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Article

Well-Posedness and Stability Results for Lord Shulman Swelling Porous Thermo-Elastic Soils with Microtemperature and Distributed Delay

1
Department of Material Sciences, Faculty of Sciences, Amar Teledji Laghouat University, Laghouat 03000, Algeria
2
Department of Mathematics, College of Sciences and Arts in ArRass, Qassim University, Buraydah 51452, Saudi Arabia
3
Institute of Energy Infrastructure (IEI), Department of Civil Engineering, College of Engineering, Universiti Tenaga Nasional (UNITEN), Putrajaya Campus, Jalan IKRAM-UNITEN, Kajang 43000, Selangor, Malaysia
4
Department of Mathematics and Statistics, Imam Mohammad Ibn Saud Islamic University (IMSIU), Riyadh 11564, Saudi Arabia
*
Author to whom correspondence should be addressed.
Mathematics 2023, 11(23), 4785; https://doi.org/10.3390/math11234785
Submission received: 23 October 2023 / Revised: 14 November 2023 / Accepted: 23 November 2023 / Published: 27 November 2023

Abstract

:
The Lord Shulman swelling porous thermo-elastic soil system with the effects of microtemperature, temperatures and distributed delay terms is considered in this study. The well-posedness result is established by the Lumer–Phillips corollary applied to the Hille–Yosida theorem. The exponential stability result is proven by the energy method under suitable assumptions.

1. Introduction and Preliminaries

The first theory that included a viscous liquid, solid and gas mixture was proposed by Eringen [1]. The field equations were obtained by investigating this heat-resistant combination [2]. The porous media theory, which investigates this type of issue, has also been used to classify expansive (swelling) soils. Due to numerous investigations aimed at mitigating the adverse effects of expansive soils, especially within the fields of architecture and civil engineering, this subject appears promising for further research exploration. For additional information, visit [3,4,5,6,7,8,9]. From the linear theory of swelling porous elastic soils, the fundamental field equations are
ρ u u t t = P 1 x + G 1 + H 1 , ρ ϑ ϑ t t = P 2 x + G 2 + H 2 ,
in which ρ ϑ , ρ u > 0 are the densities of the elastic solid material and fluid, while their respective displacements are denoted by u , ϑ . Furthermore, ( P 1 , G 1 , H 1 ) represent the partial tension, internal forces of body and eternal forces acting on the displacement. ( P 2 , G 2 , H 2 ) are similar, but applied to the elastic solid. Also, the constitutive equations for partial tensions are provided by
P 1 P 2 = a 1 , a 2 a 2 , a 3 A . u x ϑ x ,
where a 1 , a 3 > 0 , and a 2 0 is a real number. A is matrix positive definite with a 1 a 3 > a 2 2 .
Quintanilla [9] studied (1) by considering
G 1 = G 2 = ξ ( u t ϑ t ) , H 1 = a 3 u x x t , H 2 = 0 ,
where ξ > 0 ; the exponential stability can be achieved. Also, in [10], the researchers considered (1) by taking different conditions:
G 1 = G 2 = 0 , H 1 = ρ u γ ( x ) u t , H 2 = 0 ,
where the internal viscous damping function γ ( x ) has a positive mean. They were able to determine the exponential stability using the spectral approach. To discover more, read [9,10,11,12,13,14,15,16]. Time delays are of significant importance in the majority of natural phenomena and industrial systems, as they have the potential to induce instability and should be treated with utmost consideration. Additionally, there are numerous works that have examined this category of issues, including [17,18,19,20,21,22,23].
Numerous researchers worked on similar problems in the literature from different perspectives [24,25,26,27,28]. In recent times, there has been a substantial surge of interest among scientists in Lord Shulman’s thermo-elasticity, leading to an extensive collection of contributions aimed at elucidating this theory. This theoretical framework encompasses the examination of a system comprising four hyperbolic equations coupled with heat transfer dynamics. Moreover, Lord Shulman thermo-elastic theory was introduced to usher in a more robust heat conduction law, as it concerns thermo-elastic materials exhibiting elastic vibrations. Notably, the heat equation within this context is itself hyperbolic and parallels the equation initially formulated by Fourier’s law. To delve deeper into the specifics and gain a comprehensive understanding of this theory, it is recommended that the reader consult the following papers: [29,30]. The core evolutionary equations governing one-dimensional models of porous thermo-elasticity, incorporating both microtemperature and temperature effects [31,32,33,34], can be expressed as follows:
ρ u u t t = T x , ρ φ ϑ t t = H x + G , ρ T 0 η t = q x , ρ E t = P x * + q Q .
In the context provided, the symbols T, T 0 , H , E, η , q, G, Q and P * denote the stress, reference temperature, equilibrated stress, first energy moment, entropy, heat flux vector, equilibrated body force, mean heat flux and first heat flux moment, respectively. For simplicity in computations, we set T 0 to be equal to 1.
This paper addresses the inherent counterpart of microtemperatures within the Lord Shulman theory. In this scenario, it becomes possible to adapt the constitutive equations in the subsequent manner:
T = P 1 + G 1 + H 1 P * = k 2 x , H = P 2 + P 3 ρ η = γ 0 u x + γ 1 ϑ + β 1 ( κ θ t + θ ) , G = G 2 + H 2 Q = ( k 1 k 3 ) + ( k k 1 ) θ x , q = k θ x + k 1 ρ E = β 2 ( κ t + ) γ 2 ϑ x ,
in which the microtemperature vector is indicated by , κ > 0 is the relaxation parameter and ρ u , ρ ϑ , a 1 , a 2 , a 3 , β 1 , β 2 > 0 . The coefficients γ 0 , k , γ 1 denote the coupling between the temperature and displacement, the thermal conductivity, the coupling between the volume fraction and the temperature, respectively.
Taking a 2 0 and the coefficients k 1 , k 2 , k 3 , γ 2 > 0 satisfies the inequalities
a = a 3 a 2 2 a 1 > 0 ,
k 1 2 < k k 3 .
In the current work, we focus on the thermal effects, which is why we make the assumption β 1 , β 2 > 0 for heat capicity. To add interest to the problem, we also add a distributed delay term to the second equation, creating a new case that differs from earlier research. Under the right assumptions, the system is shown to be well posed, and we use the energy method to demonstrate the result of the exponential stability.
In this work, the following are taken into account:
G 1 = G 2 = 0 , P 3 = γ 2 ( κ t + ) , H 1 = γ 0 ( κ θ t + θ ) , H 2 = γ 1 ( κ θ t + θ ) ϖ 1 ϑ t ν 1 ν 2 ϖ 2 ( s ) ϑ t x , t s d s .
By substituting (4)–(7) into (3), we have
ρ u u t t a 1 u x x a 2 ϑ x x + γ 0 ( κ θ t + θ ) x = 0 , ρ ϑ ϑ t t a 3 ϑ x x a 2 u x x γ 1 ( κ θ t + θ ) + γ 2 ( κ t + ) x + ϖ 1 ϑ t + ν 1 ν 2 ϖ 2 ( s ) ϑ t x , t s d s = 0 , β 1 ( κ θ t + θ ) t + γ 0 u t x + γ 1 ϑ t k θ x x k 1 x = 0 , β 2 ( κ t + ) t k 2 x x + γ 2 ϑ t x + k 3 + k 1 θ x = 0 ,
where
( x , s , t ) H = ( 0 , 1 ) × ( ν 1 , ν 2 ) × ( 0 , ) ,
and
u x , 0 = u 0 x , u t x , 0 = u 1 x , θ ( x , 0 ) = θ 0 ( x ) , ϑ x , 0 = ϑ 0 x , ϑ t x , 0 = ϑ 1 x , θ t ( x , 0 ) = θ 1 ( x ) , x , 0 = 0 x , t x , 0 = 1 x , x 0 , 1 , u 0 , t = u 1 , t = ϑ 0 , t = ϑ 1 , t = 0 , 0 t , ϑ t ( x , t ) = f 0 ( x , t ) , ( x , t ) ( 0 , 1 ) × ( 0 , ν 2 ) , θ 0 , t = θ 1 , t = 0 , t = 1 , t = 0 , 0 t .
Next, we introduce a new variable, as mentioned in [23]:
Y ( x , ρ , s , t ) = ϑ t ( x , t s ρ ) ,
thus, the following is obtained:
s Y t ( x , ρ , s , t ) + Y ρ ( x , ρ , s , t ) = 0 , Y ( x , 0 , s , t ) = ϑ t ( x , t ) .
Our problem can be expressed in the following form:
ρ u u t t a 1 u x x a 2 ϑ x x + γ 0 ( κ θ t + θ ) x = 0 , ρ ϑ ϑ t t a 3 ϑ x x a 2 u x x γ 1 ( κ θ t + θ ) + γ 2 ( κ t + ) x + ϖ 1 ϑ t + ν 1 ν 2 ϖ 2 ( s ) Y x , 1 , s , t d s = 0 , β 1 ( κ θ t + θ ) t + γ 0 u t x + γ 1 ϑ t k θ x x k 1 x = 0 , β 2 ( κ t + ) t k 2 x x + γ 2 ϑ t x + k 3 + k 1 θ x = 0 , s Y t ( x , ρ , s , t ) + Y ρ ( x , ρ , s , t ) = 0 ,
in which
( x , ρ , s , t ) ( 0 , 1 ) × H ,
with
u x , 0 = u 0 x , u t x , 0 = u 1 x , θ ( x , 0 ) = θ 0 ( x ) , ϑ x , 0 = ϑ 0 x , ϑ t x , 0 = ϑ 1 x , θ t ( x , 0 ) = θ 1 ( x ) , x , 0 = 0 x , t x , 0 = 1 x , x 0 , 1 , Y ( x , ρ , s , 0 ) = f 0 ( x , s ρ ) , ( x , ρ , s ) ( 0 , 1 ) × ( 0 , 1 ) × ( 0 , ν 2 ) ,
and
u 0 , t = u 1 , t = ϑ 0 , t = ϑ 1 , t = 0 , θ 0 , t = θ 1 , t = 0 , t = 1 , t = 0 , 0 t .
In this context, the integrals denote the presence of distributed delay components, where ν 1 and ν 2 —both greater than zero—represent time delays. The functions ϖ 1 and ϖ 2 are L functions and must adhere to the following conditions.
Hypothesis 1.
ϖ 2 : [ ν 1 , ν 2 ] R is a bounded function satisfying
ν 1 ν 2 | ϖ 2 ( s ) | d s < ϖ 1 .
In this investigation, we delve into the realm of the Lord Shulman model for swelling porous thermo-elastic soils, incorporating the influence of microtemperature, temperatures and distributed delay components. Our focus lies in demonstrating the system’s well-posedness and examining the outcomes related to its exponential stability. This work is structured as follows: in Section 2, the well-posedness is illustrated, and the exponential stability is demonstrated in Section 3. We state that c > 0 in each of the sentences that follow.

