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Article

Existence, Uniqueness and Asymptotic Behavior of Solutions for Semilinear Elliptic Equations

School of Mathematics and Statistics Sciences, Ludong University, Yantai 264025, China
*
Author to whom correspondence should be addressed.
Mathematics 2024, 12(22), 3624; https://doi.org/10.3390/math12223624
Submission received: 20 October 2024 / Revised: 14 November 2024 / Accepted: 19 November 2024 / Published: 20 November 2024
(This article belongs to the Section Difference and Differential Equations)

Abstract

:
A class of semilinear elliptic differential equations was investigated in this study. By constructing the inverse function, using the method of upper and lower solutions and the principle of comparison, the existence of the maximum positive solution and the minimum positive solution was explored. Furthermore, the uniqueness of the positive solution and its asymptotic estimation at the origin were evaluated. The results show that the asymptotic estimation is similar to that of the corresponding boundary blowup problems. Compared with the conclusions of Wei’s work in 2017, the asymptotic behavior of the solution only depends on the asymptotic behavior of b ( x ) at the origin and the asymptotic behavior of g at infinity.

1. Introduction

In the theoretical and applied research of differential equations, the boundary blowup problem, or large solution problem, is a hot topic. The problem originated from the research of Riemannian surface theory and automatic-function theory with negative curvature constant. Later, it was found that the boundary blowup problem appeared in many fields, such as stable constrained stochastic control, superdiffusion process in stochastic process, differential geometry, concentrated wealth effect in ecology, electric potential in hot hollow metal shells, high-speed diffusion in a chemical reaction, etc. These discoveries have prompted many mathematicians to turn their attention to the research of boundary blowup, leading to the continuous development and fine-tuning of the boundary blowup theory.
From the point of view of the research content, the boundary blowup problem mainly focuses on the existence, asymptotic property, and uniqueness of the solution, as well as the asymptotic expansion of the solution at the boundary. The research can be traced back to 1916 by L. Bieberbach [1]. He first studied the following semilinear elliptic equation with an exponential source, which is expressed as follows:
Δ u = e u , x Ω , u = , x Ω .
Regarding the study of boundary blowup problems, a landmark result should be attributed to J.B. Keller [2] and R. Osserman [3]. They revealed that a sufficient and necessary condition for the existence of a solution of the equation
Δ u = f ( u ) , u > 0 , x Ω , u = , x Ω .
is that the inequality 1 2 u s 0 t f ( s ) d s 1 / 2 d t < + is true. This condition came to be known as the Keller–Osserman condition. It played a very important role in subsequent research on the boundary blowup problem. For research on boundary blowup problems, we may refer to [4,5,6,7], among others.
Later, research mainly focused on the following semilinear elliptic differential equation:
Δ u = a ( x ) u b ( x ) g ( u ) , x Ω ,
where Ω R N ( N 3 ) is a domain with C 2 boundary Ω ; a ( x ) is a continuous function in Ω 0 Ω ; b ( x ) is a non-negative continuous function in Ω ¯ ; and g : R 1 R 1 is also assumed to be a non-negative continuous function.
The classical Logistic equation
Δ u = λ u b ( x ) u p , x Ω , u = 0 , x Ω ,
is a special case of (1); here, λ R 1 can be seen as a parameter, and p > 1 is a constant. In [8], Professor Du studied (2) thoroughly and obtained the following theorem:
Theorem 1 
