Home Mathematics Existence, symmetry, and regularity of ground states of a nonlinear Choquard equation in the hyperbolic space
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Existence, symmetry, and regularity of ground states of a nonlinear Choquard equation in the hyperbolic space

  • Diksha Gupta EMAIL logo and Konijeti Sreenadh
Published/Copyright: December 4, 2025

Abstract

In this study, we explore the positive solutions of a nonlinear Choquard equation involving the Green kernel of the fractional operator ( Δ B N ) α 2 in the hyperbolic space, where Δ B N represents the Laplace-Beltrami operator on B N , with α ( 0 , N ) and N 3 . This study is analogous to the Choquard equation in the Euclidean space, which involves the nonlocal Riesz potential operator. We consider the functional setting within the Sobolev space H 1 ( B N ) , employing advanced harmonic analysis techniques, particularly the Helgason Fourier transform and semigroup approach to the fractional Laplacian. Moreover, the Hardy-Littlewood-Sobolev inequality on complete Riemannian manifolds, as developed by Varopoulos, is pivotal in our analysis. We prove an existence result for the problem ( F α , λ ) in the subcritical case. Moreover, we also demonstrate that solutions exhibit radial symmetry, and establish the regularity properties.

MSC 2020: 35B09; 35B38; 35J20; 35R01

1 Introduction

In this study, we explore the following nonlinear Choquard problem in the hyperbolic space B N :

Δ B N u λ u = ( Δ B N ) α 2 u p u p 2 u , u > 0 in B N and u λ ( B N ) , ( F α , λ )

where Δ B N denotes the Laplace-Beltrami operator on B N , λ ( N 1 ) 2 4 , 1 < p < 2 α * = N + α N 2 , 0 < α < N , N 3 , and λ ( B N ) denotes the completion of C 0 ( B N ) with respect to the norm mentioned in (2.4). Moreover, ( Δ B N ) α 2 is the Green kernel of the fractional operator, ( N 1 ) 2 4 is the bottom of the L 2 -spectrum of Δ B N , and 2 α * is the critical exponent in the context of the Hardy-Littlewood-Sobolev (HLS) inequality.

The equation when posed in R N bears a notable resemblance to the Choquard equation, thoroughly explored by Moroz and Schaftingen [37]. The equation is given as follows:

(1.1) Δ u + u = ( I α * u p ) u p 2 u in R N ,

where I α denotes the Riesz potential, α ( 0 , N ) , and p > 1 . The Riesz potential I α : R N R is defined as

I α ( x ) = Γ N α 2 Γ α 2 π N 2 2 α x N α ,

with Γ representing the Euler gamma function. To draw a connection between equation (1.1) and the one explored in this article, it is useful to view the Riesz potential as a representation of the inverse fractional Laplacian. In mathematical physics, the Newtonian potential of a function f S ( R N ) is defined as

I 2 ( f ) ( x ) = 1 4 π N 2 Γ N 2 2 R N f ( y ) x y N 2 d y ,

where S ( R N ) denotes the Schwartz space of rapidly decreasing functions in R N . The convolution kernel 1 4 π N 2 Γ N 2 2 1 x N 2 appearing in I 2 ( f ) matches the fundamental solution

u ( x ) = 1 ( N 2 ) ω N 1 1 x N 2

of Δ where ω N 1 is the surface area of the unit sphere in R N . Extending this idea, the generalization of the Newtonian potential indicates that for any function f S ( R N ) , in the distributional space S ( R N ) , we have I α ( Δ ) α 2 f = ( Δ ) α 2 I α f = f , where ( Δ ) α 2 can be defined in several equivalent ways [11,25].

These partial differential equations (PDEs) are not just fascinating from a purely mathematical perspective but they also show up in various physical scenarios. For example, they appear in models like the Einstein-Klein-Gordon and Einstein-Dirac systems [20]. In practical applications like nonlinear optics and Bose-Einstein condensates, similar equations help describe how waves or particle densities evolve when both linear and nonlinear effects are at play. The Choquard equation is particularly interesting because it deals with nonlocal interactions, meaning the behavior at any point in the system is influenced by the entire field. Particularly, the following Choquard equation:

Δ u + u = ( I 2 * u 2 ) u in R 3 , u H 1 ( R 3 )

originally stems from the work of Frohlich and Pekar on polarons. They studied how free electrons in an ionic lattice interact with photons or the polarization they cause, essentially depicting an electron interacting with its own induced hole [1416]. In 1976, Ph. Choquard adapted this model to explain a one-component plasma, showing its broader relevance in plasma physics. Interestingly, the Choquard equation is also known as the Schrödinger-Newton equation when it combines quantum mechanics with Newtonian gravity [24,35,41,42].

The Choquard equation in R N has been the focus of extensive research, particularly concerning the existence and qualitative properties of its solutions. Moroz and Schaftingen [37] established the existence of solutions to (1.1) by employing variational methods with the concentration-compactness lemma of P.L. Lions. The HLS inequality in R N [29] is heavily utilized in these techniques. Furthermore, in [38], they examined a more generalized form of the Choquard equation. In a subsequent study, Moroz and Schaftingen [40] considered the equation with a potential, establishing the existence of solutions for the lower critical exponent corresponding to the HLS inequality. Gao and Yang [19] also contributed by studying the Brezis-Nirenberg type Choquard equation within a bounded domain. For additional related works, refer [12,13,33,39,4750].

Recent research has extensively aimed to generalize elliptic equations to non-Euclidean domains, driven by their relevance to various physical phenomena. This exploration seeks to understand how curvature impacts the behavior and properties of the solutions. We refer to [6,9,17,23,27] and references cited therein, without any claim of completeness. Notably, Sandeep and Mancini’s seminal work [34] demonstrated the existence and uniqueness of finite-energy positive solutions for the homogeneous elliptic equation

(1.2) Δ B N u λ u = u p , u H 1 ( B N ) ,

where λ ( N 1 ) 2 4 , 1 < p N + 2 N 2 if N 3 ; 1 < p < if N = 2 . They demonstrated that, for the subcritical case and p > 1 , equation (1.2) has a positive solution if and only if λ < ( N 1 ) 2 4 , and that this solution is unique up to hyperbolic isometries, except potentially for N = 2 and λ > 2 ( p + 1 ) ( p + 3 ) 2 . Following their work, researchers of [6,17,18] examined the existence of sign-changing solutions, compactness, and nondegeneracy, while [5,7] focused on infinite energy solutions and their asymptotic behavior. Sandeep and Mancini also found that equation (1.2) emerges naturally when analyzing Euler-Lagrange equations related to Hardy-Sobolev-Maz’ya (HSM) inequalities. They derived a sharp Poincaré-Sobolev inequality (2.2) in hyperbolic space, which has spurred further interest in analogous HSM inequalities [36] involving higher-order derivatives [31,32]. Li et al. [27] have thereafter explored the existence, nonexistence, and symmetry of solutions for the higher-order Brezis-Nirenberg problem in hyperbolic space. This work relies on complex estimations of Green’s functions for fractional Laplacians, Helgason-Fourier analysis, and HLS inequality in the hyperbolic spaces. Specifically, the HLS inequality in hyperbolic space can be stated as follows: For 0 < λ < N and p = 2 N 2 N λ , if f , g L p ( B N ) ,

B N B N f ( x ) g ( y ) 2 sinh ρ ( T y ( x ) ) 2 λ d V B N ( x ) d V B N ( y ) C N , λ f p g p ,

where T y ( x ) denotes Möbius transformation, ρ denotes the hyperbolic distance (see Section 2), and

C N , λ = π λ 2 Γ ( N 2 λ 2 ) Γ ( N λ 2 ) Γ ( N 2 ) Γ ( N ) 1 + λ N

is the best HLS constant on R N . This constant is sharp, and there are no nonzero extremal functions. This result can be easily derived from the HLS inequality in R N through a conformal change in metric to the Euclidean ball [31]. Furthermore, this inequality parallels the HLS inequality in R N for the specific case when p = r = 2 N N λ , as stated in Theorem 4.3 of [29]. The presence of sinh ρ 2 in the hyperbolic space context is attributed to the Green’s function associated with the conformal Laplacian Δ B N N ( N 2 ) 4 [32]. Furthermore, Theorem 2.13 states a generalized form of the HLS inequality for any complete Riemannian manifold, under an additional assumption regarding the heat kernel.

In light of the aforementioned HLS inequality, He [23] examines an equation in the hyperbolic space that is analogous to the Choquard equation in R N . The study demonstrates the existence of a positive solution in the subcritical range, specifically for N + α N < p < N + α N 2 under the condition λ ( N 1 ) 2 4 , and also for p = N + α N 2 when N ( N 2 ) 4 < λ ( N 1 ) 2 4 . Interestingly, the upper critical exponent N + α N 2 resembles the critical Sobolev exponent 2 N N 2 that appears in the Brezis-Nirenberg problem, while the exponent N + α N naturally emerges from the application of the HLS inequality.

