Home Improved fractional Trudinger-Moser inequalities on bounded intervals and the existence of their extremals
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Improved fractional Trudinger-Moser inequalities on bounded intervals and the existence of their extremals

  • Lu Chen , Bohan Wang and Maochun Zhu EMAIL logo
Published/Copyright: May 29, 2023

Abstract

Let I be a bounded interval of R and λ 1 ( I ) denote the first eigenvalue of the nonlocal operator ( Δ ) 1 4 with the Dirichlet boundary. We prove that for any 0 α < λ 1 ( I ) , there holds

sup u W 0 1 2 , 2 ( I ) , ( Δ ) 1 4 u 2 2 α u 2 2 1 I e π u 2 d x < + ,

and the supremum can be attained. The method is based on concentration-compactness principle for fractional Trudinger-Moser inequality, blow-up analysis for fractional elliptic equation with the critical exponential growth and harmonic extensions.

MSC 2010: 46E30; 46E35

1 Introduction

Let Ω be a bounded domain in R n ; it is well known that the analogue of optimal Sobolev embedding for W 0 1 , n ( Ω ) (the Sobolev space consisting of functions vanishing on the boundary Ω ) can be given by the famous Trudinger-Moser inequality [30,33], which can be stated in the following form:

(1.1) sup u W 0 1 , n ( Ω ) , u n n 1 Ω exp ( α u n n 1 ) d x < + , iff α α n = n w n 1 1 n 1 ,

where ω n 1 is the area of unit sphere in R n . So far, Trudinger-Moser inequalities have also been generalized in many other directions such as the Trudinger-Moser inequalities on the unbounded domain, C-R spheres, compact Riemannian manifolds, Heisenberg group, and Trudinger-Moser inequalities in higher-order Sobolev spaces. We refer the interested readers to [1,6,7,10,14,17,23,31] and references therein.

In 1985, Lions [19] established the following concentration-compactness principle associated with inequality (1.1).

Theorem A

For any u k W 0 1 , n ( Ω ) with u k n 1 and u k u 0 0 in W 0 1 , n ( Ω ) , then there exists some p > 1 such that exp α n u k n n 1 is bounded in L p ( Ω ) .

This conclusion gives more precise information and is stronger than Trudinger-Moser inequality (1.1) when the function sequence u k u 0 0 . Later, the authors of [4] developed a new approach to obtain and sharpen Theorem A. The result in [4] reads as follows:

Theorem B

For any u k W 0 1 , n ( Ω ) with u k n 1 , and u k u 0 0 in W 0 1 , n ( Ω ) , then

(1.2) sup k Ω exp α n p u k n n 1 d x < ,

if p < p n = 1 ( 1 u 0 n n ) 1 n 1 . Moreover, p n is sharp in the sense that for p p n , there exists a sequence { u k } W 0 1 , n ( Ω ) with u k n = 1 such that the supreme of (1.2) is infinite.

Note that the proofs for the concentration-compactness principle in [4,19] depend on the Polya-Szego inequality in the Euclidean space, which is no longer available in the higher-order case or other settings, such as Riemannian manifolds or the Heisenberg groups. In a recent work [17], the authors obtained the concentration-compactness principle on the Heisenberg groups through a rearrangement-free argument by considering the level sets of the functions under consideration. We remark that this argument is inspired by the works [22,23] and can avoid using any rearrangement inequality (see also [27]). For other related work on the concentration-compactness principle associated with Trudinger-Moser-type inequalities, one can refer to [15,18,37] and references therein.

Inspired by the concentration-compactness principle for Trudinger-Moser inequality, Adimurthi and Druet [2] obtained an improved Trudinger-Moser inequality involving the L 2 norm on bounded domains of R 2 by the method of blow-up analysis.

Theorem C

For any 0 < α < λ 1 ( Ω ) , there holds

(1.3) sup u W 0 1 , 2 ( Ω ) , u 2 1 Ω e 4 π u 2 ( 1 + α u 2 2 ) d x < + ,

where

(1.4) λ 1 ( Ω ) = inf u W 0 1 , 2 ( Ω ) Ω u 2 d x Ω u 2 d x

denotes the first eigenvalue of the Laplacian operator with the Dirichlet boundary. Furthermore, if α λ 1 , the supremum is infinite.