(Theorem 5.1 [8]). Let λ 1 denote the first eigenvalue of the operator Δ with zero Dirichlet boundary condition; then, (2) has no positive solution when λ λ 1 and it has a unique solution when λ > λ 1 .
Many authors focus their study on (1), and a ( x ) may be allowed to be unbounded in Ω , a classical function is 1 | x | 2 (usually under this situation, 0 Ω ). As we all know, in this case, this term is usually called the Hardy potential or inverse square potential. For the study of semilinear elliptic differential equations with the Hardy potential, one can refer to [9,10,11,12,13,14,15,16].
For the study of elliptic differential equations with singular coefficients, the method of upper and lower solutions is usually used. Many scholars choose the corresponding solution of the boundary blasting problem as the upper solution; then, by constructing the appropriate lower solution, they investigate the existence of the solution with zero Dirichlet boundary conditions. In the literature, the asymptotic behavior at the singularity has been studied, but the relationship between the asymptotic behavior and the corresponding boundary blowup problem has not been specified. In this article, we hope to make some breakthroughs in this area. In this research, for elliptic equations with singular coefficients, we determine the relationship between the blowup solutions with zero Dirichlet boundary conditions at singular points and the blowup solutions at the boundary for the corresponding boundary blowup problem. Therefore, in the future, when we study the blowup behavior of solutions at singular points for elliptic equations with singular coefficients, we may first study the asymptotic behavior of solutions at the boundary for the corresponding boundary blowup problem and then study the relationship between them. We believe that many interesting results could be obtained from this kind of research.
Recently, Cîrstea studied the following equation in [12]:
Δ u = λ u | x | 2 b ( x ) h ( u ) , x Ω { 0 } ,
where λ is a parameter, and < λ ( N 2 ) 2 4 and 0 Ω . Here, b ( x ) is a positive continuous function in Ω ¯ { 0 } , which behaves near the origin as a regularly varying function at zero with index θ greater than 2 . The nonlinearity h is assumed to be continuous on R 1 and positive on ( 0 , ) with h ( 0 ) = 0 such that h ( t ) / t is bounded for small t > 0 . The author completely classified the behavior near zero of all positive solutions for (3) when h is regularly varying at with index q greater than 1. In particular, as an application of his main result, he chose h ( t ) = t q ( l o g t ) α 1 as t and b ( x ) = | x | θ ( l o g | x | ) α 2 as | x | 0 , where α 1 and α 2 are any real numbers. We can easily see that h ( t ) = t p e α t ( p > 1 and α > 0 ) does not satisfy the above conditions.
Recently, Wei and Du [17] considered
Δ u = λ u | x | 2 | x | σ u p , x Ω { 0 } ,
under the conditions λ > ( N 2 ) 2 4 , p > 1 , σ > 2 and obtained the following theorem:
Theorem 2. 
Suppose that u ( x ) is an arbitrary positive solution of (4) with zero Dirichlet boundary conditions; then,
lim | x | 0 | x | θ + 2 p 1 u ( x ) = l 1 p 1 ,
where
l = λ + θ + 2 p 1 θ + 2 p 1 + 2 N .
Remark 1. 
From the proof of Theorem 2 in [17], we can easily see that the asymptotic behavior of the solution for (4) with zero Dirichlet boundary conditions at the origin depends not only on λ and N but also on the asymptotic behavior of b ( x ) at the origin and the asymptotic behavior of g at infinity.
In this paper, we consider
Δ u = λ u | x | 2 b ( x ) u p e α u , x Ω 0 ,
where Ω R N ( N 3 ) is a bounded smooth region, and 0 Ω , λ R 1 , b ( x ) is a positive continuous function in Ω ¯ { 0 } ; p > 1 and α > 0 are two constants. We want to know whether the conclusions similar to those in Theorem 1 and Theorem 2 still hold true.

