On Anisotropic Conservative Caginalp Phase-Field System Based on Type III Heat Conduction with Two Temperatures and Periodic Boundary Conditions

On Anisotropic Conservative Caginalp Phase-Field System Based on Type III Heat Conduction with Two Temperatures and  Periodic Boundary Conditions

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On Anisotropic Conservative Caginalp Phase-Field System Based on Type III Heat Conduction with Two Temperatures and  Periodic Boundary Conditions Banner

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Background

Abstract

Our aim in this paper is to study the well-posedness results of anisotropic conservative Caginalp phase-field system based on the theory of type III thermomechanics with two temperatures for the heat conduction and periodic boundary conditions. More precisely, we prove the existence and uniqueness of solutions.

I. INTRODUCTION

The authors studied in [13](see aigain [12]) the following phase-field system, namely,

( 1.1 ) E q u a t i o n ( 1.1 ) i s f o l l o w e d b y u t Δ u + f ( u ) = α t Δ α t ,
( 1.2 ) 2 α t 2 Δ 2 α t 2 Δ α t Δ α = u t ,
( 1.3 ) α ( t , x ) = α ( 0 , x ) + 0 t T ( τ , x ) d τ ,

where, u is the order parameter, T is the relative temperature (defined as T = T ~ T E , where T ~ is the absolute temperature and T E is the equilibrium melting temperature), α is the conductive thermal displacement and f is the derivative of a double-well potential F (a typical choice is F ( s ) = 1 4 ( s 2 1 ) 2 , hence the usual cubic nonlinear term f ( s ) = s 3 s ). Furthermore, here and below, we set all physical parameters equal to one. This system has been introduced to model phase transition phenomena, such as melting-solidification phenomena, and has been much studied from a mathematical point of view. We refer the reader to, e.g., [4-5, 8-11, 14, 16, 17, 21, 23].

This system is based on the (total Ginzburg-Landau) free energy,

Ψ GL = Ω ( 1 2 | u | 2 + F ( u ) u T 1 2 T 2 ) d x ,

where Ω is the domain occupied by the system (we assume here that it is a bounded and regular domain of R n , n = 2 or n = 3 , with boundary Γ ), and the enthalpy

( 1.5 ) H = u + T Δ T .

As far as the evolution equation for the order parameter is concerned, one postulates the relaxation dynamics (with relaxation parameter set equal to one)

u u = D Ψ G L D u ,

where D D u denotes a variational derivative with respect to u . Then, we have the energy equation

( 1.7 ) H t = divq

and owing to (1.7),

( 1.8 ) T t Δ T t + divq = u t ,

where q is the heat flux. Assuming finally the usual Fourier law for heat conduction,

( 1.9 ) q = α T ,

we obtain (1.1) and (1.2).

Our aim in this paper is to study the model consisting of the conserved anisotropic to (1.1)-(1.2), namely,

( 1.10 ) u t + Δ i = 1 3 a i 2 u x i 2 Δ f ( u ) = Δ ( α t Δ α t ) , a i > 0 ,
( 1.11 ) 2 α t 2 Δ 2 α t 2 Δ α t Δ α = u t .

Our aim in this paper is to study the model consisting of the anisotropic conservative equation (1.10) and the temperature equation (1.11). In particular, we obtain the existence and uniqueness of solutions.

II. SETTING OF THE PROBLEM

Find the order parameter u : Ω × R + R and the terminal displacement α : Ω × R + R such that:

( 2.1 ) u t + Δ i = 1 3 a i 2 u x i 2 Δ f ( u ) = Δ ( α t Δ α t ) ,
( 2.2 ) 2 α t 2 Δ 2 α t 2 Δ α t Δ α = u t ,

together with periodic boundary conditions

( 2.3 ) u and α are Ω periodic ,

and the initial conditions

( 2.4 ) u | t = 0 = u 0 , α | t = 0 = α 0 , α t | t = 0 = α 1 .

We assume that

( 2.5 ) a i > 0 , i { 1 , 2 , 3 } ,

and we introduce the elliptic operator A defined by

( 2.6 ) A v , w H 1 ( Ω ) , H p e r 1 ( Ω ) = i = 1 3 a i ( ( v x i , w x i ) ) ,

where H 1 ( Ω ) is the topological dual of H p e r 1 ( Ω ) . Furthermore, ( ( . , ) ) denotes the usual L 2 -scalar product, with associated norm . ; more generally, we denote by . X the norm on the Banach space X and we set . 1 = ( Δ ) 1 2 . , ( Δ ) 1 denoting the inverse minus Laplace operator with periodic boundary conditions and acting on functions with null average, is a norm in H 1 ( Ω ) = H p e r 1 ( Ω ) which is equivalent to the usual H 1 -norm. We can note that

( v , w ) H p e r 1 ( Ω ) 2 i = 1 3 a i ( ( v x i , w x i ) )

is bilinear, symmetric, continuous and coercive, so that

A : H p e r 1 ( Ω ) H 1 ( Ω )

is indeed well defined. It then follows from elliptic regularity results for linear elliptic operators of order 2 (see [1-2]) that A is a strictly positive, selfadjoint and unbounded linear operator with compact inverse, with domain

D ( A ) = H p e r 2 ( Ω ) ,

where, for v D ( A )

A v = i = 1 3 a i 2 v x i 2 .