Inspired by the aforementioned problems and the general HLS inequality (2.13) on a complete Riemannian manifold, we have investigated the problem ( F α , λ ) in this article. The derivation of this inequality relies on Stein’s maximal ergodic theorem. A significant challenge while analyzing problems like ( F α , λ ) is the loss of compactness, even in the subcritical range, as the embedding H 1 ( B N ) L p ( B N ) is noncompact for any 2 p 2 N N 2 . This issue arises from the hyperbolic isometries in the infinite volume space B N . In Euclidean spaces, such challenges are typically addressed by dilating a given sequence, but this approach is ineffective in B N due to the equivalence of its conformal and isometry groups. To address this, we employ a concentration function approach near infinity. Another complexity arises from the nonlocal nature of the problem, driven by the Green kernel of the fractional operator. In addition to these, several technical challenges emerge in this context. These include the nonlinear nature of hyperbolic translations (as described in Section 2.1) and the complexity of the semigroup formula for the inverse fractional Laplacian, which involves the heat kernel in hyperbolic space. Unlike the Euclidean case, where the heat kernel is given by G t ( x ) = 1 ( 4 π t ) N 2 e x 2 4 t , x R N , t > 0 , the heat kernel in hyperbolic space is far more complex (refer Section 2.5). To the best of our knowledge, the problem described by ( F α , λ ) has not been studied in the literature to date.

The problem ( F α , λ ) can be analyzed using variational methods, thanks to the HLS inequality (2.14). To establish the existence of finite energy solutions, it is essential to examine the energy functional associated with (1.2), defined by

( u ) = B N [ B N u ( x ) 2 λ u 2 ( x ) ] d V B N B N ( Δ B N ) α 2 u p u p d V B N 1 p , u λ ( B N ) \ { 0 } ,

for N + α N p N + α N 2 and the space λ ( B N ) defined in Section 2. We establish the following main existence result for p within the subcritical range.

Theorem 1.1

Let 0 < α < N and N + α N < p < 2 α * = N + α N 2 for N 3 . Then, ( F α , λ ) possesses a positive solution for any λ ( N 1 ) 2 4 .

To prove the above theorem, we demonstrate the existence of a minimizer for the energy functional on the associated Nehari manifold. This proof hinges on a concentration-compactness argument at infinity and the fact that the equation under consideration is invariant under the isometry group in hyperbolic space. This minimizer is referred to as a ground state. To establish the radial symmetry of the solutions, we utilize a symmetrization argument. This method is particularly effective in Choquard-type problems due to the presence of a Polya-Szego-like inequality, which implies a strong symmetrization effect on the nonlocal term. By using the minimality of the ground state, we derive a relationship between the function and its polarization, thereby establishing radial symmetry. Finally, we obtain certain regularity results through classical bootstrap arguments.

Remark 1.1

It is not trivial to establish a nonexistence result analogous to [37, Theorem 2] in the critical case using the Pohožaev identity argument due to the nonlinear nature of the hyperbolic translation (2.1) involved in the definition of ( Δ B N ) α 2 (2.12). Nevertheless, by first deriving some a priori asymptotic estimates, one can prove the nonexistence of solutions for p = N + α N 2 and λ N ( N 2 ) 4 .

The study is structured as follows: Section 2 introduces key notations and geometric definitions, along with preliminary concepts related to the hyperbolic space. Section 3 presents the proof of Theorem 1.1. In Section 4, we state and prove the result concerning radial symmetry, while Section 5 addresses the regularity results. Numerous positive constants, whose specific values are irrelevant, are denoted by C .

2 Preliminaries

In this section, we will introduce some of the notations and definitions used in this study and also recall some of the embeddings related to the Sobolev space on the hyperbolic space.

We will denote by B N the disc model of the hyperbolic space, i.e., the Euclidean unit ball B ( 0 , 1 ) { x R N : x 2 < 1 } equipped with the Riemannian metric

d s 2 = 2 1 x 2 2 d x 2 ,

where d x is the standard Euclidean metric and x 2 = i = 1 N x i 2 is the standard Euclidean length. The corresponding volume element is given by d V B N = ( 2 1 x 2 ) N d x , where d x denotes the Lebesgue measure on B N . B N and Δ B N denote the gradient vector field and Laplace-Beltrami operator, respectively. Therefore, in terms of local (global) coordinates, B N and Δ B N take the form

B N = 1 x 2 2 2 , Δ B N = 1 x 2 2 2 Δ + ( N 2 ) 1 x 2 2 x ,

where , Δ are the standard Euclidean gradient vector field and Laplace operator, respectively, and “ ” denotes the standard inner product in R N .

2.1 Möbius transformations and convolution

[30] The Möbius transformations T a for each a B N are defined as follows:

(2.1) T a ( x ) = x a 2 a ( 1 a 2 ) ( x a ) 1 2 x a + x 2 a 2 ,

where x a = x 1 a 1 + x 2 a 2 + + x n a n represents the scalar product in R N . The measure on B N is known to be invariant under Möbius transformations.

The convolution of measurable functions f and g on B N can be defined using the Möbius transformations as follows:

( f * g ) ( x ) = B N f ( y ) g ( T x ( y ) ) d V B N ( y )

provided this integral exists. It is straightforward to verify that

f * g = g * f .

2.2 Hyperbolic distance on B N

The distance between x and y in B N can be defined as follows utilizing the Möbius transformations:

ρ ( x , y ) = ρ ( T x ( y ) ) = ρ ( T y ( x ) ) = log 1 + T y ( x ) 1 T y ( x )

where ρ ( x ) = d ( x , 0 ) = log 1 + x 1 x is the geodesic distance from the origin.

As a result, a subset of B N is a hyperbolic sphere in B N if and only if it is a Euclidean sphere in R N and contained in B N , possibly with a different center and different radius, which can be explicitly computed from the formula of d ( x , y ) [44]. Geodesic balls in B N of radius r centered at x B N will be denoted by

B r ( x ) { y B N : d ( x , y ) < r } .

Additionally, if g is radial, meaning g = g ( ρ ) , then for f , g , h L 1 ( B N ) , we have

( f * g ) * h = f * ( g * h ) .

2.3 Sharp Poincaré-Sobolev inequality

(Refer [34])

Sobolev space: We will denote by H 1 ( B N ) the Sobolev space on the disc model of the hyperbolic space B N , equipped with norm u = B N B N u 2 1 2 , where B N u is given by B N u B N u , B N u B N 1 2 .

For N 3 and every p 1 , N + 2 N 2 , there exists an optimal constant S λ , p > 0 such that

(2.2) S λ , p B N u p + 1 d V B N 2 p + 1 B N B N u 2 ( N 1 ) 2 4 u 2 d V B N ,

for every u C 0 ( B N ) . If N = 2 , then any p > 1 is allowed.

A crucial point to note is that the bottom of the spectrum of Δ B N on B N is

(2.3) ( N 1 ) 2 4 = inf u H 1 ( B N ) \ { 0 } B N B N u 2 d V B N B N u 2 d V B N .

Remark 2.1

As a result of (2.3), if λ < ( N 1 ) 2 4 , then

(2.4) u λ B N ( B N u 2 λ u 2 ) d V B N 1 2 , u C 0 ( B N )

is a norm, equivalent to the H 1 ( B N ) norm. When λ = ( N 1 ) 2 4 , the sharp Poincaré inequality (2.2) ensures that u ( N 1 ) 2 4 is also a norm on C 0 ( B N ) .

For λ ( N 1 ) 2 4 , denote by λ ( B N ) the completion of C 0 ( B N ) with respect to the norm u λ . The associated inner product is denoted by , λ . Note that

S λ , p u p + 1 d V B N 2 p + 1 u λ , p 1 , N + 2 N 2 for u λ ( B N ) .

Additionally, throughout this article, r denotes the L r -norm with respect to the volume measure for 1 r .

2.4 Helgason Fourier transform on the hyperbolic space

Now, we will make sense of the Green kernel of the fractional operator used in ( F α , λ ). To this aim we shall use the Helgason Fourier transform as follows (for further details, refer [2,30] and references therein).

Analogous to the Euclidean context, the Fourier transform can be defined as follows:

f ˆ ( β , θ ) = B N f ( x ) h β , θ ( x ) d V B N ,

for β R , θ S N 1 , where h β , θ are the generalized eigenfunctions of the Laplace-Beltrami operator that satisfies

Δ B N h β , θ = β 2 + ( N 1 ) 2 4 h β , θ .

Furthermore, given f C 0 ( B N ) , the following inversion formula is valid:

f ( x ) = S N 1 h ¯ β , θ ( x ) f ˆ ( β , θ ) d θ d β c ( β ) 2 ,

where c ( β ) represents the Harish-Chandra coefficient

1 c ( β ) 2 = 1 2 Γ N 1 2 2 Γ ( N 1 ) 2 Γ i β + N 1 2 2 Γ ( i β ) 2 .