2. Preliminaries

For convenience, we briefly explain the notations and some lemmas, which will be used hereafter.
As usual, suppose p 1 , k is a non-negative integer, C m ( Ω ) denotes the function space such that U and D α U ( | α | m ) are all continuous in Ω , C ( Ω ) = m = 0 C m ( Ω ) , C 0 ( Ω ) denotes all spaces of C ( Ω ) that have compact support sets in Ω , H 0 1 ( Ω ) is the closure of C 0 ( Ω ) in W 1 , 2 ( Ω ) . C 0 , μ ( Ω ¯ ) denotes the space of all μ -Holder continuous functions in Ω ¯ . W 0 1 , p ( Ω ) is the normal Sobolev space, and W 0 1 , 2 ( Ω ) = H 0 1 ( Ω ) . The norm in L q ( Ω ) is defined as follows:
u q = Ω u q 1 / q .
Lemma 1 
(Hardy inequality [18]). Suppose 1 < p < N , u W 0 1 , p ( Ω ) . We have
Ω u p x p d x p N p p Ω u p d x .
In particular, when p = 2 , the inequality is
Ω u 2 x 2 d x 2 N 2 2 Ω u 2 d x .
Denote H as the Hardy constant; that is, H is the best constant to ensure the following formula holds true:
Ω u 2 x 2 d x 1 H Ω u 2 d x , u H 0 1 ( Ω ) .
From Lemma 1, the best Hardy constant is H = ( N 2 ) 2 4 , and as we all know, H = ( N 2 ) 2 4 could not be obtained in H 0 1 ( Ω ) , while it can be expressed as follows:
H = inf u H 0 1 ( Ω ) { 0 } Ω u 2 d x Ω u 2 x 2 d x .
Let ω R N ( N 3 ) be a bounded and smooth domain and denote λ 1 [ c ( x ) , b ( x ) , ω ] (for short, λ 1 [ c , b , ω ] ) as the first eigenvalue for the following boundary value problem:
Δ u + c ( x ) u = μ b ( x ) u , x ω , u = 0 , x ω ,
where c ( x ) is a continuous function on ω ¯ , and c ( x ) > 0 , b ( x ) is a non-negative continuous function on ω ¯ . We denote
λ 1 [ b , ω ] = λ 1 [ 0 , b , ω ] , λ 1 ( ω ) = λ 1 [ 0 , 1 , ω ] , ω δ = { x | x ω and | x | > δ for δ > 0 } .
From the work of Cheng [19] and Wei [20], we have the following:
Lemma 2 
(Proposition 1 [20]). Let λ 1 [ c , b , ω ] be defined as above; then,
(i) If b 1 ( x ) b 2 ( x ) in ω ; then, λ 1 [ c , b 2 , ω ] λ 1 [ c , b 1 , ω ] and the equality holds if and only if b 1 ( x ) b 2 ( x ) ;
(ii) If c 1 ( x ) c 2 ( x ) in ω ; then, λ 1 [ c 1 , b , ω ] λ 1 [ c 2 , b , ω ] and the equality holds if and only if c 1 ( x ) c 2 ( x ) ;
(iii) If 0 < δ 1 < δ 2 in ω ; then, λ 1 [ c , b , ω δ 1 ] < λ 1 [ c , b , ω δ 2 ] and λ 1 [ c , b , ω δ ] λ 1 [ c , b , ω ] as δ 0 + .
Lemma 3 
(Proposition 2 [20]). If ε 0 , then λ 1 [ 1 x 2 + ε , ω ] H .
Lemma 4 
([19]). Let ω δ be defined as in (6); we have
lim δ 0 + λ 1 [ | x | 2 , ω δ ] = ( N 2 ) 2 4 .
From Lemma 2, we know that λ 1 [ | x | 2 , ω δ ] increases as δ increases.
The following four lemmas and their proofs can be found in [8]:
Lemma 5 
(Lemma 5.6 [8]). Suppose ω is a bounded domain in R N ( N 3 ) , α ( x ) C ( ω ) and | | α ( x ) | | < + , β ( x ) C ( ω ) , and β ( x ) is non-negative and not identically zero. Let u 1 , u 2 C 1 ( ω ) be positive in ω and satisfy in the weak sense
Δ u 1 + α ( x ) u 1 β ( x ) g 1 ( u 1 ) 0 Δ u 2 + α ( x ) u 2 β ( x ) g 1 ( u 2 ) , x ω ,
and
lim x ω sup ( u 2 u 1 ) 0 ,
where g 1 ( u ) is continuous and g 1 ( u ) u is strictly increasing for u in the range min { u 1 , u 2 } < u < max { u 1 , u 2 } . Then,
u 2 < u 1 .
Lemma 6 
(Theorem 6.6 [8]). Suppose f ( u ) is continuous on R 1 ; there exists s 0 > 0 , h ( u ) is a non-decreasing continuous function for u s 0 such that
f ( u ) h ( u ) > 0
and
s 0 s 0 t h ( s ) d s 1 / 2 d t < .
If Ω is a bounded Lipschitz region and there exists a v * W 1 , 2 ( Ω ) L ( Ω ) such that
Δ v * f ( v * ) , x Ω ,
then the equation
Δ u = f ( u ) , x Ω , u = , x Ω ,
has at least a solution u C 1 ( Ω ) such that u v * in Ω, and among all such solutions, there are the largest positive solution u * and the smallest positive solution u * .
Lemma 7 
(Theorem 6.8 [8]). Suppose Ω and f ( u ) satisfy the conditions in Lemma 6, then (7) has a solution u, and if Ω C 2 ; then,
lim d ( x ) 0 Ψ f [ u ( x ) ] d ( x ) = 1 ,
where
d ( x ) = d ( x , Ω )
and
Ψ f [ u ] = 1 2 u s 0 t f ( s ) d s 1 / 2 d t .
Lemma 8 
(Theorem 6.10 [8]). Suppose Ω and f ( u ) satisfy the conditions in Lemma 6; furthermore,
lim t + Ψ f ( β t ) Ψ f ( t ) > 1 , β ( 0 , 1 ) .
f ( 0 ) = 0 , f ( t ) t does not decrease on t > 0 ; then, Equation (7) has a unique non-negative solution.