2. Well-Posedness

Here, we will establish the well-posedness of the system (9)–(11). The following vector function is first introduced:
X = ( u , u t , ϑ , ϑ t , θ , θ t , , t , Y ) T ,
where variables v = u t , φ = ϑ t , χ = θ t , Σ = t ; then, the system (9) is written as follows:
X t = T X X ( 0 ) = X 0 = ( u 0 , u 1 , ϑ 0 , ϑ 1 , θ 0 , θ 1 , 0 , 1 , f 0 ) T ,
where T : S ( T ) V : V is a linear operator given by
T X = v 1 ρ u [ a 1 u x x + a 2 ϑ x x γ 0 ( κ χ + θ ) x ] φ 1 ρ ϑ [ a 3 ϑ x x + a 2 u x x + γ 1 ( κ χ + θ ) γ 2 ( κ Σ + ) x ϖ 1 φ ν 1 ν 2 ϖ 2 ( s ) Y ( x , 1 , s , t ) d s ] χ 1 κ β 1 [ γ 0 v x + γ 1 φ k θ x x + β 1 χ k 1 x ] Σ 1 κ β 2 [ k 2 x x + γ 2 φ x + k 3 + k 1 θ x + β 2 Σ ] 1 s Y ρ ,
in which energy space is denoted by V , such that
V = H 0 1 ( 0 , 1 ) × L 2 ( 0 , 1 ) × H 0 1 ( 0 , 1 ) × L 2 ( 0 , 1 ) × H 0 1 ( 0 , 1 ) × L 2 ( 0 , 1 ) × H 0 1 ( 0 , 1 ) × L 2 ( 0 , 1 ) × L 2 ( ( 0 , 1 ) × ( 0 , 1 ) × ( ν 1 , ν 2 ) ) ,
for any
X = ( u , v , ϑ , φ , θ , χ , , Σ , Y ) T V , X ^ = ( u ^ , v ^ , ϑ ^ , φ ^ , θ ^ , χ ^ , ^ , Σ ^ , Y ^ ) T V ,
with the following inner product:
< X , X ^ > V = ρ u 0 1 v v ^ d x + a 1 0 1 u x u ^ x d x + ρ ϑ 0 1 φ φ ^ d x + a 3 0 1 ϑ x ϑ ^ x d x + a 2 0 1 ( u x ϑ ^ x + u ^ x ϑ x ) d x + k 1 κ 0 1 ( θ x ^ + θ ^ x ) d x + β 1 0 1 ( κ χ + θ ) ( κ χ ^ + θ ^ ) d x + β 2 0 1 ( κ Σ + ) ( κ Σ ^ + ^ ) d x + k κ 0 1 θ x θ ^ x d x + k 2 κ 0 1 x ^ x d x + k 3 κ 0 1 ^ d x + 0 1 0 1 ν 1 ν 2 s | ϖ 2 ( s ) | Y Y ^ d s d ρ d x .
The domain of T is given by
S ( T ) = X V / u , ϑ , θ , H 2 ( 0 , 1 ) H 0 1 ( 0 , 1 ) , v , φ , χ , Σ H 0 1 ( 0 , 1 ) , Y , Y ρ L 2 ( ( 0 , 1 ) × ( 0 , 1 ) × ( ν 1 , ν 2 ) ) , Y ( x , 0 , s , t ) = φ .
Clearly, S ( T ) is dense in V .
Theorem 1.
Let X 0 V and consider that (5), (6) and (12) hold. Then, a unique solution X C ( R + , V ) for the problem (13) exists. Additionally, if X 0 S ( T ) , then
X C ( R + , S ( T ) ) C 1 ( R + , V ) .
Proof. 
First, we show that T is a dissipative operator. For any X 0 S ( T ) and by utilizing (15), we achieve
< T X , X > V = ϖ 1 0 1 φ 2 d x 0 1 ν 1 ν 2 ϖ 2 ( s ) φ Y ( x , 1 , s , t ) d s d x k 0 1 θ x 2 d x k 3 0 1 2 d x 2 k 1 0 1 θ x d x k 2 0 1 x 2 d x 0 1 0 1 ν 1 ν 2 | ϖ 2 ( s ) | Y ρ Y d s d ρ d x .
For the last term of the RHS of (16), we have
0 1 0 1 ν 1 ν 2 | ϖ 2 ( s ) | Y ρ Y d s d ρ d x = 1 2 0 1 ν 1 ν 2 0 1 | ϖ 2 ( s ) | d d ρ Y 2 d ρ d s d x = 1 2 0 1 ν 1 ν 2 | ϖ 2 ( s ) | Y 2 ( x , 1 , s , t ) d s d x + 1 2 0 1 ν 1 ν 2 | ϖ 2 ( s ) | Y 2 ( x , 0 , s , t ) d s d x .
Applying the inequality of Young, we have
0 1 ν 1 ν 2 ϖ 2 ( s ) φ Y ( x , 1 , s , t ) d s d x 1 2 ( ν 1 ν 2 | ϖ 2 ( s ) | d s ) 0 1 φ 2 d x + 1 2 0 1 ν 1 ν 2 | ϖ 2 ( s ) | Y 2 ( x , 1 , s , t ) d s d x .
Substituting (17) and (18) into (16) and utilizing Y ( x , 0 , s , t ) = φ ( x , t ) and (12), the following is obtained:
< T X , X > V k 0 1 θ x 2 d x k 3 0 1 2 d x 2 k 1 0 1 θ x d x η 0 0 1 φ 2 d x k 2 0 1 x 2 d x ,
where η 0 = ( ϖ 1 ν 1 ν 2 | ϖ 2 ( s ) | d s ) > 0 . Additionally, by (6), we have