We further note that D ( A 1 2 ) = H p e r 1 ( Ω ) and, for v D ( A 1 2 ) ,

( ( A 1 2 v , A 1 2 v ) ) = i = 1 3 a i v x i 2 .

We finally note that (see, e.g., [18]) v ( A v 2 + v 2 ) 1 2 defines a norm on H p e r 2 ( Ω ) which is equivalent to the usual H 2 -norm on D ( A ) (resp., v ( A 1 2 v 2 + v 2 ) 1 2 defines a norm on H p e r 1 ( Ω ) which is equivalent to the usual H 1 -norm on D ( A 1 2 ) ), where

. = 1 Vol ( Ω ) Ω . d x ,

being understood that, for v H 1 ( Ω )

v = 1 Vol ( Ω ) v , 1 H 1 ( Ω ) , H p e r 1 ( Ω ) ,

and we note that

v ( v v 1 2 + v 2 ) 1 2

is a norm on H 1 ( Ω ) which is equivalent to the usual one. Here, Ω = i = 1 n ( 0 , L i ) , L i > 0 , n = 2 or n = 3 . Furthermore, for a space W we shall denote by W ˙ the space

W ˙ = { v W , v = 0 } .

Remark 2.1. Actually, the conserved phase-field system usually is endowed with Neumann boundary conditions. In our case, these conditions read

u ν = Δ u ν ( = A u ν ) = α ν = 0 o n Γ ,

where ν denotes the unit outer normal.

Remark 2.2. Note that similar properties hold for the operator Δ , with obvious changes.

Having this, we rewrite (2.1) as

( 2.8 ) u t Δ A u Δ f ( u ) = Δ ( α t Δ α t ) .

Furthermore, we assume that the function f satisfies the following conditions:

( 2.9 ) f C 2 ( R ) , f ( 0 ) = 0 ,
( 2.10 ) f c 0 , c 0 0 ,
( 2.11 ) f ( s ) s c 1 F ( s ) c 2 , F ( s ) c 3 , c 1 > 0 , c 2 , c 3 0 , s R ,

where, we denote by F the primitive of f vanishing at s = 0 ,

( 2.12 ) c 4 s 2 p 1 c 5 f ( s ) c 6 s 2 p 1 + c 7 , c 4 , c 6 > 0 , c 5 , c 7 0 , p 1 , s R .

Remark 2.3. In particular, these assumptions are satisfied by function

f ( s ) = i = 1 2 p + 1 a i s i , a 2 p + 1 > 0 , s R

(and, the usual cubic nonlinear term f ( s ) = s 3 s ).

Throughout the paper, the same letters c , c and c denote (generally positive) constants which may vary from line to line. Similarly, the same letter Q denotes (positive) monotone increasing (with respect to each argument) and continuous functions which may vary from line to line.

III. A PRIORI ESTIMATES

The estimates below are formal, but they can also be justified within a Galerkin scheme for the approximated problem.

We first note that, integrating (formally) (2.8) over Ω , we have

d u d t = 0 ,

hence

( 3.1 ) u ( t ) = u 0 , t 0.

Furthermore, integrating (2.2) over Ω , we obtain, in view of (2.7),

( 3.2 ) d 2 α d t 2 = d u d t .

It thus follows from (2.4) and (3.2) that

( 3.3 ) d α d t = u 0 + α 1 u ,

meaning, in particular, that u + α t is a conserved quantity and from (3.1) that

( 3.4 ) d α d t = α 1 ,

so that

( 3.5 ) α ( t ) = α 0 + α 1 t , t 0.

We now assume that

( 3.6 ) | u 0 | M 1 , | α 1 | M 2 , | u 0 + α 1 | M 1 + M 2 ,

for fixed positive constants M 1 et M 2 . Thus,

( 3.7 ) | u ( t ) | M 1 , | α t ( t ) | M 2 , | u + α t ( t ) | M 1 + M 2 , t 0.

Furthermore, it follows from (3.5) that

( 3.8 ) | α ( t ) | | α 0 | + | α 1 | t , t 0.