This result was further extended to higher-order case or unbounded domains as well in [5,8,20,25,35,38,38]. We remark that in the work of [5], the authors can extend to (1.3) to the entire Euclidean space and the Heisenberg group by a simple scaling approach, which can avoid applying the complicated blow-up analysis often used in the literature to deal with such sharpened inequalities.

Recently, Wang and Ye [34] proved the following Trudinger-Moser inequality involved in the Hardy term:

(1.5) sup B u 2 d x B u 2 ( 1 x 2 ) 2 d x 1 B e 4 π u 2 d x < ,

where B denotes the unit ball in R 2 . In a recent article [21], Lu and Yang gave a rearrangement-free argument of (1.5) and confirmed that the conjecture for the Hardy-Trudinger-Moser inequality given in [34] indeed holds for any bounded and convex domain in R 2 via the Riemann mapping theorem. We state the result as follows:

Theorem D

Let Ω be a proper and convex bounded domain in R 2 and u C 0 ( Ω ) be such that

Ω u 2 d x 1 4 Ω u 2 d ( x , Ω ) 2 d x 1 ,

where d ( x , Ω ) = min { x x : x Ω } . Then, there exists a constant C, which is independent of u such that

Ω e 4 π u 2 d x C .

A higher-dimensional version of Theorem D has been recently established by Liang et al. in [24]. Hardy-Adams-type inequality on hyperbolic balls has also been established in [16] (see also references therein).

In the recent work [32], Tintarev modified the Hardy-type Trudinger-Moser inequality (1.5) and proved

(1.6) sup Ω u 2 d x Ω V ( x ) u 2 d x 1 Ω e 4 π u 2 d x <

for some class of V ( x ) > 0 , including the case of (1.5). In particular, when V ( x ) = α with 0 α < λ 1 , then one has

(1.7) sup Ω u 2 d x α Ω u 2 d x 1 Ω e 4 π u 2 d x < + .

We remark that (1.7) is stronger than (1.3).

In this note, we are concerned with the Trudinger-Moser inequality on the line R . In order to state the related results, we first introduce the concept of fractional Laplacian and the related fractional Sobolev space. For any s ( 0 , 1 ) and φ S ( R n ) (the Schwarz space), the fractional Laplacian ( Δ ) s φ is given by:

( Δ ) s φ ( x ) = F 1 ( ξ 2 s F φ ( ξ ) ) ( x ) ,

where F and F 1 denote the Fourier transform and inverse Fourier transform, respectively. Let us consider the space:

L s ( R n ) = u L loc 1 ( R n ) : R n u 1 + x n + 2 s d x < + ,

fractional operator ( Δ ) s can be defined on u L s ( R n ) S ( R n ) through

φ , ( Δ ) s u = ( Δ ) s φ , u .

We also define the fractional Sobolev space W s , p ( R n ) and W 0 s , p ( Ω ) ( s ( 0 , + ) and p [ 1 , + ) ) by

W s , p ( R n ) = u L p ( R n ) : ( Δ ) s 2 u L p ( R n ) , W 0 s , p ( Ω ) = { u W s , p ( R n ) : u = 0 on R n \ Ω } .

Iula et al. [26] established the following fractional Trudinger-Moser inequality on some interval of line.

Theorem E

For any I R , when α π , it holds that

sup u W 0 1 2 , 2 ( I ) , u L 2 ( I ) 2 1 I ( e α u 2 1 ) d x < + .

This result was further extended to the general fractional Sobolev space W 0 s , p ( Ω ) with s p = n by Martinazzi in [28].

Based on the aforementioned results, a natural problem arises. Whether the fractional analogue for Trudinger-Moser inequality of Tintarev type (1.7) on R still holds. In this article, we deal with this problem. Our main result states the following.

Theorem 1.1

Let I be a bounded interval of R and λ 1 ( I ) be the first eigenvalue of ( Δ ) 1 4 with Dirichlet boundary. For any 0 α < λ 1 ( I ) , there holds

(1.8) sup u W 0 1 2 , 2 ( I ) , u 1 2 , α 2 1 I e π u 2 d x < + ,

where u 1 2 , α 2 = ( Δ ) 1 4 u 2 2 α u 2 2 .

As the application of Theorem 1.1, one can easily obtain fractional Trudinger-Moser inequality involving the L 2 norm. Indeed, denote v = ( 1 + α u L 2 2 ) 1 2 u ; direct computation gives

( Δ ) 1 4 v L 2 2 α v L 2 2 ( 1 + α u L 2 2 ) ( 1 α u L 2 2 ) 1 .

