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BY 4.0 license Open Access Published by De Gruyter June 13, 2023

Multiplicity results for fractional Schrödinger-Kirchhoff systems involving critical nonlinearities

  • Soraya Fareh ORCID logo , Kamel Akrout ORCID logo , Abdeljabbar Ghanmi ORCID logo and Dušan D. Repovš ORCID logo EMAIL logo

Abstract

In this article, we study certain critical Schrödinger-Kirchhoff-type systems involving the fractional p -Laplace operator on a bounded domain. More precisely, using the properties of the associated functional energy on the Nehari manifold sets and exploiting the analysis of the fibering map, we establish the multiplicity of solutions for such systems.

MSC 2010: 35P30; 35J35; 35J60

1 Introduction

In recent years, a lot of attention has been paid to problems involving fractional and nonlocal operators. These types of problems arise in applications in many fields, e.g., in materials science [9], phase transitions [5,39], water waves [16,17], minimal surfaces [13], and conservation laws [10]. For more applications of such problems in physical phenomena, probability, and finances, we refer interested readers to [12,14,47]. Due to their importance, there are many interesting works on the existence and multiplicity of solutions for fractional and nonlocal problems either on bounded domains or on the entire space, see [1,3,4,6,23,24,34,3638].

In the last decade, many scholars have paid extensive attention to Kirchhoff-type elliptic equations with critical exponents, see [20,25,33], for the bounded domains and [26,28,29] for the entire space. In particular, in [22], the authors considered the following Kirchhoff problem:

(1.1) M R 2 n u ( x ) u ( y ) 2 x y n + 2 s d x d y ( Δ ) s u = λ f ( x , u ) + u 2 s 2 u in Ω , u = 0 on R n \ Ω ,

where t 0 and M ( t ) = a + b t for some a > 0 and b 0 . Here, and in the rest of this article, Ω will denote a bounded domain in R n with Lipschitz boundary Ω .

Under suitable conditions and by using the truncation technique method combined with the mountain pass theorem, the authors proved that for λ > 0 large enough, problem (1.1) has at least one nontrivial solution. Later, the fractional Kirchhoff-type problems were extensively studied by many authors using different methods, see [7,8,15,21,27,3032,35,40,4245]. In particular, by using the Nehari manifold method and the symmetric mountain pass theorem, Xiang et al. [43] investigated the multiplicity of solutions for some p -Kirchhoff system with Dirichlet boundary conditions.

Mingqi et al. [30] studied the following Schrödinger-Kirchhoff-type system:

(1.2) M ( [ ( u , v ) ] s , p p + u , v p , V p ) ( p s u + V ( x ) u p 2 u ) = λ H u ( x , u , v ) + α p s v β u α 2 u in R n , M ( [ ( u , v ) ] s , p p + u , v p , V p ) ( p s v + V ( x ) v p 2 v ) = λ H v ( x , u , v ) + β p s u α v β 2 v in R n ,

where λ > 0 , α + β = p s n p n s p , V : R n [ 0 , ) is a continuous function, the Kirchhoff function M : ( 0 , ) ( 0 , ) is continuous, and H u and H v are Caratheodory functions. Under some suitable assumptions and by applying the mountain pass theorem with Ekeland’s variational principle, the authors obtained the existence and asymptotic behavior of solutions for system (1.2).

By the same methods as in [30], Fiscella et al. [21] studied the existence of solutions for a critical Hardy-Schrödinger-Kirchhoff-type system involving the fractional p -Laplacian in R n . Using the three critical points theorem, Azroul et al. [8] established the existence of three weak solutions for a fractional p -Kirchhoff-type system on a bounded domain with homogeneous Dirichlet boundary conditions. Recently, Azroul et al. [7] have established the existence of three solutions for the ( p , q ) -Schrödinger-Kirchhoff-type system in R n via the three critical points theorem.

Motivated by the above-mentioned articles, we consider in this article the following Schrödinger-Kirchhoff-type system involving the fractional p -Laplacian and critical nonlinearities:

(1.3) M 1 ( u V 1 p ) ( ( Δ ) p s u + V 1 ( x ) u p 2 u ) = a 1 ( x ) u p s 2 u + λ f ( x , u , v ) in Ω , M 2 ( v V 2 p ) ( ( Δ ) p s v + V 2 ( x ) v p 2 v ) = a 2 ( x ) v p s 2 v + λ g ( x , u , v ) in Ω , u , v > 0 in Ω , u = v = 0 on R n \ Ω ,

where . V 1 and . V 2 will be given later (see (1.6)), n > p s , 0 < s < 1 < q < p , λ is a positive parameter, the weight functions a 1 and a 2 are positive and bounded on Ω , and ( Δ ) p s is the fractional p -Laplace operator, defined as follows:

( Δ ) p s u = 2 lim ε 0 R N \ B ε ( x ) u ( x ) u ( y ) p 2 ( u ( x ) u ( y ) ) x y n + p s d y , for all x R n ,

where B ε ( x ) = { y R n : x y < ε } . For more details about the fractional p -Laplacian operator and the basic properties of fractional Sobolev spaces, we refer the reader to [18].

Throughout this article, the index i will denote integers 1 or 2, and we shall assume that the potential function V i : Ω ( 0 , ) is continuous and that there exists v i > 0 such that inf Ω V i v i . In addition, we shall assume that M i : ( 0 , ) ( 0 , ) is a continuous function satisfying the following conditions:

( H 1 ) lim t t 1 p s p M i ( t ) = 0 .

( H 2 ) There exists m i > 0 such that for all t > 0 , we have M i ( t ) m i .

( H 3 ) There exists θ i 1 , p s p such that for all t > 0 , we have M i ( t ) t θ i M ^ i ( t ) , where M ^ i ( t ) = 0 t M i ( s ) d s .