k θ x 2 k 3 2 2 k 1 θ x < 0 .
Therefore, the operator T is dissipative. Now, we show that the operator T is a maximal. It is enough to prove that ( λ I T ) is a surjective operator. In fact, we demonstrate that a unique X = ( u , v , ϑ , φ , θ , χ , , Σ , Y ) T S ( T ) exists for any F = ( f 1 , f 2 , f 3 , f 4 , f 5 , f 6 , f 7 , f 8 , f 9 ) T V , such that
( λ I T ) X = F .
That is,
λ u v = f 1 H 0 1 ( 0 , 1 ) ρ u λ v a 1 u x x a 2 ϑ x x + γ 0 ( κ χ + θ ) x = ρ u f 2 L 2 ( 0 , 1 ) λ ϑ φ = f 3 H 0 1 ( 0 , 1 ) ρ ϑ λ φ a 3 ϑ x x a 2 u x x γ 1 ( κ χ + θ ) + γ 2 ( κ Σ + ) x + ϖ 1 φ + ν 1 ν 2 ϖ 2 ( s ) Y ( x , 1 , s , t ) d s = ρ ϑ f 4 L 2 λ θ χ = f 5 H 0 1 ( 0 , 1 ) β 1 κ λ χ + γ 0 v x + γ 1 φ k θ x x k 1 x + β 1 χ = β 1 κ f 6 L 2 ( 0 , 1 ) λ Σ = f 7 H 0 1 ( 0 , 1 ) β 2 κ λ Σ k 2 x x + γ 2 φ x + k 3 + k 1 θ x + β 2 Σ = β 2 κ f 8 L 2 ( 0 , 1 ) s λ Y t ( x , ρ , s , t ) + Y ρ ( x , ρ , s , t ) = s f 9 L 2 ( ( 0 , 1 ) × ( 0 , 1 ) × ( ν 1 , ν 2 ) ) .
It can be noticed that there exists a unique solution of (22)9 with Y ( x , 0 , s , t ) = φ ( x , t ) , which is given by
Y ( x , ρ , s , t ) = e λ ρ s φ + s e s ρ λ 0 ρ e λ s ϱ f 9 ( x , ϱ , s , t ) d ϱ ,
then,
Y ( x , 1 , s , t ) = e λ s φ + s e λ s 0 1 e λ s ϱ f 9 ( x , ϱ , s , t ) d ϱ ,
thus, we obtain
v = λ u f 1 , φ = λ ϑ f 3 , χ = λ θ f 5 , Σ = λ f 7 .
Inserting (24) and (25) into (22)2, (22)4, (22)6 and (22)8, we obtain
ρ u λ 2 u a 1 u x x a 2 ϑ x x + γ 0 ( κ λ + 1 ) θ x = h 1 ϖ 3 ϑ a 3 ϑ x x a 2 u x x γ 1 ( κ λ + 1 ) θ + γ 2 ( κ λ + 1 ) x = h 2 ϖ 4 θ + γ 0 λ u x + γ 1 λ ϑ k θ x x k 1 x = h 3 ϖ 5 k 2 x x + γ 2 λ ϑ x + k 1 θ x = h 4 ,
where
h 1 = ρ u ( λ f 1 + f 2 ) + γ 0 κ f 5 x , h 2 = ρ ϑ f 4 + ( ρ ϑ λ + ϖ 1 + ν 1 ν 2 | ϖ 2 ( s ) | e s λ d s ) f 3 γ 1 κ f 5 + γ 2 κ f 7 x , ν 1 ν 2 s | ϖ 2 ( s ) | e s λ 0 1 e λ s ϱ f 9 ( x , ϱ , s , t ) d ϱ d s , h 3 = κ β 1 f 6 + γ 0 f 1 x + γ 1 f 3 + β 1 ( 1 + κ λ ) f 5 , h 4 = κ β 2 f 8 + γ 2 f 3 x + β 2 ( 1 + κ λ ) f 7 , ϖ 3 = ρ ϑ λ 2 + ϖ 1 λ + λ ν 1 ν 2 | ϖ 2 ( s ) | e λ s d s , ϖ 4 = β 1 λ ( κ λ + 1 ) , ϖ 5 = β 2 λ ( κ λ + 1 ) + k 3 .
Multiplying (26) by u ^ , ϑ ^ , θ ^ , ^ , and integrating the sum over ( 0 , 1 ) , we have
B ( ( u , ϑ , θ , ) , ( u ^ , ϑ ^ , θ ^ , ^ ) ) = Γ ( u ^ , ϑ ^ , θ ^ , ^ ) ,
where
B : ( H 0 1 ( 0 , 1 ) × H 0 1 ( 0 , 1 ) × H 0 1 ( 0 , 1 ) × H 0 1 ( 0 , 1 ) ) 2 R ,
is the bilinear form given by
B ( ( u , ϑ , θ , ) , ( u ^ , ϑ ^ , θ ^ , ^ ) ) = ρ u λ 2 0 1 u u ^ d x + a 1 0 1 u x u ^ x d x + a 2 0 1 ϑ x u ^ x d x + γ 0 ( κ λ + 1 ) 0 1 θ x u ^ d x + ϖ 3 0 1 ϑ ϑ ^ d x + a 3 0 1 ϑ x ϑ ^ x d x + a 2 0 1 u x ϑ ^ x d x γ 1 ( κ λ + 1 ) 0 1 θ ϑ ^ d x + k 1 ( κ λ + 1 ) λ 0 1 x θ ^ d x + γ 2 ( κ λ + 1 ) 0 1 x ϑ ^ d x + ϖ 4 ( κ λ + 1 ) λ 0 1 θ θ ^ d x + γ 0 ( κ λ + 1 ) 0 1 u x θ ^ d x + γ 1 ( κ λ + 1 ) 0 1 ϑ θ ^ d x + k ( κ λ + 1 ) λ 0 1 θ x θ ^ x d x , + ϖ 5 ( κ λ + 1 ) λ 0 1 ^ d x + γ 2 ( κ λ + 1 ) 0 1 ϑ x ^ d x + k 1 ( κ λ + 1 ) λ 0 1 θ x ^ d x + k 2 ( κ λ + 1 ) λ 0 1 x ^ x d x ,
and