We rewrite, in view of (3.4), (2.8) as

( 3.9 ) ( Δ ) 1 u t + A u + f ( u ) f ( u ) = α t Δ α t + α 1

and, in view of (3.3) an (3.9) that

( 3.10 ) ( Δ ) 1 u t + A u + f ( u ) f ( u ) = α ¯ t Δ α ¯ t + α 1 .

Furthermore, we deduce from (2.2) and (3.2) that

( 3.11 ) 2 α ¯ t 2 Δ 2 α ¯ t 2 Δ α ¯ t Δ α ¯ = u ¯ t ,

We first multiply (3.9) by u t and obtain, noting that u t = 0

( 3.12 ) 1 2 d d t ( A 1 2 u 2 + 2 Ω F ( u ) d x ) + u t 1 2 = ( ( α t Δ α t , u t ) ) .

We then multiply (2.2) by α t Δ α t to obtain

( 3.13 ) 1 2 d d t ( α 2 + Δ α 2 + α t Δ α t 2 ) + α t 2 + Δ α t 2 = ( ( α t Δ α t , u t ) )

(note indeed that α t Δ α t 2 = α t 2 + 2 α t 2 + Δ α t 2 ).

Summing finally (3.12) and (3.13), we find a differential equality

( 3.14 ) d E 1 d t + 2 u t 1 2 + 2 α t 2 + 2 Δ α t 2 = 0
E 1 = A 1 2 u 2 + 2 Ω F ( u ) d x + α 2 + Δ α 2 + α t Δ α t 2

satisfies, owing to (2.12),

( 3.15 ) c ( A 1 2 u 2 + u L 2 p + 2 ( Ω ) 2 p + 2 + Δ α 2 + Δ α t 2 ) + c E 1 c ( A 1 2 u 2 + u L 2 p + 2 ( Ω ) 2 p + 2 + Δ α 2 + Δ α t 2 ) + c , c , c > 0.

(here and below, when not specified, the sign of the constants ( c and c ) can be arbitrary). Multiplying (3.9) by u and have, integrating over Ω and by parts,

1 2 d d t u 1 2 + A 1 2 u 2 + ( ( f ( u ) , u ) ) = ( ( α t Δ α t , u ) ) + ( ( f ( u ) , u ) ) ( ( α t Δ α t , u ) ) .

It follows from (2.11) that

( ( f ( u ) , u ) ) c 2 Ω F ( u ) d x + c ,

from (2.12) and (3.7) that

| ( ( f ( u ) , u ) ) | c M 1 Ω | f ( u ) | d x c 2 2 Ω F ( u ) d x + c M 1

and from (3.7) that

( 3.16 ) | ( ( α t , u ) ) | c M 1 , M 2 .

Therefore, owing again to (3.7) and remembering that v ( A 1 2 v 2 + v 2 ) 1 2 is a norm in H p e r 1 ( Ω ) which is equivalent to the usual H 1 -norm,

( 3.17 ) d d t u ¯ 1 2 + c ( u H p e r 1 ( Ω ) 2 + 2 Ω F ( u ) d x ) c ( α t 2 + Δ α t 2 ) + c M 1 , M 2 , c > 0.

Summing (3.14) and δ 1 ( 3.17 ) , where δ 1 > 0 is small enough, we have a differential inequality of the form

( 3.18 ) d E 2 d t + c ( u H p e r 1 ( Ω ) 2 + 2 Ω F ( u ) d x + u t 1 2 + α t H p e r 2 ( Ω ) 2 ) + c M 1 , M 2 , c > 0 ,
E 2 = E 1 + δ 1 u 1 2

satisfies

( 3.19 ) c ( A 1 2 u 2 + u L 2 p + 2 ( Ω ) 2 p + 2 + Δ α 2 + Δ α t 2 ) + c E 2 c ( A 1 2 u 2 + u L 2 p + 2 ( Ω ) 2 p + 2 + Δ α 2 + Δ α t 2 ) + c , c , c > 0.

We multiply (2.8) by u to obtain, owing to (2.9) and (2.10),

( 3.20 ) d d t u 2 + A 1 2 u 2 c ( u H p e r 1 ( Ω ) 2 + α t 2 + Δ α t 2 ) .

Summing (3.18) and δ 2 ( 3.20 ) , where δ 2 > 0 is small enough, we obtain a differential inequality of the form

( 3.21 ) d E 3 d t + c ( u H p e r 2 ( Ω ) 2 + 2 Ω F ( u ) d x + u t 1 2 + α t H p e r 2 ( Ω ) 2 ) c M 1 , M 2 , c > 0 ,

where

E 3 = E 2 + δ 2 u 2

satisfies

( 3.22 ) c ( u H p e r 1 ( Ω ) 2 + u L 2 p + 2 ( Ω ) 2 p + 2 + Δ α 2 + Δ α t 2 ) + c E 3 c ( u H p e r 1 ( Ω ) 2 + u L 2 p + 2 ( Ω ) 2 p + 2 + Δ α 2 + Δ α t 2 ) + c , c , c > 0.