Moreover, we shall assume that f , g C ( Ω ¯ × R × R , [ 0 , [ ) are positively homogeneous functions of degree ( q 1 ) , i.e., for all t > 0 and ( x , u , v ) Ω × R × R , we have

(1.4) f ( x , t u , t v ) = t q 1 f ( x , u , v ) , g ( x , t u , t v ) = t q 1 g ( x , u , v ) .

Finally, we shall also assume that there exists a function H : Ω ¯ × R × R R satisfying

H u ( x , u , v ) = f ( x , u , v ) and H v ( x , u , v ) = g ( x , u , v ) ,

where H u (respectively, H v ) denotes the partial derivative of H with respect to u (respectively, v ). We note that the primitive function H belongs to C 1 ( Ω ¯ × R × R , R ) and satisfies the following assumptions for all t > 0 , ( x , u , v ) Ω ¯ × R × R , and some constant γ > 0 :

(1.5) H ( x , t u , t v ) = t q H ( x , u , v ) , q H ( x , u , v ) = u f ( x , u , v ) + v g ( x , u , v ) , H ( x , u , v ) γ ( u q + v q ) .

Before stating our main result, let us introduce some notations. For s ( 0 , 1 ) , we define the functional space

W s , p ( Q ) = w : R n R measurable: w L p ( Ω ) and w ( x ) w ( y ) x y n p + s L p ( Q ) ,

which is endowed with the norm

w W s , p ( Q ) = w L p ( Ω ) p + Q w ( x ) w ( y ) p x y n + p s d x d y 1 p ,

where Q = R 2 n \ ( Ω c × Ω c ) and Ω c = R n \ Ω . From now on, we shall denote by q the norm on the Lebesgue space L q ( Ω ) . It is well known that ( W s , p ( Q ) , W s , p ( Q ) ) is a uniformly convex Banach space.

Next, L p ( Ω , V i ) denotes the Lebesgue space of real-valued functions, with V i ( x ) w p L 1 ( Ω ) , endowed with the following norm:

w p , V i = Ω V i ( x ) w p d x 1 p .

Let us denote by W V i s , p ( Q ) the completion of C 0 ( Q ) with respect to the norm

(1.6) w V i = w p , V i p + Q w ( x ) w ( y ) p x y n + p s d x d y 1 p .

According to [18, (Theorem 6.7]), the embedding W V i s , p ( Q ) L ν ( Ω ) is continuous for any ν [ p , p s ] . Namely, there exists a positive constant C ν such that

w ν C ν w V i for all w W V i s , p ( Q ) .

Moreover, by [46, Lemma 2.1], the embedding from W V i s , p ( Q ) into L ν ( Ω ) , is compact for any ν [ 1 , p s ) .

Let W = W V 1 s , p ( Q ) × W V 2 s , p ( Q ) be equipped with the norm ( u , v ) = ( u V 1 p + v V 2 p ) 1 p . Then, ( W , . ) is a reflexive Banach space. The interested reader can refer to [2] for more details. Let S p , V i be the best Sobolev constants for the embeddings from W V i s , p ( Q ) into L p s ( Ω ) , which is given as follows:

(1.7) S p , V i = inf u W V i s , p ( Q ) \ { 0 } w V i p w p s p .

For simplicity, in the rest of this article, S will denote the following expression:

(1.8) S = min ( S p , V 1 , S p , V 2 ) .

Next, we define the notion of solutions for problem (1.3).

Definition 1.1

We say that ( u , v ) W is a weak solution of problem (1.3), if

M 1 ( u p ) Q u ( x ) u ( y ) p 2 ( u ( x ) u ( y ) ) ( z ( x ) z ( y ) ) x y n + p s d x d y + Ω V 1 ( x ) u p 2 u z d x + M 2 ( v p ) Q v ( x ) v ( y ) p 2 ( v ( x ) v ( y ) ) ( w ( x ) w ( y ) ) x y n + p s d x d y + Ω V 2 ( x ) v p 2 v w d x = Ω ( a 1 ( x ) u p s 2 u z + a 2 ( x ) v p s 2 v w ) d x + λ Ω ( H u ( x , u , v ) z + H v ( x , u , v ) w ) d x ,

for all ( z , w ) W .

The following theorem is the main result of this article.

Theorem 1.1

Assume that s ( 0 , 1 ) , n > p s , 1 < q < p < p s , and that equations (1.4) and (1.5) hold. If M satisfies conditions ( H 1 )–( H 3 ), then there exists λ > 0 such that for all λ ( 0 , λ ) , system (1.3) has at least two nontrivial weak solutions.

This article is organized as follows. In Section 2, we present some notations and preliminary results related to the Nehari manifold and fibering maps. In Section 3, we prove Theorem 1.1.

2 The Nehari manifold method and fibering maps analysis

This section collects some basic results on the Nehari manifold method and the fibering maps analysis, which will be used in the forthcoming section; we refer the interested reader to [11,12,19] for more details. We begin by considering the Euler-Lagrange functional J λ : W R , which is defined as follows:

(2.1) J λ ( u , v ) = 1 p ( M ^ 1 ( A 1 ( u ) ) + M ^ 2 ( A 2 ( v ) ) ) 1 p s B ( u , v ) λ C ( u , v ) ,

where

A i ( w ) = w V i p , B ( u , v ) = Ω ( a 1 ( x ) u p s + a 2 ( x ) v p s ) d x , C ( u , v ) = Ω H ( x , u , v ) d x .

We can easily verify that J λ C 1 ( W , R ) ; moreover, its derivative J λ from the space W into its dual space W is given as follows:

(2.2) J λ ( u , v ) , ( u , v ) = A 1 ( u ) M 1 ( A 1 ( u ) ) + A 2 ( v ) M 2 ( A 2 ( v ) ) B ( u , v ) λ q C ( u , v ) .