Γ : ( H 0 1 ( 0 , 1 ) × H 0 1 ( 0 , 1 ) × H 0 1 ( 0 , 1 ) , × H 0 1 ( 0 , 1 ) ) R ,
is the linear functional defined as
Γ ( u ^ , ϑ ^ , θ ^ , ^ ) = 0 1 h 1 u ^ d x + 0 1 h 2 ϑ ^ d x + ( κ λ + 1 ) λ 0 1 h 3 θ ^ d x + ( κ λ + 1 ) λ 0 1 h 4 ^ d x .
Now, for V = H 0 1 ( 0 , 1 ) × H 0 1 ( 0 , 1 ) × H 0 1 ( 0 , 1 ) × H 0 1 ( 0 , 1 ) , with the norm
( u , ϑ , θ , ) V 2 = u 2 2 + u x 2 2 + ϑ 2 2 + ϑ x 2 2 + θ 2 2 + θ x 2 2 + 2 2 + x 2 2 ,
we obtain
B ( ( u , ϑ , θ , ) , ( u , ϑ , θ , ) ) = ρ u λ 2 0 1 u 2 d x + a 1 0 1 u x 2 d x + ϖ 3 0 1 ϑ 2 d x + a 3 0 1 ϑ x 2 d x + ϖ 4 ( κ λ + 1 ) λ 0 1 θ 2 d x + 2 a 2 0 1 u x ϑ x d x + k ( κ λ + 1 ) λ 0 1 θ x 2 d x + ϖ 5 ( κ λ + 1 ) λ 0 1 2 d x + k 2 ( κ λ + 1 ) λ 0 1 x 2 d x .
Also, we can write
a 1 u x 2 + 2 a 2 u x ϑ x + a 3 ϑ x 2 = 1 2 [ a 1 ( u x + a 2 a 3 ϑ x ) 2 + a 3 ( ϑ x + a 2 a 1 u x ) 2 + u x 2 ( a 1 a 2 2 a 3 ) + ϑ x 2 ( a 3 a 2 2 a 1 ) ] .
Because of (5), we deduce that
a 1 u x 2 + 2 a 2 u x ϑ x + a 3 ϑ x 2 > 1 2 u x 2 ( a 1 a 2 2 a 3 ) + ϑ x 2 ( a 3 a 2 2 a 1 ) ,
then, for some M 0 > 0 ,
B ( ( u , ϑ , θ , ) , ( u , ϑ , θ , ) ) M 0 ( u , ϑ , θ , ) V 2 .
B is, hence, coercive. As a result, we determine that (28) has a unique solution using the Lax–Milgram theorem:
u , ϑ , θ , H 0 1 ( 0 , 1 ) .
Putting u , ϑ , θ , and in (22)1,3,5,7, we have
v , φ , χ , Σ H 0 1 ( 0 , 1 ) .
In the same way, the compensation of φ in (23) with (22)9 implies that
Y , Y ρ L 2 ( ( 0 , 1 ) × ( 0 , 1 ) × ( ν 1 , ν 2 ) ) .
Additionally, if we assume u ^ = θ ^ = ^ = 0 in (29), we obtain
a 3 0 1 ϑ x ϑ ^ x d x + ϖ 3 0 1 ϑ ϑ ^ d x + a 2 0 1 u x ϑ ^ x d x γ 1 ( κ λ + 1 ) 0 1 θ ϑ ^ d x + γ 2 ( κ λ + 1 ) 0 1 x ϑ ^ d x = 0 1 h 2 ϑ ^ d x , ϑ ^ H 0 1 ( 0 , 1 ) ,
which implies
a 3 0 1 ϑ x ϑ ^ x d x = 0 1 h 2 ϖ 3 ϑ + a 2 u x x + ( κ λ + 1 ) ( γ 1 θ γ 2 x ) ϑ ^ d x , ϑ ^ H 0 1 ,
that is,
a 3 ϑ x x + a 2 u x x = ϖ 3 ϑ ( κ λ + 1 ) ( γ 1 θ γ 2 x ) h 2 L 2 ( 0 , 1 ) .
Similarly, if we take ϑ ^ = θ ^ = ^ = 0 in (29), we obtain
a 2 ϑ x x + a 1 u x x = ρ u λ 2 u + γ 0 ( κ λ + 1 ) θ x h 1 L 2 ( 0 , 1 ) .
Combining (35) and (36), and by using (5), we achieve that
u , ϑ H 2 ( 0 , 1 ) H 0 1 ( 0 , 1 ) .
In the same way, if we let u ^ = ϑ ^ = ^ = 0 in (29), we obtain
ϖ 4 ( κ λ + 1 ) λ 0 1 θ θ ^ d x + k ( κ λ + 1 ) λ 0 1 θ x θ ^ x d x + γ 0 ( κ λ + 1 ) 0 1 u x θ ^ d x + γ 1 ( κ λ + 1 ) 0 1 ϑ θ ^ d x + k 1 ( κ λ + 1 ) λ 0 1 x θ ^ d x = ( κ λ + 1 ) λ 0 1 h 3 θ ^ d x , θ ^ H 0 1 ,
which implies
k θ x x = ϖ 4 θ + γ 0 λ u x + γ 1 λ ϑ + k 1 x h 3 L 2 ( 0 , 1 ) .
Consequently,
θ H 2 ( 0 , 1 ) H 0 1 ( 0 , 1 ) .
In a similar way, if we take ϑ ^ = θ ^ = u ^ = 0 in (29), we find
k 2 x x = ϖ 5 + γ 2 ϑ x + k 1 θ x h 4 L 2 ( 0 , 1 ) .
Hence,
H 2 ( 0 , 1 ) H 0 1 ( 0 , 1 ) .
Ultimately, leveraging the principles of regularity theory for linear elliptic equations guarantees the presence of a singular X S ( T ) , which satisfies Equation (21) uniquely. In light of this, we deduce that T is a maximal dissipative operator. The well-posedness finding is obtained as a result of the Lumer–Philips theorem [35]. □