This together with the fractional Trudinger-Moser inequality (1.8) implies

Corollary 1.2

For any 0 α < λ 1 ( I ) , there holds

sup u W 0 1 2 , 2 ( I ) , ( Δ ) 1 4 u 2 2 1 I e π u 2 ( 1 + α u 2 2 ) d x < + .

Once we establish the fractional Trudinger-Moser inequality (1.8), it remains to ask whether or not there exist extremals for this inequality. The earlier study of extremals for Trudinger-Moser inequality can date back to Carleson and Chang’s work in [3]. They used the rearrangement and ODE technique to obtain the existence of extremals for classical Trudinger-Moser inequality in a unit ball of R n . Later, their results were also extended by Flucher [9] to bounded domain in R 2 and by Lin [11] to bounded domain in R n , respectively. Existence of extremals for Trudinger-Moser inequality on compact manifold has also been established by Li in [12,13]. There are also some existence results of extremals for Trudinger-Moser inequality of Tintarev type (see [36]).

Recently, Mancini and Martinazzi [29] established the existence result for the fractional Trudinger-Moser inequality on an interval in R by the harmonic extensions and commutator estimates. In this article, we will also show that fractional Trudinger-Moser inequality (1.8) of Tintarev type also has extremals. This result reads as:

Theorem 1.3

Under the assumption of Theorem 1.1, (1.8) can be attained by some function u 0 W 0 1 2 , 2 ( I ) C 1 ( I ¯ ) , with u 0 1 2 , α 2 = 1 .

Remark 1.4

The proof of Theorem 1.1 will be included in the proof of Theorem 1.3.

It is easily observed that the existence of extremals for fractional Trudinger-Moser inequality of Tintarev type on a bounded interval is equivalent to that in a symmetrical interval. For simplicity, in this context, we may assume I ( 1 , 1 ) .

This article is organized as follows. In Section 2, we study the existence of extremals for subcritical fractional Trudinger-Moser inequality of Tintarev type and give the maximizing sequences for (1.8). In Section 3, we analyze the asymptotic behavior of the maximizing sequences near and away from blow-up point when the blow-up phenomenon arises. In Section 4, we derive the Carleson-Chang-type upper bound for (1.8) through capacity estimates. Finally, in Section 5, we prove the existence of extremals for fractional Trudinger-Moser inequality of Tintarev type by constructing an appropriate test function sequence such that the upper bound can be surpassed.

2 Subcritical fractional Trudinger-Moser inequality of Tintarev type and the maximizing sequences

In this section, we establish the existence of extremals for subcritical fractional Trudinger-Moser inequality of Tintarev type and give the maximizing sequences for critical fractional Trudinger-Moser inequality of Tintarev type (1.8).

Denote

(2.1) C ε sup u W 0 1 2 , 2 ( I ) , u 1 2 , α 2 1 I e ( π ε ) u 2 d x .

We will show that there exists u ε W 0 1 2 , 2 ( I ) such that

(2.2) C ε = I e ( π ε ) u ε 2 d x .

For this purpose, we need the following Lions’ type concentration-compactness principle.

Lemma 2.1

Let u ε W 0 1 2 , 2 ( I ) , with u ε 1 2 , α = 1 and u ε u 0 0 in W 0 1 2 , 2 ( I ) . Then, for any p < 1 1 u 0 1 2 , α 2 , it holds

(2.3) limsup ε 0 I e π p u ε 2 d x < + .

Proof

By the compactness of the Sobolev embedding theorem, we obtain u ε 2 2 u 0 2 2 when ε 0 . Since u 0 and u ε 1 2 , α 2 = 1 , we can easily calculate that

lim ε 0 ( Δ ) 1 4 ( u ε u 0 ) 2 2 = 1 u 0 1 2 , α 2 < 1 .

On the other hand, a direct computation gives that for any p , there holds

I e π p u ε 2 d x I e π p ( 1 + δ ) ( u ε u 0 ) 2 + π p 1 + 1 δ u 0 2 d x I e π p ( 1 + δ ) ( u ε u 0 ) 2 r d x 1 r I e π p 1 + 1 δ u 0 2 s d x 1 s ,

where δ > 0 , r > 1 , s > 1 with 1 r + 1 s = 1 . For any p < 1 1 u 0 1 2 , α 2 , we can choose δ close to 0 and r close to 1 such that the last term in the aforementioned inequality can be controlled by:

I exp π ( u ε u 0 ) 2 ( Δ ) 1 4 ( u ε u 0 ) 2 2 d x 1 r I e π p 1 + 1 δ u 0 2 s d x 1 s ,

which is finite as a direct consequence of fractional Trudinger-Moser inequality.