From the last equation, we can see that the critical points of the functional J λ are exactly the weak solutions for problem (1.3). Moreover, since the energy functional J λ is not bounded from below on W , we shall show that J λ is bounded from below on a suitable subset of W , which is known as the Nehari manifold and is defined as follows:

N λ = { ( u , v ) W \ { ( 0 , 0 ) } , J λ ( u , v ) , ( u , v ) W = 0 } .

It is clear that ( u , v ) N λ if and only if

(2.3) A 1 ( u ) M 1 ( A 1 ( u ) ) + A 2 ( v ) M 2 ( A 2 ( v ) ) B ( u , v ) λ q C ( u , v ) = 0 .

Hence, from (2.2), we see that the elements of N λ correspond to nontrivial critical points, which are solutions of problem (1.3).

It is useful to understand N λ in terms of the stationary points of the fibering maps φ u , v : ( 0 , ) R , is defined as follows:

φ u , v ( t ) = J λ ( t u , t v ) = 1 p ( M ^ 1 ( t p A 1 ( u ) ) + M ^ 2 ( t p A 2 ( v ) ) ) t p s p s B ( u , v ) λ t q C ( u , v ) .

A simple calculation shows that for all t > 0 , we have

φ u , v ( t ) = t p 1 ( A 1 ( u ) M 1 ( t p A 1 ( u ) ) + A 2 ( v ) M 2 ( t p A 2 ( v ) ) ) t p s 1 B ( u , v ) λ q t q 1 C ( u , v ) ,

and

φ u , v ( t ) = ( p 1 ) t p 2 ( A 1 ( u ) M 1 ( t p A 1 ( u ) ) + A 2 ( v ) M 2 ( t p A 2 ( v ) ) ) + p t 2 p 2 ( ( A 1 ( u ) ) 2 M 1 ( t p A 1 ( u ) ) + ( A 2 ( v ) ) 2 M 2 ( t p A 2 ( v ) ) ) ( p s 1 ) t p s 2 B ( u , v ) λ q ( q 1 ) t q 2 C ( u , v ) .

It is easy to see that for all t > 0 , we have

φ u , v ( t ) = J λ ( t u , t v ) , ( u , v ) W = 1 t 2 J λ ( t u , t v ) , ( t u , t v ) W .

So, ( t u , t v ) N λ if and only if φ u , v ( t ) = 0 . In the special case, when t = 1 , we obtain ( u , v ) N λ , if and only if φ u , v ( 1 ) = 0 . On the other hand, from (2.3), we obtain

(2.4) φ u , v ( 1 ) = ( p 1 ) ( A 1 ( u ) M 1 ( A 1 ( u ) ) + A 2 ( v ) M 2 ( A 2 ( v ) ) ) ( p s 1 ) B ( u , v ) + p ( ( A 1 ( u ) ) 2 M 1 ( A 1 ( u ) ) + ( A 2 ( v ) ) 2 M 2 ( A 2 ( v ) ) ) λ q ( q 1 ) C ( u , v ) = p ( ( A 1 ( u ) ) 2 M 1 ( A 1 ( u ) ) + ( A 2 ( v ) ) 2 M 2 ( A 2 ( v ) ) ) ( p s p ) B ( u , v ) λ q ( q p ) C ( u , v )

(2.5) φ u , v ( 1 ) = p ( ( A 1 ( u ) ) 2 M 1 ( A 1 ( u ) ) + ( A 2 ( v ) ) 2 M 2 ( A 2 ( v ) ) ) + λ q ( p s q ) C ( u , v ) ( p s p ) ( A 1 ( u ) M 1 ( A 1 ( u ) ) + A 2 ( v ) M 2 ( A 2 ( v ) ) )

(2.6) φ u , v ( 1 ) = p ( ( A 1 ( u ) ) 2 M 1 ( A 1 ( u ) ) + ( A 2 ( v ) ) 2 M 2 ( A 2 ( v ) ) ) ( p s q ) B ( u , v ) + ( p q ) ( A 1 ( u ) M 1 ( A 1 ( u ) ) + A 2 ( v ) M 2 ( A 2 ( v ) ) ) .

Now, in order to obtain a multiplicity of solutions, we divide N λ into three parts as follows:

N λ + = { ( u , v ) N λ : φ u , v ( 1 ) > 0 } = { ( u , v ) W : φ u , v ( 1 ) = 0 and φ u , v ( 1 ) > 0 } , N λ = { ( u , v ) N λ : φ u , v ( 1 ) < 0 } = { ( u , v ) W : φ u , v ( 1 ) = 0 and φ u , v ( 1 ) < 0 } , N λ 0 = { ( u , v ) N λ : φ u , v ( 1 ) = 0 } = { ( u , v ) W : φ u , v ( 1 ) = 0 and φ u , v ( 1 ) = 0 } .

Lemma 2.1

Suppose that ( u 0 , v 0 ) is a local minimizer for J λ on N λ , with ( u 0 , v 0 ) N λ 0 . Then, ( u 0 , v 0 ) is a critical point of J λ .

Proof

If ( u 0 , v 0 ) is a local minimizer for J λ on N λ , then ( u 0 , v 0 ) solves the following optimization problem:

min ( u , v ) N λ J λ ( u , v ) = J λ ( u 0 , v 0 ) , β ( u 0 , v 0 ) = 0 ,

where

β ( u , v ) = A 1 ( u ) M 1 ( A 1 ( u ) ) + A 2 ( v ) M 2 ( A 2 ( v ) ) B ( u , v ) λ q C ( u , v ) .

By the Lagrangian multipliers theorem, there exists δ R , such that

(2.7) J λ ( u 0 , v 0 ) = δ β ( u 0 , v 0 ) .