3. Exponential Decay

In this part, we demonstrate the system (9)–(11) stability result.
The following lemmas apply to this.
Lemma 1.
The energy functional E, defined as
E t = 1 2 0 1 ρ u u t 2 + a 1 u x 2 + ρ ϑ ϑ t 2 + a 3 ϑ x 2 + 2 a 2 u x ϑ x + β 1 ( κ θ t + θ ) 2 d x + 1 2 0 1 β 2 ( κ t + ) 2 + k 2 κ x 2 + k 3 κ 2 + k κ θ x 2 + 2 k 1 κ θ x d x + 1 2 0 1 0 1 ν 1 ν 2 s | ϖ 2 ( s ) | Y 2 x , ρ , s , t d s d ρ d x ,
satisfies
E t k 4 0 1 θ x 2 d x k 2 0 1 x 2 d x k 5 0 1 2 d x η 0 0 1 ϑ t 2 d x 0 ,
where  η 0 = ϖ 1 ν 1 ν 2 | ϖ 2 ( s ) | d s > 0 , k 4 = 1 2 ( k k 1 2 k 3 ) > 0 , k 5 = 1 2 ( k 3 k 1 2 k ) > 0 .
Proof. 
First, we multiply Equation (9)1,2,3,4 by u t , ϑ t , ( κ θ t + θ ) and ( κ t + ) . In addition to this, applying (11), we have the following:
1 2 d d t 0 1 ρ u u t 2 + a 1 u x 2 + ρ ϑ ϑ t 2 + a 3 ϑ x 2 + 2 a 2 u x ϑ x + β 1 ( κ θ t + θ ) 2 d x 1 2 d d t 0 1 β 2 ( κ t + ) 2 + k 2 κ x 2 + k 3 κ 2 + k κ θ x 2 + 2 k 1 κ θ x d x + ϖ 1 0 1 ϑ t 2 d x + 0 1 ϑ t ν 1 ν 2 ϖ 2 ( s ) Y x , 1 , s , t d s d x + k 0 1 θ x 2 d x + k 3 0 1 2 d x + k 2 0 1 x 2 d x + 2 k 1 0 1 θ x d x = 0 .
Next, multiplying (9)5 by Y | ϖ 2 ( s ) | and integrating, we have
d d t 1 2 0 1 0 1 ν 1 ν 2 s | ϖ 2 ( s ) | Y 2 ( x , ρ , s , t ) d s d ρ d x = 0 1 0 1 ν 1 ν 2 | ϖ 2 ( s ) | Y Y ρ x , ρ , s , t d s d ρ d x = 1 2 0 1 0 1 ν 1 ν 2 | ϖ 2 ( s ) | d d ρ Y 2 x , ρ , s , t d s d ρ d x = 1 2 0 1 ν 1 ν 2 | ϖ 2 ( s ) | ( Y 2 x , 0 , s , t Y 2 ( x , 1 , s , t ) ) d s d x = 1 2 ν 1 ν 2 | ϖ 2 ( s ) | d s 0 1 ϑ t 2 d x 1 2 0 1 ν 1 ν 2 | ϖ 2 ( s ) | Y 2 x , 1 , s , t d s d x .
Putting (41) into (40) and utilizing Young’s inequality, the following is obtained:
E ( t ) k 0 1 θ x 2 d x k 3 0 1 2 d x k 2 0 1 x 2 d x 2 k 1 0 1 θ x d x ϖ 1 ν 1 ν 2 | ϖ 2 ( s ) | d s 0 1 ϑ t 2 d x ,
and we have the following inequality:
k θ x 2 + k 3 2 + 2 k 1 θ x > 1 2 θ x 2 ( k k 1 2 k 3 ) + 2 ( k 3 k 1 2 k ) .
By (6), we obtain
k θ x 2 + k 3 2 + 2 k 1 θ x > k 4 θ x 2 + k 5 2 ,
where
k 4 = 1 2 ( k k 1 2 k 3 ) > 0 , k 5 = 1 2 ( k 3 k 1 2 k ) > 0 ;
then, by (12), η 0 = ϖ 1 ν 1 ν 2 | ϖ 2 ( s ) | d s > 0 , so that
E ( t ) k 4 0 1 θ x 2 d x k 5 0 1 2 d x k 2 0 1 x 2 d x η 0 0 1 ϑ t 2 d x .
Thus, we achieve (39) (E is a non-increasing function). □
Remark 1.
Using (5), (6) and (32), we deduce that E ( t ) fulfills
E t > 1 2 0 1 ρ u u t 2 + a 4 u x 2 + ρ ϑ ϑ t 2 + a 5 ϑ x 2 + β 1 ( κ θ t + θ ) 2 d x + 1 2 0 1 β 2 ( κ t + ) 2 + k 2 κ x 2 + k 4 κ θ x 2 + k 5 κ 2 d x + 1 2 0 1 0 1 ν 1 ν 2 s | ϖ 2 ( s ) | Y 2 x , ρ , s , t d s d ρ d x ,
where
a 4 = 1 2 a 1 a 2 2 a 3 > 0 , a 5 = 1 2 a 3 a 2 2 a 1 > 0 .
Thus, the non-negativity of the function E ( t ) is obtained.
Lemma 2.
The functional
D 1 t : = ρ ϑ 0 1 ϑ t ϑ d x a 2 a 1 ρ u 0 1 ϑ u t d x + ϖ 1 2 0 1 ϑ 2 d x ,
satisfies, for any ε 1 > 0 ,
D 1 t a 2 0 1 ϑ x 2 d x + ε 1 0 1 u t 2 d x + c ( 1 + 1 ε 1 ) 0 1 ϑ t 2 d x + c 0 1 ( κ θ t + θ ) 2 d x + c 0 1 ( κ t + ) 2 d x + c 0 1 ν 1 ν 2 | ϖ 2 ( s ) | Y 2 x , 1 , s , t d s d x .
Proof. 
Via direct calculation, utilizing integration by parts, we obtain that
D 1 t = a 3 0 1 ϑ x 2 d x + ρ ϑ 0 1 ϑ t 2 d x + a 2 2 a 1 0 1 ϑ x 2 d x a 2 a 1 ρ u 0 1 ϑ t u t d x + γ 1 0 1 ( κ θ t + θ ) ϑ d x + a 2 γ 0 a 1 0 1 ( κ θ t + θ ) x ϑ d x γ 2 0 1 ( κ t + ) x ϑ d x 0 1 ϑ ν 1 ν 2 ϖ 2 ( s ) Y ( x , 1 , s , t ) d s d x = a 3 a 2 2 a 1 0 1 ϑ x 2 d x + ρ ϑ 0 1 ϑ t 2 d x a 2 a 1 ρ u 0 1 ϑ t u t d x + γ 1 0 1 ( κ θ t + θ ) ϑ d x a 2 γ 0 a 1 0 1 ( κ θ t + θ ) ϑ x d x + γ 2 0 1 ( κ t + ) ϑ x d x 0 1 ϑ ν 1 ν 2 ϖ 2 ( s ) Y ( x , 1 , s , t ) d s d x .
Using Poincaré’s and Young’s inequalities, for δ 1 , δ 2 , δ 3 , ε 1 > 0 , we obtain that
D 1 t ( a 3 a 2 2 a 1 ) ( ϖ 1 c δ 1 + c δ 2 + 2 δ 3 ) 0 1 ϑ x 2 d x + ε 1 0 1 u t 2 d x + c ( 1 + 1 ε 1 ) 0 1 ϑ t 2 d x + ( c δ 2 + c δ 3 ) 0 1 ( κ θ t + θ ) 2 d x + c δ 3 0 1 ( κ t + ) 2 d x + c δ 1 0 t ν 1 ν 2 | ϖ 2 ( s ) | Y 2 ( x , 1 , s , t ) d s d x .