Moreover, the following Plancherel formula holds:

B N f ( x ) 2 d V B N = R × S N 1 f ˆ ( β , θ ) 2 d θ d β c ( β ) 2 .

It is straightforward to verify through integration by parts for compactly supported functions, and thus, for every f L 2 ( B N ) that

(2.5) Δ B N f ^ ( β , θ ) = B N Δ B N f ( x ) h β , θ ( x ) d V B N ( x ) = B N f ( x ) Δ B N h β , θ ( x ) d V B N ( x ) = β 2 + ( N 1 ) 2 4 f ˆ ( β , θ ) .

Given the theory discussed above, the fractional Laplacian on the hyperbolic space can be defined as ( Δ B N ) γ f , which is the operator satisfying

( Δ B N ^ ) γ f = β 2 + ( N 1 ) 2 4 γ f ˆ , γ R .

However, to derive an explicit pointwise expression for the inverse Laplacian, we will utilize the following semigroup framework. To start, we introduce some notations related to the heat kernel in the hyperbolic space.

2.5 Semigroup approach to the fractional Laplacian

Consider the function u = u ( x , t ) , defined for x B N and t 0 , which solves the heat equation over the entire space B N with initial condition f

t u ( x , t ) = Δ B N u ( x , t ) , ( x , t ) B N × R + , u ( x , 0 ) = f ( x ) C 0 ( B N ) ,

where, for convenience, u ( x , t ) is considered to be C and compactly supported in the spatial variable.

For every fixed t , when we apply the Fourier transform in the variable x and use (2.5), we obtain

t u ˆ ( β , θ , t ) = β 2 + ( N 1 ) 2 4 u ˆ ( β , θ , t ) , for t > 0 , u ˆ ( β , θ , 0 ) = f ˆ ( β , θ ) ,

which yields

u ˆ ( β , θ , t ) = e t β 2 + ( N 1 ) 2 4 f ˆ ( β , θ ) = e t Δ B N f ( β , θ ) ^ .

where f e t Δ B N f denotes the solution operator. It is well-established [30] that

u ( x , t ) e t Δ B N f ( x ) = p t , N * f ( x ) = B N p t , N ( T x ( y ) ) f ( y ) d V B N ( y ) ,

where p t , N ( x , y ) = p t , N ( ρ ( x , y ) ) is the heat kernel on B N . The explicit formulas of heat kernel are given by [30, Theorem 7.3], [21].

If N = 2 m + 1 , then

p t , 2 m + 1 ( ρ ) = 2 m 1 π m 1 2 t 1 2 e ( N 1 ) 2 4 t 1 sinh ρ ρ m e ρ 2 4 t .

If N = 2 m , then

p t , 2 m ( ρ ) = ( 2 π ) m 1 2 t 1 2 e ( N 1 ) 2 4 t ρ + sinh r cosh r cosh ρ 1 sinh r r m e r 2 4 t d r .

Numerous researchers have investigated bounds for the heat kernel. For instance, Punzo [43, Proposition 2.2] derived the L estimate, which helps in establishing the HLS inequality in the hyperbolic space (refer Theorem 2.2). Additionally, the heat kernel p t , N satisfies the following bounds [10]: for N 2 , there exist positive constants A N and B N such that

(2.6) A N h N ( t , x , y ) p t , N ( x , y ) B N h N ( t , x , y ) for all t > 0 and x , y B N ,

where h N ( t , x , y ) is defined as

h N ( t , x , y ) h N ( t , r ) = ( 4 π t ) N 2 e ( N 1 ) 2 t 4 ( N 1 ) r 2 r 2 4 t ( 1 + r + t ) ( N 3 ) 2 ( 1 + r ) ,

with r r ( x , y ) = dist ( x , y ) .

We can now establish the semigroup definition of the inverse fractional Laplacian, derived from the following numerical identity:

ζ γ = 1 Γ ( γ ) 0 e t ζ d t t 1 γ for any ζ > 0 , γ > 0 .

Setting ζ = β 2 + ( N 1 ) 2 4 and multiplying the equation by f ˆ ( β , θ ) , we obtain

β 2 + ( N 1 ) 2 4 γ f ˆ ( β , θ ) = 1 Γ ( γ ) 0 f ˆ ( β , θ ) e t β 2 + ( N 1 ) 2 4 d t t 1 γ .

Taking the inverse transform then yields

( Δ B N ) γ f ( x ) = 1 Γ ( γ ) S N 1 h ¯ β , θ ( x ) 0 f ˆ ( β , θ ) e t β 2 + ( N 1 ) 2 4 d t t 1 γ d θ d β c ( β ) 2 = 1 Γ ( γ ) 0 S N 1 h ¯ β , θ ( x ) f ˆ ( β , θ ) e t β 2 + ( N 1 ) 2 4 d θ d β c ( β ) 2 d t t 1 γ = 1 Γ ( γ ) 0 S N 1 h ¯ β , θ ( x ) e t Δ B N f ( β , θ ) ^ d θ d β c ( β ) 2 d t t 1 γ = 1 Γ ( γ ) 0 e t Δ B N f ( x ) d t t 1 γ .

Up to this point, we have developed the above heuristics for functions f C 0 ( B N ) . Next we aim to identify a class of functions for which the aforementioned integral converges. To this end, we define the function f * ( x ) = sup t > 0 e t Δ B N f ( x ) for f L p ( B N ) , where 1 < p < . Note that f * is a well-defined measurable function, as established in [45]. We now present the following result regarding the convergence of the integral.

Theorem 2.1

Suppose N > 0 , 0 < α < N , and 1 < p < N α , with f L p ( B N ) . Then,

(2.7) ( Δ B N ) α 2 f ( x ) 1 Γ ( α 2 ) 0 e t Δ B N f ( x ) d t t 1 α 2

is convergent.

Before proving this theorem, we establish the following on-diagonal and off-diagonal estimates for the heat kernel on the hyperbolic space.

Using (2.6), we have

(2.8) p t , N ( x , x ) B N ( 4 π t ) N 2 e ( N 1 ) 2 t 4 ( 1 + t ) ( N 3 ) 2 B N ( 4 π t ) N 2 e ( N 1 ) 2 t 4 e t ( N 3 ) 2 B N ( 4 π t ) N 2 e t ( ( N 2 ) 2 + 3 ) 4 C t N 2 t > 0 .

Further, recall the following semigroup property of the heat kernel:

(2.9) p t + s , N ( x , y ) = B N p t , N ( x , z ) p s , N ( z , y ) d V B N ( z )

for x , y B N and t , s > 0 .

Specifically, by setting y = x and s = t in (2.9) and noting the radial nature of the heat kernel, we obtain

(2.10) p 2 t , N ( x , x ) = B N ( p t , N ( x , z ) ) 2 d V B N ( z ) .

By combining (2.8) and (2.10), we can deduce that p t , N ( x , y ) L 2 ( B N ) as a function of y .

Thus, using (2.9), (2.10), and (2.8), we have for t > 0

p t , N ( x , y ) = B N p t 2 , N ( x , z ) p t 2 , N ( z , y ) d V B N ( z ) B N p t 2 , N ( x , z ) d V B N ( z ) 2 1 2 B N p t 2 , N ( y , z ) d V B N ( z ) 2 1 2 = ( p t , N ( x , x ) ) 1 2 ( p t , N ( y , y ) ) 1 2 C t N 2 x , y B N .

We now present the necessary tools to establish Theorem 2.1.

Proof of Theorem 2.1

Fix x B N , and consider the integral in (2.7)

1 Γ ( α 2 ) 0 e t Δ B N f ( x ) d t t 1 α 2 = 0 1 P + 1 Q .

Due to estimate (2.8), we can apply Proposition 2.2 from [43] to obtain

e t Δ B N f ( x ) C 1 p t N 2 p f p .

Using this estimate, we have

Q C 1 p Γ ( α 2 ) f p 1 + t α 2 N 2 p 1 d t = 2 C 1 p f p ( N α p ) Γ ( α 2 ) < .

Finally,

P = 1 Γ ( α 2 ) 0 1 e t Δ B N f ( x ) d t t 1 α 2 1 Γ ( α 2 ) 0 1 t α 2 1 f * ( x ) d t = 2 α 1 Γ ( α 2 ) f * ( x ) < ,

which completes the proof.□

For simplicity, we define

(2.11) k α , N ( ρ ) = 1 Γ ( α 2 ) 0 p t , N ( ρ ) d t t 1 α 2 .

Then,

(2.12) ( Δ B N ) α 2 f ( x ) = k α , N * f ( x ) .