Since ( u 0 , v 0 ) N λ , we obtain

(2.8) δ β ( u 0 , v 0 ) , ( u 0 , v 0 ) W = J λ ( u 0 , v 0 ) , ( u 0 , v 0 ) W = 0 .

Moreover, by (2.3) and the constraint β ( u 0 , v 0 ) = 0 , we have

β ( u 0 , v 0 ) , ( u 0 , v 0 ) W = p ( ( A 1 ( u 0 ) ) 2 M 1 ( A 1 ( u 0 ) ) + ( A 2 ( v 0 ) ) 2 M 2 ( A 2 ( v 0 ) ) ) ( p s p ) B ( u 0 , v 0 ) λ q ( q p ) C ( u 0 , v 0 ) = φ u 0 , v 0 ( 1 ) .

Since ( u 0 , v 0 ) N λ 0 , we have φ u 0 , v 0 ( 1 ) 0 . Thus, by (2.8), we obtain δ = 0 . Consequently, by substituting δ in (2.7), we obtain J λ ( u 0 , v 0 ) = 0 . This completes the proof of Lemma 2.1.□

In order to understand the Nehari manifold and fibering maps, let us define the function ψ u , v : ( 0 , ) R as follows:

(2.9) ψ u , v ( t ) = t p q ( A 1 ( u ) M 1 ( t p A 1 ( u ) ) + A 2 ( v ) M 2 ( t p A 2 ( v ) ) ) t p s q B ( u , v ) λ q C ( u , v ) .

We note that t q 1 ψ u , v ( t ) = φ u , v ( t ) . Thus, it is easy to see that ( t u , t v ) N λ if and only if

(2.10) ψ u , v ( t ) = 0 .

Moreover, by a direct computation, we obtain

ψ u , v ( t ) = ( p q ) t p q 1 ( A 1 ( u ) M 1 ( t p A 1 ( u ) ) + A 2 ( v ) M 2 ( t p A 2 ( v ) ) ) + p t 2 p q 1 ( A 1 2 ( u ) M 1 ( t p A 1 ( u ) ) + A 2 2 ( v ) M 2 ( t p A 2 ( v ) ) ) ( p s q ) t p s q 1 B ( u , v ) .

Therefore,

(2.11) t q 1 ψ u , v ( t ) = φ u , v ( t ) .

Hence, ( t u , t v ) N λ + , ( respectively , ( t u , t v ) N λ ) if and only if ψ u , v ( t ) = 0 and ψ u , v ( t ) > 0 (respectively, ψ u , v ( t ) = 0 , and ψ u , v ( t ) < 0 ). Put

(2.12) m = min ( m 1 , m 2 ) , θ = max ( θ 1 , θ 2 ) ,

and

(2.13) λ = ( m S ) p s q p s p γ q Ω p s q p s p s p p s q p q ( p s q ) a p q p s p .

Now we shall prove the following crucial result.

Lemma 2.2

Assume that conditions ( H 1 ) and ( H 2 ) hold. Then, for all ( u , v ) N λ , there exist λ > 0 and unique t 1 > 0 and t 2 > 0 , such that for each λ ( 0 , λ ) , we have ( t 1 u , t 1 v ) N λ + and ( t 2 u , t 2 v ) N λ .

Proof

We begin by noting that by (2.9), we have

ψ u , v ( t ) λ q C ( u , v ) , as t 0 + , and ψ u , v ( t ) , as t .

Now, if we combine equations (1.5) and (1.7) with the Hölder inequality, we obtain

(2.14) B ( u , v ) a 1 u p s p s + a 2 v p s p s a ( u p s p s + v p s p s ) a ( S p , V 1 p s p ( A 1 ( u ) ) p s p + S p , V 2 p s p ( A 2 ( u ) ) p s p ) S p s p a ( A ( u , v ) ) p s p ,

and

(2.15) C ( u , v ) γ ( u q q + v q q ) γ Ω p s q p s ( u p s q + v p s q ) γ S q p Ω p s q p s ( A ( u , v ) ) q p ,

where a = max ( a 1 , a 2 ) , A ( u , v ) = ( u , v ) p , and S is given by equation (1.8).

On the other hand, by combining equations (2.14) and (2.15) with ( H 2 ) , we obtain

(2.16) ψ u , v ( t ) t p q ( m 1 A 1 ( u ) + m 2 A 2 ( v ) ) t p s q S p s p a ( A ( u , v ) ) p s p λ q γ S q p Ω p s q p s ( A ( u , v ) ) q p m t p q A ( u , v ) t p s q S p s p a ( A ( u , v ) ) p s p λ q γ S q p Ω p s q p s ( A ( u , v ) ) q p ( A ( u , v ) ) q p F u , v ( t ) ,

where m is given by equation (2.12) and F u , v is defined for t > 0 by

F u , v ( t ) = m t p q ( A ( u , v ) ) p q p t p s q S p s p a ( A ( u , v ) ) p s q p λ q γ S q p Ω p s q p s .

Since 1 < q < p < p s , it is easy to see that lim t 0 + F u , v ( t ) < 0 and lim t F u , v ( t ) = . So, by a simple calculation, we can prove that F u , v attains its unique global maximum at

(2.17) t max ( u , v ) = m S p s p a p q p s q 1 p s p ( A ( u , v ) ) 1 p .

Moreover,

(2.18) F u , v ( t max ) = q γ S q p Ω p s q p s ( λ λ ) ,

where λ is given by (2.13).

If we choose λ < λ , then we obtain from (2.16)

(2.19) ψ u , v ( t max ) ( A ( u , v ) ) q p F u , v ( t max ) > 0 .