Bearing in mind (5) and letting δ 1 = a 6 ϖ 1 c , δ 2 = a 6 c , δ 3 = a 12 , we obtain estimate (47). □
Lemma 3.
The functional
D 2 t : = a 2 0 1 ϑ t u d x 0 1 ϑ u t d x ,
satisfies,
D 2 t a 2 2 2 ρ ϑ 0 1 u x 2 d x + c 0 1 ϑ x 2 d x + c 0 1 ϑ t 2 d x + c 0 1 ( κ θ t + θ ) 2 d x + c 0 1 ( κ t + ) 2 d x + c 0 1 ν 1 ν 2 | ϖ 2 ( s ) | Y 2 ( x , 1 , s , t ) d s d x .
Proof. 
By differentiating D 2 , then utilizing (9), integration by parts and (11), we obtain
D 2 t = a 2 2 ρ ϑ 0 1 u x 2 d x + a 2 2 ρ u 0 1 ϑ x 2 d x a 2 a 3 ρ ϑ a 1 a 2 ρ u 0 1 ϑ x u x d x a 2 γ 0 ρ u 0 1 ( κ θ t + θ ) ϑ x d x + a 2 γ 1 ρ ϑ 0 1 ( κ θ t + θ ) u d x + a 2 γ 2 ρ ϑ 0 1 ( κ t + ) u x d x a 2 ϖ 1 ρ ϑ 0 1 u ϑ t d x a 2 ρ ϑ 0 1 u ν 1 ν 2 ϖ 2 ( s ) Y ( x , 1 , s , t ) d s d x .
We now evaluate the final six terms in the right hand side of (51), utilizing Poincaré’s and Young’s inequalities. For δ 4 , δ 5 > 0 , we have
a 2 a 3 ρ ϑ a 1 a 2 ρ u 0 1 ϑ x u x d x δ 4 0 1 u x 2 d x + c δ 4 0 1 ϑ 2 d x ,
a 2 ϖ 1 ρ ϑ 0 1 u ϑ t d x c δ 5 0 1 u x 2 d x + c δ 5 0 1 ϑ t 2 d x ,
a 2 γ 1 ρ ϑ 0 1 ( κ θ t + θ ) u d x c δ 5 0 1 u x 2 d x + c δ 5 0 1 ( κ θ t + θ ) 2 d x ,
a 2 γ 2 ρ ϑ 0 1 ( κ t + ) u x d x δ 4 0 1 u x 2 d x + c δ 4 0 1 ( κ t + ) 2 d x ,
and
a 2 ρ ϑ 0 1 u ν 1 ν 2 ϖ 2 ( s ) Y ( x , 1 , s , t ) d s d x c δ 5 0 1 u x 2 d x + c δ 5 0 1 ν 1 ν 2 | ϖ 2 ( s ) | Y 2 ( x , 1 , s , t ) d s d x .
By letting δ 4 = a 2 8 ρ ϑ , δ 5 = a 2 12 c ρ ϑ and putting these into (51), we obtain (50). □
Lemma 4.
The functional
D 3 t : = ρ u 0 1 u t u d x ,
satisfies
D 3 t ρ u 0 1 u t 2 d x + 3 a 1 0 1 u x 2 d x + a 3 4 0 1 ϑ x 2 d x + γ 0 2 4 a 1 0 1 ( κ θ t + θ ) 2 d x .
Proof. 
Direct computations give
D 3 t = ρ u 0 1 u t 2 d x + a 1 0 1 u x 2 d x + a 2 0 1 u x ϑ x d x γ 0 0 1 u x ( κ θ t + θ ) d x .
Estimate (52) easily follows by utilizing Young’s inequality. □
Lemma 5.
The functional
D 4 t : = β 1 κ 2 0 1 θ t θ d x β 1 κ 2 0 1 θ 2 d x β 2 κ 2 0 1 t d x β 2 κ 2 0 1 2 d x ,
satisfies, for any ε 2 > 0 ,
D 4 t β 1 2 0 1 ( κ θ t + θ ) 2 d x β 2 2 0 1 ( κ t + ) 2 d x + ε 2 0 1 u t 2 d x + c 0 1 ϑ t 2 d x + c ( 1 + 1 ε 2 ) 0 1 θ x 2 d x + c 0 1 x 2 d x + c 0 1 2 d x .
Proof. 
Direct computations give
D 4 t = β 1 κ 0 1 ( κ θ t + θ ) t θ d x β 1 κ 2 0 1 θ t 2 d x β 2 κ 0 1 ( κ t + ) t d x β 2 κ 2 0 1 t 2 d x = γ 0 κ 0 1 θ u t x d x + γ 1 κ 0 1 ϑ t θ d x + k κ 0 1 θ x 2 d x β 1 κ 2 0 1 θ t 2 d x + 2 k 1 κ 0 1 θ x d x + k 2 κ 0 1 x 2 d x + k 3 κ 0 1 2 d x γ 2 κ 0 1 ϑ t x d x β 2 κ 2 0 1 t 2 d x .
Further simplification of (53) leads us to
0 1 ( κ θ t ) 2 d x 1 2 0 1 ( κ θ t + θ ) 2 d x + 0 1 θ 2 d x , 0 1 ( κ t ) 2 d x 1 2 0 1 ( κ t + ) 2 d x + 0 1 2 d x .
 □
Now, we introduce a functional stated in Lemma 6.
Lemma 6.
The functional
D 5 t : = 0 1 0 1 ν 1 ν 2 s e s ρ | ϖ 2 ( s ) | Y 2 x , ρ , s , t d s d ρ d x ,
satisfies
D 5 t η 1 0 1 0 1 ν 1 ν 2 s | ϖ 2 ( s ) | Y 2 x , ρ , s , t d s d ρ d x + ϖ 1 0 1 ϑ t 2 d x η 1 0 1 ν 1 ν 2 | ϖ 2 ( s ) | Y 2 x , 1 , s , t d s d x ,
where η 1 > 0 .
Proof. 
By differentiating D 5 with respect to t and utilizing the last equation in (9), we obtain
D 5 t = 2 0 1 0 1 ν 1 ν 2 e s ρ | ϖ 2 ( s ) | Y Y ρ x , ρ , s , t d s d ρ d x = 0 1 0 1 ν 1 ν 2 s e s ρ | ϖ 2 ( s ) | Y 2 x , ρ , s , t d s d ρ d x 0 1 ν 1 ν 2 | ϖ 2 ( s ) | [ e s Y 2 x , 1 , s , t Y 2 x , 0 , s , t ] d s d x .
Utilizing that Y ( x , 0 , s , t ) = ϑ t ( x , t ) and e s e s ρ 1 , ∀ 0 < ρ < 1 , we achieve that
D 5 t 0 1 0 1 ν 1 ν 2 s e s | ϖ 2 ( s ) | Y 2 x , ρ , s , t d s d ρ d x 0 1 ν 1 ν 2 e s | ϖ 2 ( s ) | Y 2 x , 1 , s , t d s d x + ( ν 1 ν 2 | ϖ 2 ( s ) | d s ) 0 1 ϑ t 2 d x .
 □