To establish the finiteness of the energy functional associated with ( F α , λ ), we will rely on the following HLS inequality in the hyperbolic space. This connection between HLS theory and heat kernel estimates is attributed to Varopoulos.

Theorem 2.2

(HLS inequality) Let ( M , g ) be a complete Riemannian manifold with dimension N 1 , and let L denote the Laplace-Beltrami operator on M , 0 < α < N , and 1 < s < N α . If there exists a constant C > 0 such that for all t > 0 and for every x , y M ,

p ( x , y , t ) C t N 2 ,

where p ( x , y , t ) represents the heat kernel associated with the semigroup corresponding to L. Then, for every function f L μ s ( M ) , the following inequality holds:

(2.13) ( L ) α 2 f N s N s α C ˜ ( N , α , s ) f s ,

where

(2.14) C ˜ ( N , α , s ) = s s 1 1 α N 2 N C α N α ( N s α ) Γ ( α 2 ) .

For a detailed proof of this theorem, refer [4].

3 Existence

To establish the proof of Theorem 1.1, we recall the energy functional associated with ( F α , λ ), which is defined as

( u ) = B N B N u ( x ) 2 λ u 2 ( x ) d V B N B N ( Δ B N ) α 2 u p u p d V B N 1 p , u λ ( B N ) \ { 0 } ,

and

ζ = inf u λ ( B N ) \ { 0 } ( u ) .

Observe that, owing to Theorem 2.2, the functional ( u ) is well-defined. For u λ ( B N ) , it suffices to ensure the finiteness of the integral in the denominator of ( u ) . By applying Hölder’s inequality and Theorem 2.2 with s = 2 N N + α , we obtain

B N ( Δ B N ) α 2 u p u p d V B N B N ( Δ B N ) α 2 u p 2 N N α d V B N N α 2 N B N u 2 N p N + α d V B N N + α 2 N C ( N , α ) B N u 2 N p N + α d V B N N + α N ,

where C ( N , α ) = C ˜ ( N , α , 2 N N + α ) is defined in (2.14). Therefore, the integral

B N ( Δ B N ) α 2 u p u p d V B N

is well-defined as u p L 2 N N + α ( B N ) . This is guaranteed by the assumptions u λ ( B N ) , the range of p , i.e., N + α N p 2 α * = N + α N 2 , and the sharp Poincaré-Sobolev inequality.

Observe that ( F α , λ ) is invariant under the isometry group of B N , which is identical to its conformal group. To demonstrate the existence result using a concentration-compactness type argument, define for r > 0 ,

S r = { x R N : x 2 = 1 + r 2 } ,

and for a S r , define

A ( a , r ) = B ( a , r ) B N ,

where B ( a , r ) is the open ball in the Euclidean space with center a and radius r > 0 . Moreover, for the choice of a and r , B ( a , r ) is orthogonal to S N 1 . Let us recall a lemma from [6] before proving the theorem.

Lemma 3.1

Let r 1 > 0 and r 2 > 0 , and let A ( a i , r i ) for i = 1 , 2 be as defined above. Then, there exists τ I ( B N ) such that τ ( A ( a 1 , r 1 ) ) = A ( a 2 , r 2 ) , where I ( B N ) is the isometry group of B N .

Before proceeding to the main result, we establish the following variant of the Brezis-Lieb lemma [3].

Lemma 3.2

Consider 0 < α < N and N + α N < p < N + α N 2 . Suppose { u n } is a bounded sequence in L 2 N p N + α ( B N ) such that u n u almost everywhere in B N as n . Then, we have

lim n B N ( Δ B N ) α 2 u n p u n p d V B N B N ( Δ B N ) α 2 u n u p u n u p d V B N = B N ( Δ B N ) α 2 u p u p d V B N .

Proof

First, observe that

(3.1) B N ( Δ B N ) α 2 u n p u n p d V B N B N ( Δ B N ) α 2 u n u p u n u p d V B N = B N ( Δ B N ) α 2 ( u n p u n u p ) ( u n p u n u p ) d V B N + 2 B N ( Δ B N ) α 2 ( u n p u n u p ) u n u p d V B N .

Next, since u n L 2 N p N + α ( B N ) , by the Brezis-Lieb lemma, we have

(3.2) u n u p u n p u p in L 2 N N + α ( B N ) .

By employing the HLS inequality (2.13) along with (3.2), we derive the following:

(3.3) B N ( Δ B N ) α 2 ( u n p u n u p ) ( u n p u n u p ) d V B N B N ( Δ B N ) α 2 u p u p d V B N = B N ( Δ B N ) α 2 ( u n p u n u p u p ) ( u n p u n u p ) d V B N + B N ( Δ B N ) α 2 ( u p ) ( u n p u n u p u p ) d V B N 0 .

Furthermore, for u n L 2 N p N + α ( B N ) with u n ( x ) u ( x ) a.e. in B N , we have

(3.4) u n u p 0 weakly in L 2 N N + α ( B N ) .

Consider now the following integral:

(3.5) B N ( Δ B N ) α 2 ( u n p u n u p ) u n u p d V B N = B N ( Δ B N ) α 2 ( u n p u n u p u p ) u n u p d V B N + B N ( Δ B N ) α 2 u p u n u p d V B N 0 ,

which follows from (2.13), (3.2), and (3.4).

By combining (3.1), (3.3), and (3.5), we arrive at the desired conclusion.□

Lemma 3.3

Let 0 < α < N and N + α N < p < 2 α * = N + α N 2 if N 3 . Then, for λ ( N 1 ) 2 4 , ζ is attained by some nonnegative function in λ ( B N ) .

Proof

The associated Nehari manifold is defined as

N u λ ( B N ) : u λ 2 = B N ( Δ B N ) α 2 u p u p d V B N , u 0 .

It is straightforward to see that

ζ = inf u λ ( B N ) \ { 0 } ( u ) = inf u N ( u ) .

By utilizing the HLS inequality (2.13) and the Poincaré-Sobolev inequality (2.2), we obtain

(3.6) ζ ( C ( N , α ) ) 1 p S λ , 2 N p N + α > 0 .

We assert that ζ is attained.

Let { u n } be a minimizing sequence for ζ in N , meaning

(3.7) u n λ 2 ( p 1 ) p = B N ( Δ B N ) α 2 u n p u n p d V B N p 1 p ζ as n .

It is evident that { u n } is bounded in λ ( B N ) by some constant M > 0 . Consequently, we can assume, up to a subsequence, that u n u weakly in H λ ( B N ) . To demonstrate that ζ is attained, it suffices to show that { u n } converges weakly, and pointwise, to some u N up to the isometry group of B N .

The proof will be divided into the following steps:

Step 1: The goal of this step is to identify a sequence of translations to restore compactness. Since { u n } is a minimizing sequence for ζ , and in light of (3.6) and (3.7), u n does not strongly converge to zero. Therefore, we have

liminf n B N ( Δ B N ) α 2 u n p u n ( x ) p d V B N > δ 1 > 0 .

By applying the HLS inequality (2.2), it follows that

liminf n B N u n 2 N p N + α d V B N > δ 2 > 0 .

Choose a positive constant δ such that

0 < 2 δ < δ 2 < ( C ( N , α ) ) 1 S λ , 2 N p N + α 1 + p 2 M p 2 p 2 N p N + α .

Define the concentration function Q n : ( 0 , + ) R by

Q n ( r ) = sup x S r A ( x , r ) u n 2 N p N + α d V B N .

It follows that lim r 0 Q n ( r ) = 0 and lim r Q n ( r ) > δ . Therefore, we can find R n > 0 and x n S R n such that

sup x S R n A ( x , R n ) u n 2 N p N + α d V B N = A ( x n , R n ) u n 2 N p N + α d V B N = δ .

Fix x 0 S 3 , use Lemma 3.1 to select isometry T n I ( B N ) such that A ( x n , r n ) = T n A ( x 0 , 3 ) for all n .

Step 2: This step aims to locate the candidate for the minimizer.

Define v n ( x ) = u n T n ( x ) . With T n being an isometry, it is trivial to observe that { v n ( x ) } N and remains a minimizing sequence, i.e.,

v n λ 2 ( p 1 ) p = B N ( Δ B N ) α 2 v n p v n p d V B N p 1 p ζ as n .

Furthermore,

(3.8) A ( x 0 , 3 ) v n 2 N p N + α d V B N = A ( x n , R n ) u n 2 N p N + α d V B N = δ = sup x S 3 A ( x , 3 ) v n 2 N p N + α d V B N .

Following the Ekeland principle, we can assume that the sequence { v n } is a Palais-Smale sequence. Specifically,

(3.9) v n , w λ = B N ( Δ B N ) α 2 v n p v n ( x ) p 2 v n ( x ) w d V B N + o n ( 1 ) w for w λ ( B N ) ,

where o n ( 1 ) 0 as n in λ . Consequently, up to a subsequence, we may assume v n v in λ ( B N ) . Furthermore, due to this weak convergence and the continuity of the functional u J ( u ) where J ( u ) = B N ( Δ B N ) α 2 u p u p d V B N , it is not difficult to deduce that

v λ 2 = B N ( Δ B N ) α 2 v p v p d V B N .