Hence, by a variation of ψ u , v ( t ) , there exist unique t 1 < t max ( u , v ) and unique t 2 > t max ( u , v ) , such that ψ u , v ( t 1 ) > 0 and ψ u , v ( t 2 ) < 0 . Moreover, ψ u , v ( t 1 ) = 0 = ψ u , v ( t 2 ) . Finally, it follows from (2.10) and (2.11) that ( t 1 u , t 1 v ) N λ + and ( t 2 u , t 2 v ) N λ . This completes the proof of Lemma 2.2.□

We can see from Lemma 2.2 that sets N λ + and N λ are nonempty. In the following lemma, we shall provide a property related to N λ 0 .

Lemma 2.3

Assume that condition ( H 2 ) holds. Then, for all λ ( 0 , λ ) , we have N λ 0 = .

Proof

We shall argue by contradiction. Assume that there exists λ > 0 in ( 0 , λ ) such that N λ 0 . Let ( u 0 , v 0 ) N λ 0 . Then, invoking ( H 2 ) , (2.5), and (2.15), we have

(2.20) 0 = φ u ( 1 ) = p ( ( A 1 ( u ) ) 2 M 1 ( A 1 ( u ) ) + ( A 2 ( v ) ) 2 M 2 ( A 2 ( v ) ) ) ( p s p ) ( A 1 ( u ) M 1 ( A 1 ( u ) ) + A 2 ( v ) M 2 ( A 2 ( v ) ) ) + λ q ( p s q ) C ( u , v ) p ( ( A 1 ( u ) ) 2 M 1 ( A 1 ( u ) ) + ( A 2 ( v ) ) 2 M 2 ( A 2 ( v ) ) ) ( p s p ) ( m 1 A 1 ( u ) + m 2 A 2 ( v ) ) + λ q ( p s q ) C ( u , v ) p ( ( A ( u ) ) 2 M ( A ( u ) ) + ( A ( v ) ) 2 N ( A ( v ) ) ) ( p s p ) m A ( u , v ) + λ q ( p s q ) γ S q p Ω p s q p s ( A ( u , v ) ) q p .

On the other hand, by ( H 2 ) , (2.6), and (2.14), one has

(2.21) 0 = φ u ( 1 ) = p ( ( A 1 ( u ) ) 2 M 1 ( A 1 ( u ) ) + ( A 2 ( v ) ) 2 M 2 ( A 2 ( v ) ) ) + ( p q ) ( A 1 ( u ) M 1 ( A 1 ( u ) ) + A 2 ( v ) M 2 ( A 2 ( v ) ) ) ( p s q ) B ( u , v ) p ( ( A 1 ( u ) ) 2 M 1 ( A 1 ( u ) ) + ( A 2 ( v ) ) 2 M 2 ( A 2 ( v ) ) ) + ( p q ) ( m 1 A 1 ( u ) + m 2 A 2 ( v ) ) ( p s q ) B ( u , v ) p ( ( A 1 ( u ) ) 2 M 1 ( A 1 ( u ) ) + ( A 2 ( v ) ) 2 M 2 ( A 2 ( v ) ) ) + ( p q ) m A ( u , v ) ( p s q ) S p s p a ( A ( u , v ) ) p s p .

Combining (2.20) and (2.21), we obtain

(2.22) λ m ( A ( u , v ) ) p q p S p s p a ( A ( u , v ) ) p s q p q γ S q p Ω p s q p s .

Next, we define the function H on ( 0 , ) by

H ( t ) = m t p q p S p s p a t p s q p q γ S q p Ω p s q p s .

Since 1 < q < p < p s , it follows that lim t 0 + H ( t ) = 0 and lim t H ( t ) = . A simple computation now shows that H attains its maximum at

t ˜ = p q p s q m S p s p a p p s p ,

and

(2.23) max t > 0 H ( t ) = H ( t ˜ ) = λ .

Hence, it follows from (2.22) and (2.23), that λ max t > 0 H ( t ) = λ , which contradicts λ ( 0 , λ ) . Therefore, we can conclude that that indeed N λ 0 = , for λ ( 0 , λ ) . This completes the proof of Lemma 2.3.□

Lemma 2.4

Assume that conditions ( H 2 ) and ( H 3 ) hold. Then, J λ is coercive and bounded from below on N λ .

Proof

Let ( u , v ) N λ . Then, by (2.3), we obtain

B ( u , v ) = A 1 ( u ) M 1 ( A 1 ( u ) ) + A 2 ( v ) M 2 ( A 2 ( v ) ) λ q C ( u , v ) .

Therefore,

J λ ( u , v ) = 1 p ( M ^ 1 ( A 1 ( u ) ) + M ^ 2 ( A 2 ( v ) ) ) 1 p s ( A 1 ( u ) M 1 ( A 1 ( u ) ) + A 2 ( v ) M 2 ( A 2 ( v ) ) ) λ 1 q p s C ( u , v ) .

Moreover, by ( H 2 ) , ( H 3 ) , and (2.15), we have

J λ ( u , v ) 1 θ 1 p A 1 ( u ) M 1 ( A 1 ( u ) ) + 1 θ 2 p A 2 ( v ) M 2 ( A 2 ( v ) ) 1 p s A 1 ( u ) M 1 ( A 1 ( u ) ) 1 p s A 2 ( v ) M 2 ( A 2 ( v ) ) λ 1 q p s C ( u , v ) 1 θ p 1 p s ( A 1 ( u ) M 1 ( A 1 ( u ) ) + A 2 ( v ) M 2 ( A 2 ( v ) ) ) λ 1 q p s C ( u , v ) 1 θ p 1 p s ( m 1 A 1 ( u ) + m 2 A 2 ( v ) ) λ 1 q p s C ( u , v ) m 1 θ p 1 p s A ( u , v ) λ 1 q p s γ S q p Ω p s q p s ( A ( u , v ) ) q p .

Since q < p and θ p < p s , it follows that J λ is coercive and bounded from below on N λ . This completes the proof of Lemma 2.4.□

By Lemma (2.3), we can write N λ = N λ + N λ , and by Lemma (2.4), we can define

α λ = inf ( u , v ) N λ J λ ( u , v ) and α λ + = inf ( u , v ) N λ + J λ ( u , v ) .