Now, multiplying (3.10) by u t , we have

( 3.23 ) 1 2 d d t ( A 1 2 u 2 + 2 Ω F ( u ) d x ) + u t 1 2 = ( ( α ¯ t Δ α ¯ t , u ¯ t ) ) .

We then multiply (3.11) by α t Δ α t

( 3.24 ) 1 2 d d t ( α 2 + Δ α 2 + α t Δ α t 2 ) + α t 2 + Δ α t 2 = ( ( α ¯ t Δ α ¯ t , u ¯ t ) )

(note indeed that α t Δ α t 2 = α t 2 + 2 α t 2 + Δ α t 2 ).

Summing finally (3.21), (3.23) and (3.24), we obtain a differential inequality of the form

( 3.25 ) d E 4 d t + c ( u H p e r 2 ( Ω ) 2 + 2 Ω F ( u ) d x + u t 1 2 + α t H p e r 2 ( Ω ) 2 + α t H p e r 2 ( Ω ) 2 ) c M 1 , M 2 , c > 0 ,

where

E 4 = E 3 + A 1 2 u 2 + 2 Ω F ( u ) d x + α 2 + Δ α 2 + α t Δ α t 2

satisfies

( 3.26 ) c ( u H p e r 1 ( Ω ) 2 + u L 2 p + 2 ( Ω ) 2 p + 2 + Δ α 2 + Δ α t 2 + Δ α 2 + Δ α t 2 ) + c E 4 . c ( u H p e r 1 ( Ω ) 2 + u L 2 p + 2 ( Ω ) 2 p + 2 + Δ α 2 + Δ α t 2 + Δ α ¯ 2 + Δ α ¯ t 2 ) + c , c , c > 0.

We finally assume that p = 1 when n = 3 and multiply (2.8) by A u to find

1 2 d d t A 1 2 u 2 + A u 2 + ( ( f ( u ) u , A u ) ) = ( ( α t Δ α t , A u ) ) .

We assume that n = 3 and p = 1 (the case n = 2 can be treated in a similar way) and have, owing to (2.12) and Hölder's inequality,

| ( ( f ( u ) u , A u ) ) | c Ω ( | u | 2 + 1 ) | u | | A u | d x c ( u L 6 ( Ω ) 2 + 1 ) u L 6 ( Ω ) A u c ( u H p e r 1 ( Ω ) 2 + 1 ) u H p e r 2 ( Ω ) A u .

Notes

Therefore,

( 3.27 ) d d t A 1 2 u 2 + A u 2 c ( u H p e r 1 ( Ω ) 4 + 1 ) u H p e r 2 ( Ω ) 2 + c ( α t 2 + Δ α t 2 ) .

IV. WELL-POSEDNESS

We have the following result.

Theorem 4.1. We assume that (2.9)-(2.12) hold. Then, for every ( u 0 , α 0 , α 1 ) ( H p e r 1 ( Ω ) L 2 p + 2 ( Ω ) ) × H p e r 2 ( Ω ) × H p e r 2 ( Ω ) ) , (2.1)-(2.4) possesses at least one solution ( u , α , α t ) such that

u L ( 0 , T ; H p e r 1 ( Ω ) L 2 p + 2 ( Ω ) ) L 2 ( 0 , T ; H p e r 2 ( Ω ) ) ,
u t L 2 ( 0 , T ; H 1 ( Ω ) ) ,
α , α L ( 0 , T ; H p e r 2 ( Ω ) )

and

α t , α t L ( 0 , T ; H p e r 2 ( Ω ) ) L 2 ( 0 , T ; H p e r 2 ( Ω ) )

T > 0

Furthermore, if p = 1 when n = 3 , then

u L 2 ( 0 , T ; H p e r 3 ( Ω ) ) .

Proof. The proof is based on (3.8), (3.25), (3.27) and, e.g., a standard Galerkin scheme.

We have, concerning the uniqueness, the following.

Theorem 4.2. We assume that the assumptions of Theorem 4.1 hold and that p = 1 when n = 3 and p [ 1 , 2 ] when n = 2 . Then, the solution obtained in Theorem 4.1 is unique.