Thus, it remains to show that v 0 to conclude that v N .

Step 3: Assume, if possible, that v 0 . We propose that for any 1 > r > 2 3 ,

B N { x r } v n 2 N p N + α d V B N = o ( 1 ) .

To establish this, select a point a S 3 . Define Φ C 0 ( A ( a , 3 ) ) such that 0 Φ 1 , and substitute w = Φ 2 v n in (3.9). This yields

B N B N v n B N ( Φ 2 v n ) λ v n Φ 2 v n d V B N = B N ( Δ B N ) α 2 v n p v n p 2 v n Φ 2 v n d V B N + o ( 1 ) .

Using local compact embedding, we simplify the left-hand side (LHS) of the above expression as in ([6, pg. 255])

v n , ϕ 2 v n λ = ϕ v n λ 2 + o ( 1 ) .

Thus, combining the two expressions above gives

(3.10) B N B N ( Φ v n ) 2 λ ( Φ v n ) 2 d V B N = B N ( Δ B N ) α 2 v n p v n p 2 ( Φ v n ) 2 d V B N + o ( 1 ) .

Using (3.10), along with the Hölder’s inequality, the HLS inequality (2.2), and the Poincaré-Sobolev inequality, we derive

S λ , 2 N p N + α B N Φ v n 2 N p N + α d V B N 2 2 N p N + α C ( N , α ) B N v n 2 N p N + α d V B N N + α 2 N B N [ v n p 2 ( v n Φ ) 2 ] 2 N N + α d V B N N + α 2 N C ( N , α ) S λ , 2 N p N + α p 2 u n λ p B N [ v n p 2 ( v n Φ ) 2 ] 2 N N + α d V B N N + α 2 N C ( N , α ) S λ , 2 N p N + α p 2 M p B N Φ v n 2 N p N + α d V B N 2 p N + α 2 N A ( a , 3 ) v n 2 N p N + α d V B N p 2 p N + α 2 N .

Now, if

B N Φ v n ( x ) 2 N p N + α d V B N ( x ) 0 ,

we have

δ p 2 p N + α 2 N > A ( a , 3 ) v n 2 N p N + α d V B N p 2 p N + α 2 N ( C ( N , α ) ) 1 S λ , 2 N p N + α 1 + p 2 M p > δ p 2 p N + α 2 N ,

which is a contradiction. Therefore,

B N Φ v n ( x ) 2 N p N + α d V B N ( x ) 0 .

Since a S 3 is arbitrary, the claim is proven.

Since the condition N + α N < p < N + α N 2 ensures that v n 0 in L loc 2 N p N + α ( B N ) , this, combined with the previous assertion, directly contradicts (3.8). Consequently, we conclude that v 0 and v N .□

Thus, the proof of Theorem 1.1 is straightforwardly derived from the preceding theorem and the application of the maximum principle.

4 Radial symmetry

The objective of this section is to demonstrate the hyperbolic symmetry of ground states. Specifically, we will prove the following result.

Proposition 4.1

Let 0 < α < N and N + α N p 2 α * = N + α N 2 for N 3 . If u λ ( B N ) is a positive ground state of ( F α , λ ), then there exists a point x 0 B N and a function v : ( 0 , ) R , which is nonnegative and nonincreasing, such that for almost every x B N

u ( x ) = v ( d ( x , x 0 ) ) .

To demonstrate the radial symmetry, we will utilize the polarization technique, which is also referred to as the method of symmetrization or rearrangement. To facilitate this, we first introduce some notations for use throughout this section. Fix an origin e in B N . Let H B N be a closed, totally geodesic hypersurface such that e H . The components of B N \ H are denoted as H + and H , where H + contains e and H does not. Let σ H : B N B N represent the reflection w.r.t H . Specifically, σ H is an isometry of B N , satisfying σ H 2 = I d , σ H ( x ) = x for x H , and σ H H + = H [1].

For a function f : B N R , we define its polarization by f H : B N R as follows:

f H ( x ) = f ( x ) , if x H , max ( f ( x ) , f ( σ H ( x ) ) ) , if x H + , min ( f ( x ) , f ( σ H ( x ) ) ) , if x H .

An initial step is to explore how polarization affects the nonlocal term and to analyze the equality cases.

Lemma 4.1

Let α ( 0 , N ) , u L 2 N N + α ( B N ) , and H B N be a closed, totally geodesic hypersurface. If u 0 and

B N ( Δ B N ) α 2 u ( y ) u ( y ) d V B N ( y ) B N ( Δ B N ) α 2 u H ( y ) u H ( y ) d V B N ( y ) ,

then u H must either be equal to u or u σ H .

Before proceeding with the proof of this lemma, it is crucial to establish the following monotonicity result (refer also [28]).

Lemma 4.2

The function k α , N , as defined in (2.11), is positive and radially decreasing with respect to the geodesic distance ρ .

Proof

For N = 2 m + 1

k α , 2 m + 1 ( ρ ) = 1 Γ ( α 2 ) 0 p t , 2 m + 1 ( ρ ) d t t 1 α 2 = 1 Γ ( α 2 ) 0 2 m 1 π m 1 2 t 1 2 e ( N 1 ) 2 4 t 1 sinh ρ ρ m e ρ 2 4 t d t t 1 α 2 = 1 Γ ( α 2 ) 2 m 1 π m 1 2 0 t α 3 2 e ( N 1 ) 2 4 t 1 sinh ρ ρ m e ρ 2 4 t d t .

To obtain the monotonicity result, we differentiate the expression above. Observe that

ρ 1 sinh ρ ρ m e ρ 2 4 t = ( sinh ρ ) 1 sinh ρ ρ 1 sinh ρ ρ m e ρ 2 4 t = sinh ρ 1 sinh ρ ρ m + 1 e ρ 2 4 t .

Since the heat kernel is positive as per (2.6), we obtain

d d ρ k α , 2 m + 1 ( ρ ) = 2 π sinh ρ Γ ( α 2 ) 2 ( m + 1 ) 1 π ( m + 1 ) 1 2 0 t α 3 2 e N t e ( m + 1 ) 2 t 1 sinh ρ ρ m + 1 e ρ 2 4 t d t = 2 π sinh ρ Γ ( α 2 ) 0 e N t p t , 2 m + 3 ( ρ ) d t t 1 α 2 < 0 .

Using the same approach, we find that ρ p t , 2 m + 1 ( ρ ) < 0 .

For N = 2 m , applying Fubini’s theorem, we obtain

k α , 2 m ( ρ ) = 1 Γ ( α 2 ) 0 p t , 2 m ( ρ ) d t t 1 α 2 = 1 Γ ( α 2 ) 0 ( 2 π ) m 1 2 t 1 2 e ( N 1 ) 2 4 t ρ + sinh r cosh r cosh ρ 1 sinh r r m e r 2 4 t d r d t t 1 α 2 = 1 Γ ( α 2 ) ρ + sinh r cosh r cosh ρ 0 ( 2 π ) m 1 2 t 1 2 e ( N 1 ) 2 4 t 1 sinh r r m e r 2 4 t d t t 1 α 2 d r = 2 Γ ( α 2 ) 0 e t 4 ( 2 N 1 ) t 1 α 2 ρ + sinh r cosh r cosh ρ p t , 2 m + 1 ( r ) d r d t .

Making a change in variables, let w = cosh r cosh ρ , then

d d ρ p t , 2 m + 1 ( r ) = d p t , 2 m + 1 ( r ) d r r ρ = d p t , 2 m + 1 ( r ) d r sinh ρ sinh r < 0 .

Thus,

d d ρ k α , 2 m ( ρ ) = 2 2 Γ ( α 2 ) 0 e t 4 ( 2 N 1 ) t 1 α 2 0 d d ρ p t , 2 m + 1 ( r ( w , ρ ) ) d w d t < 0 .