3 Proof of the main result

In this section, we shall prove the main result of this article (Theorem 1.1). First, we need to prove two propositions.

Proposition 3.1

Assume that conditions ( H 2 ) and ( H 3 ) hold. Then, there exist t 0 > 0 and ( u 0 , v 0 ) W \ { 0 } , with ( u 0 , v 0 ) > 0 in R n , such that

(3.1) 1 p ( M ^ 1 ( A 1 ( u 0 ) t 0 p ) + M 2 ^ ( A 2 ( v 0 ) t 0 p ) ) t 0 p s p s B ( u 0 , v 0 ) = s n θ 1 θ p a n s p s m S θ n s p .

Proof

For any ( u , v ) W \ { 0 } , we define the function ζ u , v : ( 0 , ) R as follows:

ζ u , v ( t ) = 1 p ( M ^ 1 ( A 1 ( t u ) ) + M 2 ^ ( A 2 ( t v ) ) ) 1 p s B ( t ( u , v ) ) = 1 p ( M ^ 1 ( t p A 1 ( u ) ) + M ^ 2 ( t p A 2 ( v ) ) ) t p s p s B ( u , v ) .

By ( H 3 ) , it can be shown that lim t 0 + ζ u , v ( t ) 0 and lim t ζ u , v ( t ) = . It is clear that ζ is of class C 1 . Moreover, invoking ( H 2 ) and ( H 3 ) , we obtain

ζ u , v ( t ) t p θ 1 p A 1 ( u ) M 1 ( t p A 1 ( u ) ) + t p θ 2 p A 2 ( v ) M 2 ( t p A 2 ( v ) ) t p s p s B ( u , v ) t p θ p ( A 1 ( u ) M 1 ( t p A 1 ( u ) ) + A 2 ( v ) M 2 ( t p A 2 ( v ) ) ) t p s p s B ( u , v ) t p θ p ( m 1 A 1 ( u ) + m 2 A 2 ( v ) ) t p s p s B ( u , v ) m θ p t p A ( u , v ) t p s p s B ( u , v ) = ω u , v ( t ) .

Since lim t 0 ω u , v ( t ) = 0 and lim t ω u , v ( t ) = , it follows that ω u , v attains its global maximum at

t = m A ( u , v ) θ B ( u , v ) 1 p s p .

Moreover, from (2.14) and the fact that p s > θ p , we have

(3.2) sup t > 0 ω u , v ( t ) = ω u , v ( t ) = p s p p p s m θ p s p s p ( A ( u , v ) ) p s p s p ( B ( u , v ) ) p p s p = p s p p p s m θ p s p s p ( A ( u , v ) ) p s p B ( u , v ) p p s p = s n m θ n s p ( A ( u , v ) ) n s p ( B ( u , v ) ) n s p s s n a n s p s m S θ n s p s n θ 1 θ p a n s p s m S θ n s p = p s θ p θ p p s a n s p s m S θ n s p > 0 .

Therefore, using the variations of the functions ζ u , v and ω u , v , we obtain

sup t > 0 ζ u , v sup t > 0 ω u , v s n θ 1 θ p a n s p s m S θ n s p .

Hence, there exists t 0 > 0 such that

ζ u , v ( t 0 ) = s n θ 1 θ p a n s p s m S θ n s p .

This completes the proof of Proposition 3.1.□

Set now

(3.3) L = ( p q ) m q s n θ 1 θ p q p q p s q θ p 2 p p q γ S q p Ω p s q p s p p q .

Proposition 3.2

Assume that conditions ( H 2 ) and ( H 3 ) hold. If 1 < q < p < p s , then every Palais-Smale sequence { ( u k , v k ) } W for J λ at level c , with

(3.4) c < s n θ 1 θ p a n s p s m S θ n s p λ p p q L ,

possesses a convergent subsequence.

Proof

Let { ( u k , v k ) } be a Palais-Smale sequence for J λ at level c , i.e.,

J λ ( u k , v k ) c , and J λ ( u k , v k ) 0 , as k .

By Lemma (2.4), we know that { ( u k , v k ) } is bounded in W . So up to a subsequence, still denoted by { ( u k , v k ) } , there exists ( u , v ) W , μ > 0 , and η > 0 , such that as k tends to infinity, we have

(3.5) ( u k , v k ) ( u , v ) weakly in W , u k V 1 μ , v k V 2 η , ( u k , v k ) ( u , v ) weakly in L p s ( Ω ) × L p s ( Ω ) , ( u k , v k ) ( u , v ) strongly in L q ( Ω ) × L q ( Ω ) , 1 q < p s , ( u k , v k ) ( u , v ) a.e. in Ω ,

Since 1 q < p s , it follows from [41, Theorem IV-9] that there exist functions l 1 , l 2 L q ( Ω ) such that for a.e. x Ω , we have u k ( x ) l 1 ( x ) , v k ( x ) l 2 ( x ) . Hence, by the dominated convergence theorem,

(3.6) C ( u k , v k ) C ( u , v ) as k .

On the other hand, by the Brezis-Lieb lemma [21, Lemma 1.32], for k large enough, we have

A 1 ( u k ) = A 1 ( u k u ) + A 1 ( u ) + o ( 1 ) , A 2 ( v k ) = A 2 ( v k v ) + A 2 ( v ) + o ( 1 ) ,

and

B ( u k , v k ) = B ( u k u , v k v ) + B ( u , v ) + o ( 1 ) .