3. Main Results

Now, we consider Equation (5) with zero Dirichlet boundary conditions as follows:
Δ u = λ u | x | 2 b ( x ) u p e α u , x Ω 0 , u = 0 , x Ω .
First, we have
Theorem 3. 
Let H be defined as in Section 2; then, (8) has no positive solution when λ H , and it has at least a minimal positive solution and a maximal positive solution when λ > H .
Proof. 
Assume that u C 1 ( Ω ) is a positive solution of (8); from the first equation of (8), we have
Ω u Δ u d x = Ω λ u 2 | x | 2 d x Ω b ( x ) u p + 1 e α u d x .
Using the integration by parts, we deduce
Ω u 2 d x = λ Ω u 2 | x | 2 d x Ω b ( x ) u p + 1 e α u d x ,
and therefore,
H Ω u 2 d x Ω u 2 | x | 2 d x = λ Ω b ( x ) u p + 1 e α u d x Ω u 2 | x | 2 d x < λ .
From the above inequality, we know if λ H , then (8) has no positive solution. This completes the proof of the first part of Theorem 3.
Now, we suppose λ > H . By Lemma 4, δ 0 > 0 such that for any δ δ 0 , λ 1 | x | 2 , Ω δ < λ . Let ϕ δ > 0 be the solution of
Δ u = λ 1 | x | 2 , Ω δ u | x | 2 , x Ω δ , u = 0 , x Ω δ .
Then, we can easily obtain that for any ε > 0 sufficiently small,
Δ ( ε ϕ δ ) = ε λ 1 | x | 2 , Ω δ ϕ δ | x | 2 < ε λ ϕ δ | x | 2 ε p b ( x ) ϕ δ p e α ε ϕ δ , x Ω δ , ε ϕ δ = 0 , x Ω δ ,
which means that ε ϕ δ is a lower solution of the following equation:
Δ u = λ u | x | 2 b ( x ) u p e α u , x Ω δ , u = 0 , x Ω δ .
On the other hand, consider the following equation:
Δ u = λ u | x | 2 b ( x ) u p e α u , x Ω δ , u = , x Ω δ .
Notice that
Δ u = λ u | x | 2 b ( x ) u p e α u λ u M 2 b u u p e α u ,
where | x | M for any x Ω ¯ and b u = max x Ω δ ¯ b ( x ) . Let
f ( u ) = b u u p e α u λ u M 2 .
Then, by Lemma 6 and Lemma 8, we know that the equation
Δ u = λ u M 2 b u u p e α u , x Ω δ , u = , x Ω δ ,
has a unique non-negative solution u δ , ( x ) C 1 ( Ω δ ) , which means that u δ , ( x ) is an upper solution of (10). Then based on the upper and lower theorem, Equation (10) has at least a maximal positive solution and a minimal positive solution. By Lemma 5, we know that all solutions of (10), if exist, must be unique. Denote it as u δ ( x ) ; then, 0 < ε ϕ δ u δ ( x ) u δ , ( x ) . From Lemma 2, we know that u δ ( x ) decreases as δ decreases, so u ̲ ( x ) : = lim δ 0 + u δ ( x ) is well defined in Ω ¯ { 0 } . By the regularity of elliptic equations, u ̲ ( x ) is a solution of (8); now, we prove that u ̲ ( x ) is a minimal positive solution of (8). In fact, for any positive solution u of (8), u is an upper solution of (10); then, Lemma 5 implies that u u δ ( x ) , and thus, u u ̲ ( x ) .
On the other hand, we consider the following equation:
Δ u = λ u | x | 2 b ( x ) u p e α u , x Ω δ , u = 0 , x Ω , u = n , | x | = δ .
Notice that u δ ( x ) is a lower solution of (12) and u δ , ( x ) is an upper solution of (12); then, the upper and lower theorem and Lemma 5 imply that (12) has a unique positive solution u δ , n ( x ) such that
u δ ( x ) u δ , n ( x ) u δ , ( x ) .