With this, we achieve the desired result, thus completing the proof.□

Proof of Lemma 4.1

Consider the following:

B N ( Δ B N ) α 2 u ( y ) u ( y ) d V B N ( y ) = B N [ k α , N * u ] ( y ) u ( y ) d V B N ( y ) = B N B N [ k α , N ( d ( T y ( x ) , 0 ) ) u ( x ) d V B N ( x ) ] u ( y ) d V B N ( y ) = B N B N k α , N ( d ( T y ( x ) , 0 ) ) u ( x ) u ( y ) d V B N ( x ) d V B N ( y ) = H + H + k α , N ( d ( T y ( x ) , 0 ) ) [ u ( x ) u ( y ) + u ( σ H ( x ) ) u ( σ H ( y ) ) ] + k α , N ( d ( T σ H ( y ) ( x ) , 0 ) ) [ u ( x ) u ( σ H ( y ) ) + u ( σ H ( x ) ) u ( y ) ] d V B N ( x ) d V B N ( y ) ,

and similarly for u H . We aim to establish that the following inequality holds for all x H + and y H + :

(4.1) k α , N ( d ( T y ( x ) , 0 ) ) [ u ( x ) u ( y ) + u ( σ H ( x ) ) u ( σ H ( y ) ) ] + k α , N ( d ( T σ H ( y ) ( x ) , 0 ) ) [ u ( x ) u ( σ H ( y ) ) + u ( σ H ( x ) ) u ( y ) ] k α , N ( d ( T y ( x ) , 0 ) ) [ u H ( x ) u H ( y ) + u H ( σ H ( x ) ) u H ( σ H ( y ) ) ] + k α , N ( d ( T σ H ( y ) ( x ) , 0 ) ) [ u H ( x ) u H ( σ H ( y ) ) + u H ( σ H ( x ) ) u H ( y ) ] .

We will now analyze each case individually to verify this inequality.

Case I u ( σ H ( x ) ) u ( x ) , u ( σ H ( y ) ) u ( y ) .

In this case, we have

u H ( x ) = u ( x ) , u H ( y ) = u ( y ) , u H ( σ H ( x ) ) = u ( σ H ( x ) ) , u H ( σ H ( y ) ) = u ( σ H ( y ) ) .

Consequently, equality holds in (4.1).

Case II u ( σ H ( x ) ) u ( x ) , u ( σ H ( y ) ) u ( y ) .

This case can be handled in a manner similar to the previous one.

Case III u ( x ) u ( σ H ( x ) ) , u ( σ H ( y ) ) u ( y ) .

Here, we have

u H ( x ) = u ( σ H ( x ) ) , u H ( y ) = u ( y ) , u H ( σ H ( x ) ) = u ( x ) , u H ( σ H ( y ) ) = u ( σ H ( y ) ) .

Moreover, given that u 0 , the subsequent inequality is satisfied

(4.2) [ u ( σ H ( x ) ) u ( x ) ] u ( y ) [ u ( σ H ( x ) ) u ( x ) ] u ( σ H ( y ) ) u ( σ H ( x ) ) u ( y ) + u ( x ) u ( σ H ( y ) ) u ( σ H ( x ) ) u ( σ H ( y ) ) + u ( x ) u ( y ) .

Now, consider the LHS of (4.1)

k α , N ( d ( T y ( x ) , 0 ) ) [ u ( x ) u ( y ) + u ( σ H ( x ) ) u ( σ H ( y ) ) ] + k α , N ( d ( T σ H ( y ) ( x ) , 0 ) ) [ u ( x ) u ( σ H ( y ) ) + u ( σ H ( x ) ) u ( y ) ] = k α , N ( d ( T σ H ( y ) ( x ) , 0 ) ) [ u ( x ) u ( y ) + u ( σ H ( x ) ) u ( σ H ( y ) ) + u ( x ) u ( σ H ( y ) ) + u ( σ H ( x ) ) u ( y ) ] + [ k α , N ( d ( T y ( x ) , 0 ) ) k α , N ( d ( T σ H ( y ) ( x ) , 0 ) ) ] ( u ( x ) u ( y ) + u ( σ H ( x ) ) u ( σ H ( y ) ) ) k α , N ( d ( T σ H ( y ) ( x ) , 0 ) ) [ u ( x ) u ( y ) + u ( σ H ( x ) ) u ( σ H ( y ) ) + u ( x ) u ( σ H ( y ) ) + u ( σ H ( x ) ) u ( y ) ] + [ k α , N ( d ( T y ( x ) , 0 ) ) k α , N ( d ( T σ H ( y ) ( x ) , 0 ) ) ] ( u ( σ H ( x ) ) u ( y ) + u ( x ) u ( σ H ( y ) ) ) = k α , N ( d ( T σ H ( y ) ( x ) , 0 ) ) [ u ( x ) u ( y ) + u ( σ H ( x ) ) u ( σ H ( y ) ) ] + k α , N ( d ( T y ( x ) , 0 ) ) [ u ( σ H ( x ) ) u ( y ) + u ( x ) u ( σ H ( y ) ) ] = k α , N ( d ( T y ( x ) , 0 ) ) [ u H ( x ) u H ( y ) + u H ( σ H ( x ) ) u H ( σ H ( y ) ) ] + k α , N ( d ( T σ H ( y ) ( x ) , 0 ) ) [ u H ( σ H ( x ) ) u H ( y ) + u H ( x ) u H ( σ H ( y ) ) ] .

where we used the fact that x , y H + , along with Lemma 4.2 and the rearrangement inequality (4.2).

Case IV u ( σ H ( x ) ) u ( x ) , u ( y ) u ( σ H ( y ) ) .

This scenario can be addressed in a manner similar to Case III.

Therefore, the lemma can be concluded utilizing (4.1) and the provided hypothesis.□

Now, we will showcase how the condition that either u H = u or u H = u σ H can be leveraged to infer certain symmetry properties.

Lemma 4.3

For any s 1 and u L s ( B N ) , if u 0 and for every closed, totally geodesic hypersurface H B N , it holds that u H = u or u H = u σ H , then there exist x 0 B N and a nonincreasing function v : ( 0 , ) R such that for almost every x B N , u ( x ) = v ( d ( x , x 0 ) ) .

To establish Lemma 4.3, we begin by proving the following result (refer also to [46]).

Lemma 4.4

Let u L s ( B N ) and w L t ( B N ) with 1 s + 1 t = 1 be a radial function such that for every x , y B N with d ( x , 0 ) d ( y , 0 ) , w ( x ) w ( y ) , with equality if and only if d ( x , 0 ) = d ( y , 0 ) . Let H B N be a closed, totally geodesic hypersurface. If y 0 H + and

B N u H ( x ) w ( T y 0 ( x ) ) B N u ( x ) w ( T y 0 ( x ) ) ,

then u = u H .

Proof

We will divide the proof into the following two distinct cases for x H + :

Case I u ( x ) u ( σ H ( x ) ) . In this case, we obtain

u H ( x ) = u ( σ H ( x ) ) , u H ( σ H ( x ) ) = u ( x ) .

Additionally, for any x H + , we observe that since y 0 H + , d ( σ H ( x ) , y 0 ) > d ( x , y 0 ) , or equivalently, d ( T y 0 ( σ H ( x ) ) , 0 ) > d ( T y 0 ( x ) , 0 ) . Thus, w ( T y 0 ( x ) ) > w ( T y 0 ( σ H ( x ) ) ) .

Now, consider

[ u H ( x ) u ( x ) ] w ( T y 0 ( x ) ) = [ u ( σ H ( x ) ) u H ( σ H ( x ) ) ] w ( T y 0 ( x ) ) [ u ( σ H ( x ) ) u H ( σ H ( x ) ) ] w ( T y 0 ( σ H ( x ) ) ) ,

which leads to the inequality

(4.3) u ( x ) w ( T y 0 ( x ) ) + u ( σ H ( x ) ) w ( T y 0 ( σ H ( x ) ) ) u H ( x ) w ( T y 0 ( x ) ) + u H ( σ H ( x ) ) w ( T y 0 ( σ H ( x ) ) ) .

Case II u ( x ) u ( σ H ( x ) ) .

In this case, we arrive at

u ( x ) w ( T y 0 ( x ) ) + u ( σ H ( x ) ) w ( T y 0 ( σ H ( x ) ) ) = u H ( x ) w ( T y 0 ( x ) ) + u H ( σ H ( x ) ) w ( T y 0 ( σ H ( x ) ) ) .

Thus, inequality (4.3) holds in either case. By integrating this inequality over H + , we obtain

B N u H ( x ) w ( T y 0 ( x ) ) B N u ( x ) w ( T y 0 ( x ) ) .

Hence, based on the given assumption, we have for almost every x H +

(4.4) u ( x ) w ( T y 0 ( x ) ) + u ( σ H ( x ) ) w ( T y 0 ( σ H ( x ) ) ) = u H ( x ) w ( T y 0 ( x ) ) + u H ( σ H ( x ) ) w ( T y 0 ( σ H ( x ) ) ) .

Since y 0 H + , d ( σ H ( x ) , y 0 ) > d ( x , y 0 ) , and noting that w is radially decreasing, we have w ( T y 0 ( x ) ) > w ( T y 0 ( σ H ( x ) ) ) . Therefore, it must be that u H ( x ) = u ( x ) and u H ( σ H ( x ) ) = u ( σ H ( x ) ) , because otherwise, we would fall under Case I and derive a strict inequality in (4.3), contradicting (4.4).□

Lemma 4.5

Let u L s ( B N ) . If for every closed, totally geodesic hypersurface H B N with x 0 H + , we have u H = u , then there exists a nonincreasing function v : ( 0 , ) R such that u ( x ) = v ( d ( x , x 0 ) ) for almost every x B N .