Proof. Let ( u ( 1 ) , α ( 1 ) , α ( 1 ) t ) and ( u ( 2 ) , α ( 2 ) , α ( 2 ) t ) be two solutions to (2.1)-(2.3) with initial data ( u 0 ( 1 ) , α 0 ( 1 ) , α 1 ( 1 ) ) and ( u 0 ( 2 ) , α 0 ( 2 ) , α 1 ( 2 ) ) , respectively, such that

( 4.1 ) | u 0 ( i ) | M 1 , | α 1 ( i ) | M 2 , | u 0 ( i ) + α 1 ( i ) | M 1 + M 2 , i = 1 , 2 ,

for fixed positive constants M 1 and M 2 .We set

( u , α , α t ) = ( u ( 1 ) , α ( 1 ) , α ( 1 ) t ) ( u ( 2 ) , α ( 2 ) , α ( 2 ) t )

and

( u 0 , α 0 , α 1 ) = ( u 0 ( 1 ) , α 0 ( 1 ) , α 1 ( 1 ) ) ( u 0 ( 2 ) , α 0 ( 2 ) , α 1 ( 2 ) ) .

We have

( 4.2 ) ( Δ ) 1 u t + A u + f ( u ( 1 ) ) f ( u ( 2 ) ) f ( u ( 1 ) ) f ( u ( 2 ) ) = α t Δ α t + α 1 ,
( 4.3 ) 2 α t 2 Δ 2 α t 2 Δ α t Δ α = u t ,
( 4.4 ) u a n d α a r e Ω p e r i o d i c ,
( 4.5 ) u | t = 0 = u 0 , α | t = 0 = α 0 , α t | t = 0 = α 1 .

We multiply (4.2) by u t (note that u t = 0 ) and obtain

( 4.6 ) 1 2 d d t A 1 2 u 2 + u t 1 2 = ( ( α t Δ α t , u t ) ) ( ( f ( u ( 1 ) ) f ( u ( 2 ) ) , u t ) ) .

We first assume that n = 3 and p = 1 . We have

| ( ( f ( u ( 1 ) ) f ( u ( 2 ) ) , u t ) ) | = | ( ( f ( u ( 1 ) ) f ( u ( 2 ) ) f ( u ( 1 ) ) f ( u ( 2 ) ) , u t ) ) |
( f ( u ( 1 ) ) f ( u ( 2 ) ) ) u t 1 = ( 0 1 f ( u ( 1 ) + s ( u ( 2 ) u ( 1 ) ) ) d s u ) u t 1 0 1 f ( u ( 1 ) + s ( u ( 2 ) u ( 1 ) ) ) d s u u t 1 + u 0 1 f ( u ( 1 ) + s ( u ( 2 ) u ( 1 ) ) ) ( u ( 1 ) + s ( u ( 2 ) u ( 1 ) ) ) d s u t 1 .

Furthermore, owing to Agmon's inequality,

0 1 f ( u ( 1 ) + s ( u ( 2 ) u ( 1 ) ) ) d s u 2 c Ω ( | u ( 1 ) | 4 + | u ( 2 ) | 4 + 1 ) | u | 2 d x c ( u ( 1 ) L ( Ω ) 4 + u ( 2 ) L ( Ω ) 4 + 1 ) u 2 c ( u ( 1 ) H p e r 1 ( Ω ) 2 + u ( 2 ) H p e r 1 ( Ω ) 2 + 1 ) × ( u ( 1 ) H p e r 2 ( Ω ) 2 + u ( 2 ) H p e r 2 ( Ω ) 2 + 1 ) u 2

and, owing to Hölder's inequality,

u 0 1 f ( u ( 1 ) + s ( u ( 2 ) u ( 1 ) ) ) ( u ( 1 ) + s ( u ( 2 ) u ( 1 ) ) ) d s 2 c Ω ( | u ( 1 ) | 2 + | u ( 2 ) | 2 + 1 ) ( | u ( 1 ) | 2 + | u ( 2 ) | 2 ) | u | 2 d x c ( u ( 1 ) H p e r 1 ( Ω ) 2 + u ( 2 ) H p e r 1 ( Ω ) 2 + 1 ) ( u ( 1 ) H p e r 2 ( Ω ) 2 + u ( 2 ) H p e r 2 ( Ω ) 2 ) u H p e r 1 ( Ω ) 2 .

We now assume that n = 2 and we take the most complicated case p = 2 . Then, owing to Agmon's inequality and a proper interpolation inequality,

| | 0 1 f ( u ( 1 ) + s ( u ( 2 ) u ( 1 ) ) ) d s u | | 2 c Ω ( | u ( 1 ) | 8 + | u ( 2 ) | 8 + 1 ) | u | 2 d x c ( u ( 1 ) L ( Ω ) 8 + u ( 2 ) L ( Ω ) 8 + 1 ) u 2 c ( u ( 1 ) 4 u ( 1 ) H p e r 2 ( Ω ) 4 + u ( 1 ) 4 u ( 1 ) H p e r 2 ( Ω ) 4 + 1 ) u 2 c ( u ( 1 ) H p e r 1 ( Ω ) 6 + u ( 2 ) H p e r 1 ( Ω ) 6 + 1 ) ( u ( 1 ) H p e r 3 ( Ω ) 2 + u ( 2 ) H p e r 3 ( Ω ) 2 + 1 ) u 2 .