Consequently, by letting k tend to infinity, we obtain

o ( 1 ) = J λ ( u k , v k ) , ( u k u , v k v ) W = M 1 ( A 1 ( u k ) ) Q u k ( x ) u k ( y ) p 1 ( ( u k u ) ( x ) ( u k u ) ( y ) ) x y n + p s d x d y + Ω V 1 ( x ) u k p 1 ( u k u ) d x Ω a 1 ( x ) u k p s 1 ( u k u ) d x + M 2 ( A 2 ( v k ) ) Q v k ( x ) v k ( y ) p 1 ( ( v k v ) ( x ) ( v k v ) ( y ) ) x y n + p s d x d y + Ω V 2 ( x ) v k p 1 ( v k v ) d x Ω a 2 ( x ) v k p s 1 ( v k v ) d x λ Ω ( H u ( x , u k , v k ) ( u k u ) + H v ( x , u k , v k ) ( v k v ) ) d x = M 1 ( μ p ) ( μ p A 1 ( u ) ) + M 2 ( η p ) ( η p A 2 ( v ) ) Ω ( a 1 ( x ) u k p s + a 2 ( x ) v k p s ) d x + Ω ( a 1 ( x ) u p s + a 2 ( x ) v p s ) d x λ Ω ( H u ( x , u k , v k ) ( u k u ) + H v ( x , u k , v k ) ( v k v ) ) d x + o ( 1 ) = M 1 ( μ p ) A 1 ( u k u ) + M 2 ( η p ) A 2 ( v k v ) B ( u k u , v k v ) λ Ω ( H u ( x , u k , v k ) ( u k u ) + H v ( x , u k , v k ) ( v k v ) ) d x + o ( 1 ) .

Therefore,

M 1 ( μ p ) lim k A 1 ( u k u ) + M 2 ( η p ) lim k A 2 ( v k v ) = lim k B ( u k u , v k v ) + lim k λ Ω ( H u ( x , u k , v k ) ( u k u ) + H v ( x , u k , v k ) ( v k v ) ) d x

By (1.5), (3.5), and the Holder inequality, it follows that

Ω ( H u ( x , u k , v k ) ( u k u ) + H v ( x , u k , v k ) ( v k v ) ) d x γ q Ω u k q 1 ( u k u ) d x + γ q Ω v k q 1 ( v k v ) d x γ q u k q q 1 u k u q + γ q v k q q 1 v k v q C q γ q u k V 1 q 1 u k u q + C q γ q v k V 2 q 1 v k v q

for some positive constant C q . So, we obtain

(3.7) lim k Ω ( H u ( x , u k , v k ) ( u k u ) + H v ( x , u k , v k ) ( v k v ) ) d x = 0 .

Thus, from (3.7), we can deduce that

lim k B ( u k u , v k v ) = M 1 ( μ p ) lim k A 1 ( u k u ) + M 2 ( η p ) lim k A 2 ( v k v ) .

For simplicity, set b lim k B ( u k u , v k v ) . Note that b 0 . Moreover, to prove that ( u k , v k ) converges strongly to ( u , v ) , it suffices to prove that b = 0 . Suppose to the contrary, that b > 0 . Then, by ( H 2 ) , we obtain

(3.8) A 1 ( u k u ) M 1 ( μ p ) + A 2 ( v k v ) M 2 ( η p ) m 1 A 1 ( u k u ) + m 2 A 2 ( v k v ) m A ( u k u , v k v ) .

Using (2.14), we obtain

(3.9) A ( u k u , v k v ) S a p p s ( B ( u k u , v k v ) ) p p s .

So by combining (3.8) and (3.9), we obtain

A 1 ( u k u ) M 1 ( A 1 ( u ) ) + A 2 ( v k v ) M 2 ( A 2 ( v ) ) m S a p p s ( B ( u k u , v k v ) ) p p s .

By letting k tend to infinity, we conclude that

(3.10) b a n s p s ( m S ) n s p .

On the other hand, by ( H 3 ) , (3.6), and (3.10), one has

c = lim k J λ ( u k , v k ) = lim k J λ ( u k , v k ) 1 p s J λ ( u k , v k ) , ( u k , v k ) W = lim k 1 p ( M ^ 1 ( A 1 ( u k ) ) + M ^ 2 ( A 2 ( v k ) ) ) 1 p s A 1 ( u k ) M 1 ( A 1 ( u k ) ) 1 p s A 2 ( v k ) M 2 ( A 2 ( v k ) ) λ p s q p s C ( u k , v k ) lim k 1 θ 1 p A 1 ( u k ) M 1 ( A 1 ( u k ) ) + 1 θ 2 p A 2 ( v k ) M 2 ( A 2 ( v k ) ) 1 p s ( A 1 ( u k ) M 1 ( A 1 ( u k ) ) + A 2 ( v k ) M 2 ( A 2 ( v k ) ) ) λ p s q p s C ( u k , v k ) lim k 1 θ p 1 p s ( A 1 ( u k ) M 1 ( A 1 ( u k ) ) + A 2 ( v k ) M 2 ( A 2 ( v k ) ) ) λ p s q p s C ( u k , v k ) = lim k p s θ p θ p p s A 1 ( u k ) M 1 ( μ p ) + p s θ p θ p p s A 2 ( v k ) M 2 ( η p ) λ p s q p s C ( u k , v k ) = lim k p s θ p θ p p s ( A 1 ( u k u ) M 1 ( μ p ) + A 2 ( v k v ) M 2 ( η p ) ) + p s θ p θ p p s ( A 1 ( u ) M 1 ( μ p ) + A 2 ( v ) M 2 ( η p ) ) λ p s q p s C ( u k , v k ) = s n θ 1 θ p b + s n θ 1 θ p ( A 1 ( u ) M 1 ( μ p ) + A 2 ( v ) M 2 ( η p ) ) λ p s q p s C ( u , v ) s n θ 1 θ p b + s n θ 1 θ p ( m 1 A 1 ( u ) + m 2 A 2 ( v ) ) λ p s q p s C ( u , v ) s n θ 1 θ p a n s p s ( m S ) n s p + s n θ 1 θ p m A ( u , v ) λ p s q p s C ( u , v ) .