For a function u : B N R + + , the symmetric rearrangement, also known as Schwarz symmetrization, u * : B N R + + , is defined as the unique function such that for every λ > 0 , there exists R 0 satisfying

{ x B N : u * ( x ) > λ } = B R ( 0 ) ,

and

μ { x B N : u * ( x ) > λ } = μ { x B N : u ( x ) > λ } ,

where B R ( 0 ) denotes the geodesic ball in B N centered at 0 with radius R , and μ denotes the volume measure in B N .

Thus, u * is a radial and radially decreasing function whose superlevel sets have the same measure as those of u .

Clearly, Lemma 4.5 follows from the subsequent lemma.

Lemma 4.6

Let s 1 and u L s ( B N ) be nonnegative. The following conditions are equivalent:

  1. u * = u .

  2. For almost every x , y B N , if d ( x , 0 ) d ( y , 0 ) , then u ( x ) u ( y ) .

  3. For every closed, totally geodesic hypersurface H such that 0 H + , u ( x ) u ( σ H ( x ) ) , for almost every x H + .

  4. For every closed, totally geodesic hypersurface H B N such that 0 H + , u H = u .

Proof

The implication (1) (2) is straightforward. To prove (2) (1) , since u is radially decreasing, there exists a decreasing function v : [ 0 , + ) R such that u ( x ) = v ( d ( x , 0 ) ) . Given that u L s ( B N ) , it is evident that lim r + v ( r ) = 0 . Hence, u 0 and for all λ > 0 , μ { x B N : u * ( x ) > λ } = μ { x B N : u ( x ) > λ } , which implies u = u * .

There is nothing to prove for (2) (3) . To prove (3) (2) , let x , y B N be such that x y and d ( x , 0 ) d ( y , 0 ) . There exists a closed, totally geodesic hypersurface H such that x H + and y = σ H ( x ) . By assumption, we have u ( y ) = u ( σ H ( x ) ) u ( x ) .

Finally, the equivalence (3) (4) follows from the definition of u H .□

Proof of Lemma 4.3

Select w 0 satisfying the assumptions of Lemma 4.4. For x B N , define the function

W ( x ) = B N u ( y ) w ( T x ( y ) ) d V B N ( y ) .

This function is nonnegative, continuous, and lim d ( x , 0 ) W ( x ) = 0 , indicating it attains a maximum at some point x 0 B N .

To finalize the proof using Lemma 4.5, we need to show that for every closed, totally geodesic hypersurface H B N where x 0 is in H + , the equality u H = u holds. Specifically, if u H = u σ H , then, considering that w is radial and based on the definition of x 0 ,

B N u H ( y ) w ( T x 0 ( y ) ) d V B N ( y ) = B N u ( σ H ( y ) ) w ( T x 0 ( y ) ) d V B N ( y ) = B N u ( y ) w ( T σ H ( x 0 ) ( y ) ) d V B N ( y ) B N u ( y ) w ( T x 0 ( y ) ) d V B N ( y ) .

Therefore, by Lemma 4.4, we have u H = u .□

Proof of Proposition 4.1

Consider a closed, totally geodesic hypersurface H B N . Observe the following equalities:

B N B N u H 2 = B N B N u 2 and B N u H 2 = B N u 2 .

Based on the characterization of ground states, it follows that

B N ( Δ B N ) α 2 u p ( y ) u p ( y ) d V B N ( y ) B N ( Δ B N ) α 2 u H p ( y ) u H p ( y ) d V B N ( y ) .

According to Lemma 4.1, for any closed, totally geodesic hypersurface H B N , it holds that either u H = u or u H = u σ H . Therefore, the conclusion can be drawn from Lemma 4.3.□

5 Regularity

In this section, we examine the regularity of the solution to the problem ( F α , λ ) following the approach of [38]. To do this, we require a nonlocal analog of the estimate provided in [8, Lemma 2.1] by Brezis and Kato, which can be established using the inequality stated in Lemma 5.2. In particular, we prove the following result in this section.

Theorem 5.1

Let N 3 , λ < ( N 1 ) 2 4 , and α ( 0 , N ) . If u is a solution of ( F α , λ ) for N + α N p N + α N 2 , then u L q ( B N ) for every q 2 , N α 2 N N 2 . Moreover, if 2 < p N + α N 2 and 1 α < N , then u L ( B N ) .

To establish the preceding theorem, we need the following auxiliary lemmas.

Lemma 5.1

Let N 2 , α ( 0 , N ) , and θ ( 0 , 2 ) . If H , K L 2 N α + 2 ( B N ) + L 2 N α ( B N ) and α N < θ < 2 α N , then for every ε > 0 , there exists C ε , θ R such that for every u H 1 ( B N ) ,

B N ( Δ B N ) α 2 ( H u θ ) K u 2 θ d V B N ε 2 B N B N u 2 d V B N + C ε , θ B N u 2 d V B N .

Lemma 5.2

Let N 2 and 0 < α < N . Suppose q , r , s , t [ 1 , ) and τ [ 0 , 2 ] satisfy the following conditions:

1 + α N 1 s 1 t = τ q + 2 τ r .

If θ ( 0 , 2 ) satisfies

min ( q , r ) α N 1 s < θ < max ( q , r ) 1 1 s , min ( q , r ) α N 1 t < 2 θ < max ( q , r ) 1 1 t ,

then for every H L s ( B N ) , K L t ( B N ) , and u L q ( B N ) L r ( B N ) ,

B N ( Δ B N ) α 2 ( H u θ ) K u 2 θ C H L s ( B N ) K L t ( B N ) u L q ( B N ) τ u L r ( B N ) 2 τ .

The proofs of the above two lemmas follow exactly on the same lines as [38, Lemma 3.2, 3.3], utilizing the Hölder and HLS inequalities repeatedly. Consequently, we omit the proofs here.

Proposition 5.1

If H , K L 2 N α ( B N ) + L 2 N α + 2 ( B N ) , λ < ( N 1 ) 2 4 , and u H 1 ( B N ) solves

Δ B N u λ u = ( Δ B N ) α 2 H u K ,

then u L p ( B N ) for every p 2 , N α 2 N N 2 .

Proof

By setting θ = 1 in Lemma 5.1, there exists a constant β > 0 such that β > 2 λ and

(5.1) B N ( Δ B N ) α 2 H ϕ K ϕ 1 2 B N B N ϕ 2 d V B N + β 2 B N ϕ 2 d V B N

for all ϕ H 1 ( B N ) . Consider the sequences { H k } k N and { K k } k N in L 2 N α ( B N ) such that H k H , H k ( x ) H ( x ) almost everywhere, and K k K , K k ( x ) K ( x ) almost everywhere in B N . For each k N , define a k : H 1 ( B N ) × H 1 ( B N ) R such that for w , v H 1 ( B N )

a k ( w , v ) B N B N w B N v λ B N w v + β B N w v B N ( Δ B N ) α 2 H k w K k v .

Using (2.3) and (5.1), we obtain

a k ( v , v ) B N B N v 2 d V B N + ( β λ ) B N v 2 d V B N 1 2 B N B N v 2 d V B N + β 2 B N v 2 d V B N 1 2 B N B N v 2 d V B N + β 2 λ B N v 2 d V B N C v λ 2 .

Furthermore, by applying Hölder’s inequality to the last term of a k ( w , v ) , with the exponents chosen such that 1 r 1 = 1 2 α 2 N and 1 r 2 = α 2 N + 1 2 , and then employing the HLS inequality, the boundedness of the bilinear form can be easily established. Consequently, a k is a bounded and coercive bilinear form. Therefore, by invoking the Lax-Milgram theorem for the functional f : H 1 ( B N ) R defined as:

f ( v ) = B N β u v d V B N v H 1 ( B N ) ,

there exists unique u k H 1 ( B N ) such that a k ( u k , v ) = f ( v ) holds for every v H 1 ( B N ) . Consequently, u k satisfies the equation

(5.2) Δ B N u k λ u k + β u k = ( Δ B N ) α 2 H k u k K k + β u in B N .

It follows that the sequence { u k } u in H 1 ( B N ) as k . For any γ > 0 , we define the truncated function u k , γ by

u k , γ ( x ) = γ if u k ( x ) γ , u k ( x ) if γ < u k ( x ) < γ , γ if u k ( x ) γ .

By choosing the test function v ( x ) = u k , γ q 2 u k , γ H 1 ( B N ) as a test function in (5.2), we obtain

( q 1 ) B N u k , γ q 2 B N u k B N u k , γ d V B N + ( β λ ) B N u k , γ q 2 u k u k , γ d V B N = B N ( Δ B N ) α 2 H k u k K k u k , γ q 2 u k , γ d V B N + β B N u u k , γ q 2 u k , γ d V B N .