Furthermore, owing to Hölder's inequality,

u 0 1 f ( u ( 1 ) + s ( u ( 2 ) u ( 1 ) ) ) ( u ( 1 ) + s ( u ( 2 ) u ( 1 ) ) ) d s 2 c Ω ( | u ( 1 ) | 6 + | u ( 2 ) | 6 + 1 ) ( | u ( 1 ) | 2 + | u ( 2 ) | 2 ) | u | 2 d x c ( u ( 1 ) H p e r 1 ( Ω ) 6 + u ( 2 ) H p e r 1 ( Ω ) 6 + 1 ) ( u ( 1 ) H p e r 2 ( Ω ) 2 + u ( 2 ) H p e r 1 ( Ω ) 2 ) u H p e r 1 ( Ω ) 2 .

Finally, we obtain, in both cases, an inequality of the form

d d t A 1 2 u 2 + u t 1 2 2 ( ( α t Δ α t , u t ) ) + c ( u ( 1 ) H p e r 1 ( Ω ) q + u ( 2 ) H p e r 1 ( Ω ) q + 1 ) ( u ( 1 ) H p e r 3 ( Ω ) 2 + u ( 2 ) H p e r 3 ( Ω ) 2 + 1 ) u 2 , q 1. ( 4. 7 )

Multiplying then (4.3) by α t Δ α t , we find

( 4.8 ) d d t ( α 2 + Δ α 2 + α t Δ α t 2 ) + 2 α t 2 + 2 Δ α t 2 = 2 ( ( α t Δ α t , u t ) ) .

Summing finally (4.7) and (4.8), we have, an inequality of the form

( 4.9 ) d E 5 d t c ( u ( 1 ) H p e r 1 ( Ω ) q + u ( 2 ) H p e r 1 ( Ω ) q + 1 ) ( u ( 1 ) H p e r 3 ( Ω ) 2 + u ( 2 ) H p e r 3 ( Ω ) 2 + 1 ) E 4 ,

q 1 , where

E 5 = A 1 2 u 2 + α 2 + Δ α 2 + α t Δ α t 2 .

Then, We deduce from (4.9), (3.8), the estimates obtained in the previous subsection and Gronwall's lemma the uniqueness, as well as the continuous dependence with respect to the initial data.

V. REGULARITY OF SOLUTIONS

We have the following result which gives the existence and uniqueness of more regular solutions.

Theorem 5.1. We assume that the assumptions of Theorem 4.1 hold and that (2.12) is replaced by

( 5.1 ) | f ( s ) | ϵ F ( s ) + c ϵ , ϵ > 0 , s R .

Then, if ( u 0 , α 0 , α 1 ) H p e r 2 ( Ω ) × H p e r 3 ( Ω ) × H p e r 3 ( Ω ) , the problem possesses a unique solution such that

u L ( 0 , T ; H p e r 2 ( Ω ) )

and

α , α t L ( 0 , T ; H p e r 3 ( Ω ) ) , T > 0.

Proof. The proof of uniqueness is obtained by proceeding as in that of Theorem 4.2, noting that, with the higher regularity considered here, no growth assumption on f is needed, owing to the continuous embedding H p e r 2 ( Ω ) L ( Ω ) .

We now turn to the proof of existence and, more precisely, of the further regularity of the solutions.

We multiply (2.8) by u t , we have

( 5.2 ) 1 2 d d t A 1 2 u 2 + u t 2 = ( ( Δ f ( u ) , u t ) ) + ( ( u t , α t Δ α t ) ) .

Multiplying then (2.2) by Δ ( α t Δ α t ) , we obtain

( 5.3 ) 1 2 d d t ( Δ α 2 + Δ α 2 + α t Δ α t 2 ) + Δ α t 2 + Δ α t 2 = ( ( u t , α t Δ α t ) ) .

Summing finally (5.2) and (5.3), we find

( 5.4 ) 1 2 d d t ( A 1 2 u 2 + Δ α 2 + Δ α 2 + α t Δ α t 2 ) + u t 2 + Δ α t 2 + Δ α t 2 = ( ( Δ f ( u ) , u t ) ) .

It follows from (5.4) and the continuous embedding H p e r 2 ( Ω ) C ( Ω ) that

( 5.5 ) d d t ( A 1 2 u 2 + Δ α 2 + Δ α 2 + α t Δ α t 2 ) + u t 2 + 2 Δ α t 2 + 2 Δ α t 2 Q ( Δ u 2 ) .