As e s is an increasing function, we have e s e ν 2 , for all s [ ν 1 , ν 2 ] . By setting η 1 = e ν 2 and remembering (12), we discover (55). We can now proceed to proving the primary finding.
Theorem 2.
Let (5), (6) and (12) hold. Then, there exist ζ 1 , ζ 2 > 0 such that the energy functional provide by (38) holds:
E t ζ 1 e ζ 2 t , t 0 .
Proof. 
To prove the required result, we introduce the Lyapunov functional as follows:
P t : = N E t + N 1 D 1 t + N 2 D 2 t + D 3 t + N 4 D 4 t + N 5 D 5 t ,
where N , N 1 , N 2 , N 4 , N 5 > 0 ; we assign them later.
By differentiating (57) and using (39), (47), (50), (52), (53) and (55), we have
P t a N 1 2 c N 2 a 3 4 0 1 ϑ x 2 d x ρ u ε 1 N 1 ε 2 N 4 0 1 u t 2 d x a 2 2 N 2 2 ρ ϑ 3 a 1 0 1 u x 2 d x k 4 N c ( 1 + 1 ε 2 ) N 4 0 1 θ x 2 d x η 0 N c N 1 ( 1 + 1 ε 1 ) c N 2 c N 4 ϖ 1 N 5 0 1 ϑ t 2 d x β 1 2 N 4 c N 1 c N 2 γ 0 4 a 1 0 1 ( κ θ t + θ ) 2 d x β 2 2 N 4 c N 1 c N 2 0 1 ( κ t + ) 2 d x k 2 N c N 4 0 1 x 2 d x k 5 N c N 4 0 1 2 d x N 5 η 1 c N 1 c N 2 0 1 ν 1 ν 2 | ϖ 2 ( s ) | Y 2 x , 1 , s , t d s d x N 5 η 1 0 1 0 1 ν 1 ν 2 s | ϖ 2 ( s ) | Y 2 x , ρ , s , t d s d ρ d x .
by setting
ε 1 = ρ u 4 N 1 , ε 2 = ρ u 4 N 4 ,
we obtain
P t a N 1 2 c N 2 a 3 4 0 1 ϑ x 2 d x ρ u 2 0 1 u t 2 d x a 2 2 N 2 2 ρ ϑ 3 a 1 0 1 u x 2 d x k 4 N c N 4 ( 1 + N 4 ) 0 1 θ x 2 d x η 0 N c N 1 ( 1 + N 1 ) N 2 c N 4 c ϖ 1 N 5 0 1 ϑ t 2 d x β 1 2 N 4 c N 1 c N 2 γ 0 2 4 a 1 0 1 ( κ θ t + θ ) 2 d x β 2 2 N 4 c N 1 c N 2 0 1 ( κ t + ) 2 d x k 2 N c N 4 0 1 x 2 d x k 5 N c N 4 0 1 2 d x N 5 η 1 c N 1 c N 2 0 1 ν 1 ν 2 | ϖ 2 ( s ) | Y 2 x , 1 , s , t d s d x N 5 η 1 0 1 0 1 ν 1 ν 2 s | ϖ 2 ( s ) | Y 2 x , ρ , s , t d s d ρ d x .
Now, we choose our constants.
We take N 2 large enough, such that
α 1 = a 2 2 N 2 2 ρ ϑ 3 a 1 > 0 ;
then, we pick N 1 large enough, in such a way that
α 2 = a N 1 2 c N 2 a 3 4 > 0 .
Then, we pick N 4 and N 5 large enough, in such a way that
α 3 = β 1 2 N 4 c N 1 c N 2 γ 0 2 4 a 1 > 0 , α 4 = β 2 2 N 4 c N 1 c N 2 > 0 , α 5 = N 5 η 1 c N 1 c N 2 > 0 .
Thus, we obtain that
P t α 2 0 1 ϑ x 2 d x ρ u 2 0 1 u t 2 d x α 1 0 1 u x 2 d x [ η 0 N c ] 0 1 ϑ t 2 d x [ k 4 N c ] 0 1 θ x 2 d x α 3 0 1 ( κ θ t + θ ) 2 d x α 4 0 1 ( κ t + ) 2 d x α 5 0 1 ν 1 ν 2 | ϖ 2 ( s ) | Y 2 x , 1 , s , t d s d x k 2 N c 0 1 x 2 d x k 5 N c 0 1 2 d x α 6 0 1 0 1 ν 1 ν 2 s | ϖ 2 ( s ) | Y 2 x , ρ , s , t d s d ρ d x ,
where α 6 = η 1 N 5 > 0 .
Similarly, if we assume
L t = N 1 D 1 t + N 2 D 2 t + D 3 t + N 4 D 4 t + N 5 D 5 t ,
then
L t N 1 ρ ϑ 0 1 ϑ ϑ t d x + N 1 a 2 a 1 ρ u 0 1 ϑ u t d x + N 1 ϖ 1 2 0 1 ϑ 2 d x + N 2 a 2 0 1 ϑ u t u ϑ t d x + ρ u 0 1 u t u d x + N 4 β 1 κ 2 0 1 | θ t θ | d x + N 4 β 1 κ 2 0 1 θ 2 d x + N 4 β 2 κ 2 0 1 | t | d x + N 4 β 2 κ 2 0 1 2 d x + N 5 0 1 0 1 ν 1 ν 2 s e s ρ | ϖ 2 ( s ) | Y 2 x , ρ , s , t d s d ρ d x .
According to the Cauchy–Schwartz, Poincaré’s and Young’s inequalities, we find
L t c 0 1 u t 2 + ϑ t 2 + ϑ x 2 + u x 2 + ( κ θ t + θ ) 2 + θ x 2 d x + c 0 1 2 + x 2 + ( κ t + ) 2 d x + c 0 1 0 1 ν 1 ν 2 s | ϖ 2 ( s ) | Y 2 x , ρ , s , t d s d ρ .
On the other hand, by (32), we have
a 1 u x 2 + 2 a 2 ϑ x u x + a 3 ϑ x 2 > 1 2 ( a 1 a 2 2 a 3 ) u x 2 + ( a 3 a 2 2 a 1 ) ϑ x 2 .
Similarly, by ( k k 3 > k 1 2 ) , we have
k θ x 2 + 2 k 1 θ x + k 3 2 > 1 2 ( k k 1 2 k 3 ) θ x 2 + ( k 3 k 1 2 k ) 2 .
Hence, we obtain
L t = P t N E t c E t ,
that is,
N c E t P t N + c E t .
At this point, we choose N large enough, such that
N c > 0 , N η 0 c > 0 , N k 4 c > 0 > 0 , N k 2 c > 0 , N k 5 c > 0 > 0 .
Simplification of (38), (58) and (59) leads us to
c 1 E t P t c 2 E t , t 0 ,
and
P t d 1 E t , t 0 ,
for some d 1 , c 1 , c 2 > 0 .
Consequently, for some ζ 2 > 0 , we find
P t ζ 2 P t , t 0 .
From further simplification of (62), we have the following:
P t P 0 e ζ 2 t , t 0 .
Hence, (56) is achieved by (60) and (63). □