Additionally, by the construction of u k , γ , we have u k , γ q u k , γ q 2 u k , γ u k . Furthermore, using the relation B N u ( x ) B N 2 = 1 x 2 2 2 u ( x ) 2 , we obtain

( q 1 ) B N u k , γ q 2 B N u k , γ 2 d V B N + ( β λ ) B N u k , γ q 2 u k , γ u k d V B N 4 ( q 1 ) q 2 B N B N ( u k , γ ) q 2 2 d V B N + ( β λ ) B N u k , γ q 2 2 d V B N .

Thus, we have

4 ( q 1 ) q 2 B N B N ( u k , γ ) q 2 2 d V B N + ( β λ ) B N u k , γ q 2 2 d V B N ( q 1 ) B N u k , γ q 2 B N u k , γ B N u k d V B N + ( β λ ) B N u k , γ q 2 u k , γ u k d V B N = B N ( Δ B N ) α 2 H k u k K k u k , γ q 2 u k , γ d V B N + β B N u u k , γ q 2 u k , γ d V B N .

For 2 q < 2 N α , selecting θ = 2 q α N , 2 α N and u = u k , γ in Lemma 5.1, we obtain

B N ( Δ B N ) α 2 H k u k , γ K k u k , γ q 2 u k , γ 2 ( q 1 ) q 2 B N B N ( u k , γ ) q 2 2 + C B N u k , γ q 2 2 .

Now, setting A k , γ = { x B N : u k ( x ) > γ } , we derive

4 ( q 1 ) q 2 B N B N ( u k , γ ) q 2 2 d V B N + ( β λ ) B N u k , γ q 2 2 d V B N C B N u k , γ q 2 2 d V B N 2 ( q 1 ) q 2 B N B N ( u k , γ ) q 2 2 d V B N 2 A k , γ ( Δ B N ) α 2 K k u k q 1 H k u k d V B N + β B N u k , γ q 2 u k , γ u d V B N .

This implies

(5.3) 2 ( q 1 ) q 2 B N B N ( u k , γ ) q 2 2 d V B N 2 A k , γ ( Δ B N ) α 2 K k u k q 1 H k u k d V B N + C B N u k , γ q 2 u k , γ u + u k , γ q d V B N 2 A k , γ ( Δ B N ) α 2 K k u k q 1 H k u k d V B N + C B N u k q + u q d V B N .

Applying the HLS inequality gives

A k , γ ( Δ B N ) α 2 K k u k q 1 H k u k C B N K k u k q 1 r 1 r A k , γ H k u k s 1 s ,

where 1 r = α 2 N + 1 1 q and 1 s = α 2 N + 1 q . Assuming u k L q ( B N ) , it follows from Hölder’s inequality that K k u k q 1 L r ( B N ) and H k u k L s ( B N ) . As a result, we have

A k , γ ( Δ B N ) α 2 K k u k q 1 H k u k 0 as γ .

By taking the limit γ in (5.3), we derive

2 ( q 1 ) q 2 B N B N ( u k ) q 2 2 d V B N C B N u k q + u q d V B N .

This indicates that u k q 2 H 1 ( B N ) L 2 N N 2 ( B N ) . Therefore, by Fatou’s lemma

B N u k q 2 2 N N 2 d V B N 2 ( N 2 ) 2 N C ( u k ) q 2 λ 2 C B N u k q + u q d V B N C B N u k q d V B N + limsup k B N u k q d V B N .

Thus, we conclude

limsup k B N u k N q N 2 d V B N 1 2 N C limsup k B N u k q d V B N .

By iterating the above argument finitely many times on q , we obtain u L r ( B N ) for all r 2 , 2 N α N N 2 .□

Proof of Theorem 5.1

Let u ( x ) be a solution of ( F α , λ ). Since N + α N p N + α N 2 , we obtain

u ( x ) p 1 u ( x ) α N + u ( x ) α + 2 N 2 .

Setting H ( x ) = K ( x ) = u ( x ) p 2 u ( x ) , it follows that H , K L 2 N α ( B N ) + L 2 N α + 2 ( B N ) . Therefore, by Proposition 5.1, we conclude that u L q ( B N ) for q 2 , N α 2 N N 2 .

We will now demonstrate that u L ( B N ) . To establish this, we begin by claiming that ( Δ B N ) α 2 u p L ( B N ) .

To justify this claim, observe that for β R , R > 0 , we have

B R ( 0 ) 1 ( sinh ( d ( x , 0 ) ) ) β d V B N ( x ) = ω N 1 0 R ( sinh ρ ) N 1 ( sinh ρ ) β d ρ ω N 1 0 R ( sinh ρ ) N 1 cosh ρ ( sinh ρ ) β d ρ ,

where ω N 1 is the volume of S N 1 . Consequently, this integral converges when β < N Similarly, if β > N , then

( B R ( 0 ) ) 1 ( sinh ( d ( x , 0 ) ) ) β d V B N ( x ) < .

Using the estimates from (4.1) in [26], we obtain

for 0 < ρ < 1 , 0 < α < N

k α , N ( ρ ) C 1 ρ N α C ( N , α ) 1 ( sinh ρ ) N α .

Further, for ρ 1 and α > 2

k α , N ( ρ ) C ρ α 2 2 e ( N 1 ) ρ C ρ α 2 e ( N 1 ) ρ C e ρ ( N α ) C 1 ( sinh ρ ) N α .

For 1 α 2 , and ρ 1 , note that

e ( N 1 ) ρ ( sinh ρ ) N α ρ 2 α 2 sinh ρ e ρ N e ρ ( sinh ρ ) α 1 ( sinh ρ ) α 1 e ρ sinh ρ C .

Now, consider

( Δ B N ) α 2 u p = k α , N * u p = ( χ B R ( 0 ) k α , N ) * u p + ( χ ( B R ( 0 ) ) k α , N ) * u p .

From the estimates above, we can find p 1 , p 2 such that

χ B R ( 0 ) k α , N L p 1 ( B N ) for some p 1 1 , N N α ,

and

χ ( B R ( 0 ) ) k α , N L p 2 ( B N ) for some p 2 N N α , .

Given that N + α N p N + α N 2 , it follows that 2 < N p α < N α 2 N N 2 . Therefore, there exist q 1 and q 2 such that

u p L q 1 ( B N ) L q 2 ( B N ) ,

where q i and p i are conjugate indices for i = 1 , 2 . Applying Hölder’s inequality, we establish the desired claim. We can conclude the theorem by applying Theorem 4.1 from [6], noting that 2 < p N + α N 2 < 2 N N 2 .□

Remark 5.1

The L p Calderón-Zygmund inequality on noncompact Riemannian manifolds has been investigated in [22]. However, to achieve W 2 , p -type regularity in the current setting, the results from [22] cannot be directly applied; additional assumptions on the solution are necessary (refer [22, Proposition 3.8]).

Acknowledgments

The authors are grateful for the reviewer’s valuable comments that improved the manuscript. Authors also sincerely acknowledge D. Ganguly for the valuable discussions and insights.

  1. Funding information: First author was supported by the Prime Minister’s Research Fellowship (PMRF ID- 1401219). A part of this research is supported by DST-FIST project No. SR/FST/MS-1/2019/45.

  2. Author contributions: All authors have accepted responsibility for the entire content of this manuscript and consented to its submission to the journal, reviewed all the results, and approved the final version of the manuscript. D.G. and K.S. jointly developed the study, formulated the mathematical framework, established the main results, and prepared the manuscript together.

  3. Conflict of interest: The authors state no conflict of interest.

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Received: 2024-12-29
Revised: 2025-10-15
Accepted: 2025-10-29
Published Online: 2025-12-04

© 2025 the author(s), published by De Gruyter

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  65. Global boundedness and stability of a quasilinear two-species chemotaxis-competition model with nonlinear sensitivities
  66. Non-existence, radial symmetry, monotonicity, and Liouville theorem of master equations with fractional p-Laplacian
  67. Global existence, asymptotic behavior, and finite time blow up of solutions for a class of generalized thermoelastic system with p-Laplacian
  68. Formation of singularities for a linearly degenerate hyperbolic system arising in magnetohydrodynamics
  69. Linear stability and bifurcation analysis for a free boundary problem arising in a double-layered tumor model
  70. Hopf's lemma, asymptotic radial symmetry, and monotonicity of solutions to the logarithmic Laplacian parabolic system
  71. Generalized quasi-linear fractional Wentzell problems
  72. Existence, symmetry, and regularity of ground states of a nonlinear Choquard equation in the hyperbolic space
  73. Normalized solutions for NLS equations with general nonlinearity on compact metric graphs
  74. Boundedness and global stability in a predator-prey chemotaxis system with indirect pursuit-evasion interaction and nonlocal kinetics
  75. Review Article
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