, we considered nonlinear Boussinesq-type equations describing the heat transfer and steady viscous flows of weakly concentrated water solutions of polymers in a bounded three-dimensional domain with sufficiently smooth boundary. We proved the existence of weak solutions in suitable function classes. Besides, some estimates for weak solutions are obtained in terms of the data of this model.

Author Contributions

Writing—Original draft M.A.A.; methodology, E.S.B.; Writing—review and editing, E.S.B.

Funding

This research received no external funding.

Conflicts of Interest

The authors declare no conflict of interest.

Appendix A

For the reader’s convenience, let us state an important generalization of the Brouwer fixed-point theorem, which is used in our proof.
Proposition A1.
Suppose B r = def { x R d : | x | < r } and a continuous operator F : B ¯ r × [ 0 , 1 ] R d satisfies the following conditions:
  • F ( x , λ ) 0 for any ( x , λ ) B r × [ 0 , 1 ] ;
  • F ( x , 0 ) = A x for any x B ¯ r , where A : R d R d is an isomorphism.
Then, for any λ [ 0 , 1 ] , the equation F ( x , λ ) = 0 has at least one solution x λ , which belong to the ball B r .
This proposition can be proved by methods of the topological degree theory (see, e.g., [31]).
In addition, recall the well-known theorem of M.A. Krasnoselskii on a superposition operator acting in Lebesgue spaces.
Proposition A2.
Let f : Ω × R R be a function such that
  • the function f ( · , ξ ) : Ω R is measurable for every ξ R ;
  • the function f ( x , · ) : R R is continuous for almost every x Ω ;
  • there exist constants q 1 , q 2 1 , C > 0 and a function ϕ L q 2 ( Ω ) such that the following inequality holds
    | f ( x , ξ ) | ϕ ( x ) + C | ξ | q 1 / q 2 ,
    for almost every x Ω and every ξ R .
Under these hypotheses, the superposition operator Φ f defined by
Φ f : L q 1 ( Ω ) L q 2 ( Ω ) , Φ f ( w ) ( x ) = def f ( x , w ( x ) )
is a bounded and continuous mapping.
The proof of this result can be found in the book ([32] Chap. 1).

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MDPI and ACS Style

Artemov, M.A.; Baranovskii, E.S. Solvability of the Boussinesq Approximation for Water Polymer Solutions. Mathematics 2019, 7, 611. https://doi.org/10.3390/math7070611

AMA Style

Artemov MA, Baranovskii ES. Solvability of the Boussinesq Approximation for Water Polymer Solutions. Mathematics. 2019; 7(7):611. https://doi.org/10.3390/math7070611

Chicago/Turabian Style

Artemov, Mikhail A., and Evgenii S. Baranovskii. 2019. "Solvability of the Boussinesq Approximation for Water Polymer Solutions" Mathematics 7, no. 7: 611. https://doi.org/10.3390/math7070611

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