It is easy to see that { u δ , n ( x ) } is increasing in n, so lim n u δ , n ( x ) exists; denote it as U δ ( x ) , and U δ ( x ) is a solution of (12) with n = . Similarly, lim δ 0 + U δ ( x ) exists; denote it as u ¯ ( x ) . Then, it is a positive solution of (8) and it is also the maximal positive solution of (8). This completes the proof. □
The lemma below will be useful for our study. Since the proof is relatively elementary, we omit it.
Lemma 9. 
Let Ψ g be defined as in Lemma 7 with f replaced by g; then, we have
(i) Φ g ( t ) = 2 G ( Φ g ( t ) ) and Φ g ( t ) = g ( Φ g ( t ) ) , where G ( t ) = s 0 t g ( s ) d s ;
(ii) Φ g ( 0 ) = + and Φ g ( t ) > 0 for t > 0 .
Theorem 4. 
Suppose that there exists a constant β 0 and b ( x ) satisfies
lim | x | 0 + b ( x ) | x | β = c ,
if λ > H , then (8) has a unique positive solution u such that
lim | x | 0 + u ( x ) Φ g ( ξ | x | r ) = 1 ,
where Φ g is the inverse of Ψ g and g ( t ) = t p e α t ,   ξ = c r , r = β + 2 2 .
Proof. 
Notice that
lim u + G ( u ) g ( u ) = 1 α ,
and thus,
lim t 0 + t G ( Φ g ( t ) ) = lim t 0 + Φ g ( t ) + d s 2 G ( s ) G ( Φ g ( t ) ) 1 / 2 = lim t 0 + 2 G ( Φ g ( t ) ) 1 / 2 1 / 2 G ( Φ g ( t ) ) 3 / 2 g ( Φ g ( t ) ) = 2 α ,
by Lemma 9(i), (16) and (17), we have
lim t 0 + t Φ g ( t ) Φ g ( t ) = lim t 0 + t g ( Φ g ( t ) ) 2 G ( Φ g ( t ) ) = 1 .
From (17), we have for any α > 0 ,
lim t 0 + Φ g ( t ) t α = 0 ,
and thus,
lim t 0 + Φ g ( t ) t 2 / r t Φ g ( t ) = 0 and lim t 0 + Φ g ( t ) t Φ g ( t ) = .
Also notice that (14) holds, and we can easily infer that for any 0 < ε < min { r 1 + r 2 , c } , there exists a positive constant δ such that
( c ε ) | x | β b ( x ) ( c + ε ) | x | β , for 0 < | x | < 2 δ ,
and
1 ε < t Φ g ( t ) Φ g ( t ) < 1 + ε ,
ε < r N 1 t + λ Φ g ( t ) t 2 / r t Φ g ( t ) < ε ,
λ Φ g ( t ) t Φ g ( t ) + 2 r ( N 1 ) 0 ,
for any 0 < t < 2 δ and λ > H .
By Lemma 4 and λ > H , we know there exists a positive constant σ 1 < 2 δ such that
H < λ 1 | x | 2 , Ω σ 1 2 δ < λ ,
where
Ω σ 1 2 δ : = { x Ω | σ 1 < | x | < 2 δ } .
Let ξ ̲ = ( c + ε ) ( 1 + ε ) r 2 ε ε r 2 , ξ ¯ = ( c ε ) ( 1 ε ) r + ε r 2 + 2 ε , for any σ ( 0 , σ 1 ) , σ < | x | < 2 δ ; define
v ¯ σ = Φ g ξ ¯ ( | x | σ ) r ,
and for any σ ( 0 , σ 1 ) , 2 σ < | x | + σ < 2 δ , define
v ̲ σ = Φ g ( ξ ̲ | x | + σ r ) .
Let t = ξ ¯ ( | x | σ ) r ; then,
v ¯ σ = Φ g ξ ¯ ( | x | σ ) r = Φ g ( t ) .
Notice that Φ g ( t ) = 2 G ( Φ g ( t ) ) , so
v ¯ σ x i = Φ g ( t ) ξ ¯ r ( | x | σ ) r 1 x i | x | ,
2 v ¯ σ x i 2 = Φ g ( t ) ξ ¯ 2 r 2 ( | x | σ ) 2 r 2 x i 2 | x | 2 + Φ g ( t ) ξ ¯ r ( r 1 ) ( | x | σ ) r 2 x i 2 | x | 2 + Φ g ( t ) ξ ¯ r ( | x | σ ) r 1 1 | x | Φ g ( t ) ξ ¯ r ( | x | σ ) r 1 x i 2 | x | 3 ;
thus,
Δ v ¯ σ = Φ g ( t ) ξ ¯ r 2 ( | x | σ ) 2 r 2 + Φ g ( t ) ξ ¯ r ( r 1 ) ( | x | σ ) r 2 + Φ g ( t ) ξ ¯ r ( | x | σ ) r 1 N 1 | x | ,
and therefore, for any σ < | x | < 2 δ , we have
Δ v ¯ σ λ | x | 2 v ¯ σ + b ( x ) g ( v ¯ σ ) = Φ g ( t ) r 2 ξ ¯ ( | x | σ ) 2 r 2 Φ g ( t ) r ( r 1 ) ξ ¯ ( | x | σ ) r 2 Φ g ( t ) r ξ ¯ ( | x | σ ) r 1 N 1 | x | λ | x | 2 Φ g ( t ) + b ( x ) g ( Φ g ( t ) ) Φ g ( t ) ξ ¯ ( | x | σ ) r 2 r 2 t Φ g ( t ) Φ g ( t ) + r ( r 1 ) + r N 1 | x | σ | x | + λ Φ g ( t ) ( | x | σ ) 2 t Φ g ( t ) | x | 2 c ε Φ g ( t ) | x | σ 2 | x | β t Φ g ( t ) .