4. Conclusions

This work studies a swelling porous elastic system coupled with thermo-elasticity of the Lord Shulman type, microtemperature and distributed delay, an approach which is more general than classical thermo-elasticity. Furthermore, the problem circumvents the absurd situation of the infinite propagation of the effect of a thermal or mechanical disturbance in the medium. We established the well-posedness of our problem using the semigroup method. Additionally, we used the energy method to prove the stability result for the system. It is intriguing to know that the result was obtained independently of the wave velocities of the system or any form of interactions between coefficients of the system other than hypotheses (5), (6) and (12), which guarantees the positivity of the energy of the system. The present result contributes significantly to the existing literature on swelling porous elastic problems. In future work, we will investigate the system with some damping and source terms.

Author Contributions

Conceptualization, A.C. and R.J.; methodology, A.C. and S.B.; validation, R.J., S.B. and M.A.; formal analysis, M.A. and R.A.; investigation, R.A.; resources, S.B.; writing—original draft preparation, A.C.; writing—review and editing, R.A.; visualization, R.J. and M.A.; supervision, S.B.; project administration, R.J.; funding acquisition, S.B. All authors have read and agreed to the published version of the manuscript.

Funding

This work was supported and funded by the Deanship of Scientific Research at Imam Mohammad Ibn Saud Islamic University (IMSIU) (grant number IMSIU-RG23118).

Data Availability Statement

Data are contained within the article.

Conflicts of Interest

The authors declare no conflict of interest.

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Choucha, A.; Boulaaras, S.; Jan, R.; AbaOud, M.; Alrajhi, R. Well-Posedness and Stability Results for Lord Shulman Swelling Porous Thermo-Elastic Soils with Microtemperature and Distributed Delay. Mathematics 2023, 11, 4785. https://doi.org/10.3390/math11234785

AMA Style

Choucha A, Boulaaras S, Jan R, AbaOud M, Alrajhi R. Well-Posedness and Stability Results for Lord Shulman Swelling Porous Thermo-Elastic Soils with Microtemperature and Distributed Delay. Mathematics. 2023; 11(23):4785. https://doi.org/10.3390/math11234785

Chicago/Turabian Style

Choucha, Abdelbaki, Salah Boulaaras, Rashid Jan, Mohammed AbaOud, and Rowaida Alrajhi. 2023. "Well-Posedness and Stability Results for Lord Shulman Swelling Porous Thermo-Elastic Soils with Microtemperature and Distributed Delay" Mathematics 11, no. 23: 4785. https://doi.org/10.3390/math11234785

APA Style

Choucha, A., Boulaaras, S., Jan, R., AbaOud, M., & Alrajhi, R. (2023). Well-Posedness and Stability Results for Lord Shulman Swelling Porous Thermo-Elastic Soils with Microtemperature and Distributed Delay. Mathematics, 11(23), 4785. https://doi.org/10.3390/math11234785

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