We set

( 5.6 ) y = A 1 2 u 2 + Δ α 2 + Δ α 2 + α t Δ α t 2

and we deduce from (5.5) that we have an inequality of the form

( 5.7 ) y Q ( y ) .

Let z be the solution to the ordinary differential equation

( 5.8 ) z = Q ( z ) , z ( 0 ) = y ( 0 ) .

It follows from the comparison principle that there exists T 0 = T 0 ( u 0 H p e r 2 ( Ω ) , α 0 H p e r 3 ( Ω ) , α 1 H p e r 3 ( Ω ) ) (say, belongin to ( 0 , 1 2 ) ) such that

( 5.9 ) y ( t ) z ( t ) , t [ 0 , T 0 ] ,

from which it follows, owing also to (3.8) and (3.25), that

( 5.10 ) u ( t ) H p e r 2 ( Ω ) 2 + α ( t ) H p e r 3 ( Ω ) 2 + α t ( t ) H p e r 3 ( Ω ) 2 Q M 1 , M 2 ( u 0 H p e r 2 ( Ω ) , α 0 H p e r 3 ( Ω ) , α 1 H p e r 3 ( Ω ) ) , t [ 0 , T 0 ] .

We now differentiate (3.9) with respect to times and have, owing to (2.2),

( 5.11 ) ( Δ ) 1 t u t + A u t + f ( u ) u t f ( u ) u t = Δ α + Δ α t u t .

We multiply (5.11) by t u t and have

1 2 d d t ( t u t 1 2 ) + t A 1 2 u t 2 + t ( ( f ( u ) u t , u t ) ) = t ( ( α , u t ) ) t ( ( α t , u t ) ) t u t 2 + 1 2 u t 1 2 ,

which yields, owing to (2.10) and a proper interpolation inequality (see the proof of Theorem 4.2),

( 5.12 ) d d t ( t u t 1 2 ) + c t u t H p e r 1 ( Ω ) 2 c t ( α 2 + α t 2 + u t 1 2 ) + u t 1 2 , c > 0.

It follows from (3.25), (5.12) and Gronwall's lemma that

( 5.13 ) u t ( t ) 1 2 1 t Q M 1 , M 2 ( u 0 H p e r 2 ( Ω ) , α 0 H p e r 3 ( Ω ) , α 1 H p e r 3 ( Ω ) ) , t ( 0 , T 0 ] .

Next, we multiply (5.11) by u t and obtain, proceeding similarly,

( 5.14 ) d d t u t 1 2 + c u t H p e r 1 ( Ω ) 2 c ( α 2 + α t 2 + u t 1 2 ) , c > 0.

We deduce from (3.25), (5.14) and Gronwall's lemma that

u t ( t ) 1 2 e c t Q M 1 , M 2 ( u 0 H p e r 2 ( Ω ) , α 0 H p e r 3 ( Ω ) , α 1 H p e r 3 ( Ω ) ) u t ( T 0 ) 1 2 , t T 0 ,

hence, owing to (5.13),

( 5.15 ) u t ( t ) 1 2 e c t Q M 1 , M 2 ( u 0 H p e r 2 ( Ω ) , α 0 H p e r 3 ( Ω ) , α 1 H p e r 3 ( Ω ) ) , t T 0 .

We rewrite, for t T 0 fixed, (3.9) as an elliptic equation,

( 5.16 ) A u + f ( u ) f ( u ) = h u ( t ) , u i s Ω p e r i o d i c ,

where

( 5.17 ) h u ( t ) = ( Δ ) 1 u t + α t Δ α t + α 1

satisfies, owing to (3.25) and (5.15),

( 5.18 ) h u ( t ) e c t Q M 1 , M 2 ( u 0 H p e r 2 ( Ω ) , α 0 H p e r 3 ( Ω ) , α 1 H p e r 3 ( Ω ) ) , t T 0 .

Multiplying (5.16) by u , we find, owing to (2.11) and (5.1),

( 5.19 ) A 1 2 u ( t ) 2 + c Ω F ( u ( t ) ) d x c M 1 ( h u ( t ) 2 + 1 ) , c > 0 , t T 0 .

Multiplying then (5.16) by A u , we have, owing to (2.10),

( 5.20 ) A u ( t ) 2 c ( A 1 2 u ( t ) 2 + h u ( t ) 2 ) , t T 0 .

Combining (5.19) and (5.20), we finally obtain, owing to (3.25) and (5.18),

( 5.21 ) u ( t ) H p e r 2 ( Ω ) 2 e c t Q M 1 , M 2 ( u 0 H p e r 2 ( Ω ) , α 0 H p e r 3 ( Ω ) , α 1 H p e r 3 ( Ω ) ) , t T 0 ,

hence, owing to (5.10),

( 5.22 ) u ( t ) H p e r 2 ( Ω ) 2 e c t Q M 1 , M 2 ( u 0 H p e r 2 ( Ω ) , α 0 H p e r 3 ( Ω ) , α 1 H p e r 3 ( Ω ) ) , t 0.