From β 0 , we have
c ε Φ g ( t ) | x | σ 2 | x | β t Φ g ( t ) c ε t Φ g ( t ) ξ ¯ 2 Φ g ( t ) .
By (19) and (20), we can obtain
Φ g ( t ) ξ ¯ ( | x | σ ) r 2 r 2 t Φ g ( t ) Φ g ( t ) + r ( r 1 ) + r N 1 | x | σ | x | + λ Φ g ( t ) ( | x | σ ) 2 t Φ g ( t ) | x | 2 c ε t Φ g ( t ) ξ ¯ 2 Φ g ( t ) ε Φ g ( t ) ξ ¯ ( | x | σ ) r 2 0 .
Similarly, notice that 2 σ < | x | + σ < 2 δ implies b ( x ) < ( c + ε ) | x | β and σ < | x | < 2 δ ; thus, by (19)–(21), we have
Δ v ̲ σ λ | x | 2 v ̲ σ + b ( x ) g ( v ̲ σ ) Φ g ( s ) ξ ̲ ( | x | + σ ) r 2 r 2 s Φ g ( s ) Φ g ( s ) + r ( r 1 ) + r N 1 | x | + σ | x | + λ Φ g ( s ) ( | x | + σ ) 2 s Φ g ( s ) | x | 2 ( c + ε ) Φ g ( s ) | x | + σ 2 | x | β s Φ g ( s ) Φ g ( s ) ξ ̲ ( | x | + σ ) r 2 r 2 ( 1 + ε ) + r ( r 1 ) + 2 r N 1 + λ Φ g ( s ) s Φ g ( s ) + ( c + ε ) ( 1 + ε ) ξ ̲ 2 ε Φ g ( s ) ξ ̲ ( | x | + σ ) r 2 0 ,
where s = ξ ̲ | x | + σ r .
Let u be any positive solution of (8) and consider the equation
Δ w = λ | x | 2 w b ( x ) g ( w ) , x Ω σ 2 δ , w = , | x | = 2 δ , w = 0 , | x | = σ ,
using similar methods as that in Theorem 3 and for any σ ( 0 , σ 1 ) , H < λ 1 | x | 2 , Ω σ 2 δ < λ 1 | x | 2 , Ω σ 1 2 δ < λ , it is easy to see that the above problem has a minimum positive solution w. Let v = v ¯ σ + w ; then,
Δ v λ | x | 2 v b ( x ) g ( v ) , x Ω σ 2 δ ,
here, we use the fact that
g ( v ¯ σ + w ) g ( v ¯ σ ) + g ( w ) .
In addition,
v | | x | = 2 δ = > u | | x | = 2 δ , v | | x | = σ = > u | | x | = σ ,
by Lemma 5, we have
w + v ¯ σ u , x Ω σ 2 δ .
Similarly,
u + w v ̲ σ , x Ω σ 2 δ ,
let σ 0 ; then, we obtain
Φ g ξ ¯ ( | x | ) r + 2 w u + w Φ g ( ξ ̲ | x | r ) , 0 < | x | < 2 δ ,
and thus,
lim | x | 0 + Φ g ξ ¯ ( | x | ) r Φ g ( ξ ̲ | x | r ) lim | x | 0 + u Φ g ( ξ ̲ | x | r ) 1 ,
on the other hand,
lim ε 0 + ξ ̲ = lim ε 0 + ξ ¯ = ξ ;
therefore,
lim | x | 0 + u Φ g ( ξ | x | r ) = 1 .
Suppose u 1 and u 2 are two arbitrary positive solutions of (8); then, (23) implies that
lim | x | 0 + u 1 ( x ) u 2 ( x ) = 1 ,
which means that for any 0 < ε < 1 , there exists δ > 0 small enough such that when | x | < δ ,
( 1 ε ) u 2 ( x ) < u 1 ( x ) < ( 1 + ε ) u 2 ( x ) ,
consider the following equation:
Δ u = λ u | x | 2 b ( x ) u p e α u , x Ω δ / 2 , u = 0 , x Ω , u = u 1 ( x ) , | x | = δ 2 .
Notice that
Δ ( 1 ε ) u 2 ( x ) = λ ( 1 ε ) u 2 ( x ) | x | 2 b ( x ) ( 1 ε ) u 2 ( x ) p e α u 2 ( x ) λ ( 1 ε ) u 2 ( x ) | x | 2 b ( x ) ( 1 ε ) p u 2 ( x ) p e α ( 1 ε ) u 2 ( x ) , x Ω δ / 2 ,
by (24) and notice that u 2 ( x ) is a positive solution of (8); we have
( 1 ε ) u 2 ( x ) = 0 u 1 ( x ) , x Ω , ( 1 ε ) u 2 ( x ) u 1 ( x ) , | x | = δ 2 ;
then, Lemma 5 implies that
( 1 ε ) u 2 ( x ) u 1 ( x ) , for any x Ω δ / 2 .
Similarly, we can obtain
u 1 ( x ) ( 1 + ε ) u 2 ( x ) , for any x Ω δ / 2 .
Let ε 0 + ; we have
u 2 ( x ) u 1 ( x ) , for any x Ω { 0 } .
This completes the proof. □