Now, from (2.15), and using the fact that θ p < p s , we obtain

(3.11) c s n θ 1 θ p a n s p s ( m S ) n s p + s n θ 1 θ p m A ( u , v ) λ γ S q p Ω p s q p s p s q θ p ( A ( u , v ) ) q p = s n θ 1 θ p a n s p s ( m S ) n s p + h ( A ( u , v ) ) ,

where h is defined on [ 0 , ) by

h ( ξ ) = s n θ 1 θ p m ξ λ γ S q p Ω p s q p s p s q θ p ξ q p .

A simple computation shows that h attains its minimum at

ξ 0 = λ q γ S q p Ω p s q p s p q m p 1 s n θ p ( θ 1 ) p p q ,

and

(3.12) inf ξ > 0 h ( ξ ) = h ( ξ 0 ) = λ p p q L ,

where L is given by (3.3).

Therefore, from (3.11), (3.12), and by considering θ 1 , we obtain

c s n θ 1 θ p a n s p s ( m S ) n s p λ p p q L s n θ 1 θ p a n s p s m S θ n s p λ p p q L .

This contradicts (3.4). Hence, b = 0 . So, we deduce that ( u k , v k ) ( u , v ) strongly in W . This completes the proof.□

Proposition 3.3

Assume that conditions ( H 2 ) and ( H 3 ) hold. Then, there exist λ > 0 , t 0 > 0 , and ( u 0 , v 0 ) W such that

(3.13) J λ ( t 0 u 0 , t 0 v 0 ) s n θ 1 θ p a n s p s m S θ n s p λ p p q L ,

provided that λ ( 0 , λ ) . In particular,

(3.14) α λ < s n θ 1 θ p a n s p s m S θ n s p λ p p q L .

Proof

We put

λ = 1 L s n θ 1 θ p a n s p s m S θ n s p p q p .

Then, for any 0 < λ < λ , we have

(3.15) s n θ 1 θ p a n s p s m S θ n s p λ p p q L > 0 .

By (3.1), there exist t 0 > 0 and ( u 0 , v 0 ) W \ { 0 } such that

(3.16) J λ ( t 0 u 0 , t 0 v 0 ) = 1 p ( M ^ 1 ( t 0 p A 1 ( u 0 ) ) + M ^ 2 ( t 0 p A 2 ( v 0 ) ) ) t 0 p p B ( u 0 , v 0 ) λ t 0 q C ( u 0 , v 0 ) = s n θ 1 θ p a n s p s m S θ n s p λ t 0 q C ( u 0 , v 0 ) .

Let

λ = t 0 q C ( u 0 , v 0 ) L , p q q .

Then, for all λ ( 0 , λ ) , we have

(3.17) λ t 0 q C ( u 0 , v 0 ) < λ p p q L .

Thus, from (3.16) and (3.17), we obtain

J λ ( t 0 u 0 , t 0 v 0 ) < s n θ 1 θ p a n s p s m S θ n s p λ p p q L .

Hence, (3.13) holds. Finally, if we put λ = min ( λ , λ , λ ) , then for all 0 < λ < λ and using the analysis of the fibering maps φ u , v ( t ) = J λ ( t u , t v ) , we obtain

α λ < s n θ 1 θ p a n s p s m S θ n s p λ p p q L .

This completes the proof of Proposition 3.2.□

Now, we are in a position to prove the main result of this article.

Proof of Theorem 1.1

By Lemma 2.4, J λ is bounded from below on N λ . Consequently, it is bounded from below on N λ + and N λ . So, we can find sequences { ( u k + , v k + ) } N λ + and { ( u k , v k ) } N λ , such that if k tends to infinity, then

J λ ( u k + , v k + ) inf ( u , v ) N λ + J λ ( u , v ) = α λ + ,

and

J λ ( u k , v k ) inf ( u , v ) N λ J λ ( u , v ) = α λ .

By an analysis of fibering maps φ u , v , we can conclude that α λ + < 0 and α λ > 0 . Moreover, by Propositions 3.2 and 3.3, we have

J λ ( u k + , v k + ) J λ ( u + , v + ) = inf ( u , v ) N λ + J λ ( u , v ) = α λ + , J λ ( u k + , v k + ) 0 ,

and

J λ ( u k , v k ) J λ ( u , v ) = inf ( u , v ) N λ J λ ( u , v ) = α λ , J λ ( u k , v k ) 0 .

Therefore, ( u + , v + ) (respectively, ( u , v ) ) is a minimizer of J λ on N λ + (respectively, on N λ ). Hence, by Lemma 2.1, problem (1.3) has two solutions ( u + , v + ) N λ + and ( u , v ) N λ . Moreover, since N λ + N λ = , it follows that these two solutions are distinct. Finally, the fact that α λ + < 0 and α λ > 0 imply that ( u + , v + ) and ( u , v ) are nontrivial solutions for problem (1.3). This completes the proof of Theorem 1.1.□


;

Acknowledgments

We thank the referees for their comments and suggestions.

  1. Funding information: D.D.R. was supported by the Slovenian Research Agency program P1-0292 and grants N1-0278, N1-0114, N1-0083, J1-4031, and J1-4001.

  2. Conflict of interest: The authors declare that they have no conflict of interest. D.D.R., who is an Honorary Member of the Advisory Board, declares to have no involvement in the decision process.

  3. Data availability statement: The authors declare that all data analyzed during this study are included in this published article.

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Received: 2022-07-07
Revised: 2023-02-18
Accepted: 2023-04-30
Published Online: 2023-06-13

© 2023 the author(s), published by De Gruyter

This work is licensed under the Creative Commons Attribution 4.0 International License.

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