We now come back to (5.3), from which it follows that

( 5.23 ) d d t ( Δ α 2 + Δ α 2 + α t Δ α t 2 ) u t 2 .

Noting that it follows from (3.25), (5.14) and (5.15) that

( 5.24 ) T 0 t u t 2 d τ e c t Q M 1 , M 2 ( u 0 H p e r 2 ( Ω ) , α 0 H p e r 3 ( Ω ) , α 1 H p e r 3 ( Ω ) ) , t T 0 ,

we deduce from (3.14), (5.23) and (5.24) that

Δ α ( t ) 2 + Δ α ( t ) 2 + ( α t Δ α t ) ( t ) 2 e c t Q M 1 , M 2 ( u 0 H p e r 2 ( Ω ) , α 0 H p e r 3 ( Ω ) , α 1 H p e r 3 ( Ω ) ) + Δ α ( T 0 ) 2 + Δ α ( T 0 ) 2 + ( α t Δ α t ) ( T 0 ) 2 , t T 0 ,

hence, owing to (3.8), (3.25), (5.10) and (5.22),

( 5.25 ) u ( t ) H p e r 2 ( Ω ) 2 + α ( t ) H p e r 3 ( Ω ) 2 + α t ( t ) H p e r 3 ( Ω ) 2 e c t Q M 1 , M 2 ( u 0 H p e r 2 ( Ω ) , α 0 H p e r 3 ( Ω ) , α 1 H p e r 3 ( Ω ) ) , t 0 ,

which finishes the proof of the theorem.

ACKNOWLEDGEMENTS

The author is thankful to Alain Miranville for helpful discussions. He also wishes to thank an anonymous referee for her/his careful reading of the paper and useful comments.

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References

23 Cites in Article
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  2. S Agmon,A Douglis,L Nirenberg (1959). Estimates near the boundary for solutions of elliptic partial differential equations satisfying general boundary conditions. I.
  3. G Caginalp (1988). Conserved-phase field system: Implications for kinetic undercooling.
  4. Gunduz Caginalp (1986). An analysis of a phase field model of a free boundary.
  5. Giambattista Giacomin,Joel Lebowitz (1997). Phase segregation dynamics in particle systems with long range interactions. I. Macroscopic limits.
  6. Laurence Cherfils,Alain Miranville,Shuiran Peng,Wen Zhang (2017). Higher-order generalized Cahn–Hilliard equations.
  7. Laurence Cherfils,Alain Miranville,Shuiran Peng (2017). Higher-order anisotropic models in phase separation.
  8. Laurence Cherfils,Alain Miranville,Shuiran Peng (2016). Higher-Order Allen–Cahn Models with Logarithmic Nonlinear Terms.
  9. Alain Miranville (2016). Higher-Order Anisotropic Caginalp Phase-Field Systems.
  10. A Miranville,A Ntsokongo (2018). On the anisotropic Caginalp phase-field type models with singular nonlinear terms.
  11. Alain Miranville,Ramon Quintanilla (2016). A Caginalp phase-field system based on type III heat conduction with two temperatures.
  12. Alain Miranville,Alain Piétrus (2006). A new formulation of the Cahn–Hilliard equation.
  13. A Ntsokongo (2017). On higher-order anisotropic Caginalp phase-field systems with polynomial nonlinear terms.
  14. A Makki,A Miranville (2016). Existence of solutions for anisotropic Cahn-Hilliard and Allen-Cahn systems in higher space dimensions.
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Funding

No external funding was declared for this work.

Conflict of Interest

The authors declare no conflict of interest.

Ethical Approval

No ethics committee approval was required for this article type.

Data Availability

Not applicable for this article.

How to Cite This Article

Cyr Séraphin Ngamouyih Moussata, Armel Judice Ntsokongo, Dieudonné Ampini. 2026. "On Anisotropic Conservative Caginalp Phase-Field System Based on Type III Heat Conduction with Two Temperatures and Periodic Boundary Conditions". Global Journal of Science Frontier Research - F: Mathematics & Decision GJSFR-F Volume 23 (GJSFR Volume 23 Issue F8).

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On Anisotropic Conservative Caginalp Phase-Field System Based on Type III Heat Conduction with Two Temperatures and Periodic Boundary Conditions

Cyr Moussata
Cyr Moussata
Armel Ntsokongo
Armel Ntsokongo
Dieudonné Ampini
Dieudonné Ampini