4. Numerical Example

In this section, we give some numerical examples to verify Theorem 4. For simplicity, we suppose that N = 3 , Ω = B ( 0 ; 1 ) and b ( x ) = c | x | β , which shows that (14) holds true. According to [21], we know that all the solutions of (8) are radially symmetric. Let u ( x ) = u ( ρ ) , ρ = | x | ; then, (8) can be transformed to the following second-order ordinary differential equations with singular coefficients:
u ( ρ ) ( N 1 ) ρ u ( ρ ) = λ u ( ρ ) ρ 2 c ρ β u p ( ρ ) e α u ( ρ ) , 0 < ρ < 1 , u ( ρ ) > 0 , 0 < ρ < 1 , u ( 1 ) = 0 .
In order to use the numerical computation method for the ordinary differential equation, we assume that ρ = 1 t and set u ( ρ ) = y 1 ( t ) , u ( ρ ) = y 1 ( t ) = y 2 ( t ) ; then, (26) can be transformed into
y 1 ( t ) = y 2 ( t ) y 2 ( t ) = N 1 1 t y 2 ( t ) λ y 1 ( t ) ( 1 t ) 2 + c ( 1 t ) β y 1 p ( t ) e α y 1 ( t ) , 0 < t < 1 , y 1 ( 0 ) = 0 .
Example 1. 
Assume that β = 1 , p = 2 , α = 1 , c = 4 and λ = 1 . It is easy to verify that all conditions in Theorem 4 hold. Then, by Theorem 4, we have
lim t 1 y 1 ( t ) Φ g ( ξ ( 1 t ) r ) = 1 ,
where ξ = 8 3 , r = 3 2 .
Because the function Φ g can not be easily obtained from the inverse of Ψ g , we consider the numerical solution of the function Φ g ; notice that the function Φ g satisfies
Φ g ( t ) = 2 G ( Φ g ( t ) ) , Φ g ( 0 ) = + .
Let Φ g ( ξ ( 1 t ) r ) = z ( t ) and s = ξ ( 1 t ) r ; then, we have
z ( t ) = ξ r ( 1 t ) r 1 2 G ( z ( t ) ) , z ( 1 ) = + ,
where
G ( u ) = e u ( u 2 2 u + 2 ) 2 .
The graph of numerical boundary blowup solutions for Equations (27) and (28) is presented in Figure 1.

5. Conclusions

In this paper, a class of semilinear elliptic differential equations was investigated. By constructing the inverse function and using the method of upper and lower solutions and the principle of comparison, the existence of maximum positive solution and minimum positive solution was explored. Furthermore, the uniqueness of the positive solution and its asymptotic estimation at the origin were investigated. The results show that the asymptotic estimation is similar to that of the corresponding boundary blowup problems. It is worth mentioning that the above methods can also be used to deal with the case of α = 0 .
From Theorem 4 and its proof, we can easily see that the asymptotic behavior of the solution for (8) at the origin does not depend on λ and N; it only depends on the asymptotic behavior of b ( x ) at the origin and the asymptotic behavior of g at infinity. Comparing Theorem 4 with Theorem 2, we see that the asymptotic behavior of the solution at the origin when α = 0 is fundamentally different from that when α 0 . From this point of view, we believe that α = 0 is a branch point. On the other hand, we only consider the case of β 0 ; compared with the work of Wei [17] and Du [8], we have
Conjecture. The conclusion of Theorem 4 is also true when 2 < β < 0 .
In fact, the following numerical examples (see Figure 2) also support this conjecture:
Example 2. 
Consider (27) and (28) again. Assume that β = 1 , p = 2 , α = 1 , c = 4 and λ = 1 . Then, ξ = 2 2 , r = 1 2 .
Now, we discuss how the solution of Equation (8) changes at the origin as the parameters β   a n d c change. We only consider the single-parameter variation case. By Theorem 4, we have
u c Φ g ( s ) | x | r 2 c r , u β Φ g ( s ) c 4 r 3 / 2 + ln | x | | x | r , 0 < | x | < < 1 ,
notice that Φ g ( s ) < 0 , for s > 0 ; then,
u c < 0 , u β > 0 , 0 < | x | < < 1 ,
which shows that c can reduce the blowup rate of the solution, while β , on the contrary, can accelerate the blowup of the solution. The numerical results also support these results (see Figure 3 and Figure 4).
Let p = 2 , α = 1 , λ = 1 . When c changes, we assume β = 1 ; when β changes, we assume c = 4 .

Author Contributions

Methodology, L.-L.W. and Y.-H.F.; Software, J.-J.L.; Validation, L.-L.W., J.-J.L. and Y.-H.F.; Formal analysis, L.-L.W. and Y.-H.F.; Writing—original draft, L.-L.W. and Y.-H.F.; Writing—review & editing, L.-L.W. and Y.-H.F.; Visualization, J.-J.L. All authors have read and agreed to the published version of the manuscript.

Funding

The research is supported by the National Natural Science Foundation of China (11201213) and the Natural Science Foundation of Shandong Province (ZR2015AM026).

Data Availability Statement

The original contributions presented in the study are included in the article, further inquiries can be directed to the corresponding author.

Conflicts of Interest

The authors declare no conflict of interest.

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Figure 1. Contrast diagram of boundary blowup solution, y 1 ( t ) = u ( ρ ) , z ( t ) = Φ g ( ξ ρ r ) , ρ = | x | , t = 1 ρ . The initial condition for Equation (27) is [ 0 0.6175 ] , and the initial condition for Equation (28) is 0.4282 .
Figure 1. Contrast diagram of boundary blowup solution, y 1 ( t ) = u ( ρ ) , z ( t ) = Φ g ( ξ ρ r ) , ρ = | x | , t = 1 ρ . The initial condition for Equation (27) is [ 0 0.6175 ] , and the initial condition for Equation (28) is 0.4282 .
Mathematics 12 03624 g001
Figure 2. Contrast diagram of boundary blowup solution when β = 1 , y 1 ( t ) = u ( ρ ) , z ( t ) = Φ g ( ξ ρ r ) , ρ = | x | , t = 1 ρ . The initial condition for Equation (27) is [ 0 0.14 ] , and the initial condition for Equation (28) is 0.25 .
Figure 2. Contrast diagram of boundary blowup solution when β = 1 , y 1 ( t ) = u ( ρ ) , z ( t ) = Φ g ( ξ ρ r ) , ρ = | x | , t = 1 ρ . The initial condition for Equation (27) is [ 0 0.14 ] , and the initial condition for Equation (28) is 0.25 .
Mathematics 12 03624 g002
Figure 3. Boundary blowup solution when c = 1 , 2 , 3 , 4 , respectively. The initial condition for Equation (27) is [ 0 1 ] .
Figure 3. Boundary blowup solution when c = 1 , 2 , 3 , 4 , respectively. The initial condition for Equation (27) is [ 0 1 ] .
Mathematics 12 03624 g003
Figure 4. Boundary blowup solution when β = 1 , 2 , 3 , 4 , respectively. The initial condition for Equation (27) is [ 0 3 ] .
Figure 4. Boundary blowup solution when β = 1 , 2 , 3 , 4 , respectively. The initial condition for Equation (27) is [ 0 3 ] .
Mathematics 12 03624 g004
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Wang, L.-L.; Liu, J.-J.; Fan, Y.-H. Existence, Uniqueness and Asymptotic Behavior of Solutions for Semilinear Elliptic Equations. Mathematics 2024, 12, 3624. https://doi.org/10.3390/math12223624

AMA Style

Wang L-L, Liu J-J, Fan Y-H. Existence, Uniqueness and Asymptotic Behavior of Solutions for Semilinear Elliptic Equations. Mathematics. 2024; 12(22):3624. https://doi.org/10.3390/math12223624

Chicago/Turabian Style

Wang, Lin-Lin, Jing-Jing Liu, and Yong-Hong Fan. 2024. "Existence, Uniqueness and Asymptotic Behavior of Solutions for Semilinear Elliptic Equations" Mathematics 12, no. 22: 3624. https://doi.org/10.3390/math12223624

APA Style

Wang, L. -L., Liu, J. -J., & Fan, Y. -H. (2024). Existence, Uniqueness and Asymptotic Behavior of Solutions for Semilinear Elliptic Equations. Mathematics, 12(22), 3624. https://doi.org/10.3390/math12223624

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