Obviously, inequality (2.3) is obtained.□

Lemma 2.2

C ε could be achieved by some function u 0 W 0 1 2 , 2 ( I ) .

Proof

Let u j W 0 1 2 , 2 ( I ) be a maximizing sequence for C ε , i.e., u j 1 2 , α = 1 and

lim j I e ( π ε ) u j 2 d x = C ε .

Since 0 α < λ 1 ( I ) and I ( Δ ) 1 4 u j 2 d x α I u j 2 d x = 1 , we obtain that { u j } is bounded in W 0 1 2 , 2 ( I ) . Therefore, we obtain

u j u ε in W 0 1 2 , 2 ( I ) , u j u ε in L 2 ( I ) , u j u ε a.e. in I .

If u ε 0 , then lim j ( Δ ) 1 4 u j 2 2 = 1 . By fractional Trudinger-Moser inequality, for some p > 1 , e ( π ε ) u j 2 is bounded in L p ( I ) . If u ε 0 , in view of Lemma 2.1, we can also deduce that e ( π ε ) u j 2 is bounded in L p ( I ) for some p > 1 . It follows from Vitali convergence theorem that e ( π ε ) u j 2 e ( π ε ) u ε 2 in L 1 ( I ) . This strong convergence combines with the monotonicity of e ( π ε ) t about t , which implies that

sup u W 0 1 2 , 2 ( I ) , u 1 2 , α 2 1 I e ( π ε ) u 2 d x = I e ( π ε ) u ˜ ε 2 d x I e ( π ε ) u ε 2 d x ,

where u ˜ ε u ε u ε 1 2 , α 2 = 1 and u ˜ ε 1 2 , α = 1 ; then, the proof is accomplished.□

Using Lemma 2.1, we can see that subcritical Trudinger-Moser inequality (2.1) could be achieved by u ε . Obviously, u ε satisfies the following Euler-Lagrange equation:

(2.4) λ ε = I u ε 2 e ( π ε ) u ε 2 d x , ( Δ ) 1 4 u ε 2 2 α u ε 2 2 = 1 , 1 λ ε u ε e ( π ε ) u ε 2 = ( Δ ) 1 2 u ε α u ε in I .

Furthermore, we also have

Lemma 2.3

It holds

(2.5) lim ε 0 C ε = sup u W 0 1 2 , 2 ( I ) , u 1 2 , α 2 = 1 I e π u 2 d x .

Proof

It is obvious that

lim ε 0 C ε sup u W 0 1 2 , 2 ( I ) , u 1 2 , α 2 = 1 I e π u 2 d x .

For any u W 0 1 2 , 2 ( I ) , with u 1 2 , α = 1 , according to Fatou’s lemma, we obtain

I e π u 2 d x liminf ε 0 I e ( π ε ) u 2 d x liminf ε 0 C ε .

This implies that

sup u W 0 1 2 , 2 ( I ) , u 1 2 , α 2 = 1 I e π u 2 d x liminf ε 0 C ε .

Consequently, we obtain (2.5).□

Now, we are in position to pick up u ε as the maximizing sequences for Trudinger-Moser inequality (1.8). Assuming u ε C ( I ) C 0 , 1 2 ( I ¯ ) , which is monotonically decreasing about the origin. Since u ε is bounded in W 0 1 2 , 2 ( I ) , Banach-Alaoglu theorem and fractional compact Sobolev embedding theorem directly give that

u ε u in W 0 1 2 , 2 ( I ) u ε u in L 2 ( I ) u ε u a.e. in I .

Let

c ε = u ε ( 0 ) = max I u ε .

If c ε is bounded, then e ( π ε ) u ε 2 is also bounded, which implies that e ( π ε ) u ε 2 converges to e π u 2 in L 1 ( I ) . Hence, for any v W 0 1 2 , 2 ( I ) C 1 ( I ¯ ) with v 1 2 , α 1 , we have

lim ε 0 I e ( π ε ) u ε 2 d x = I e π u 2 d x .

This combines with Lemma 2.1; we can deduce that u is the desired extremal function.

If c ε is unbounded, without loss of generality, we claim that the weak limit of u ε is equal to zero. In fact, if u 0 0 , by concentration-compactness principle Lemma 2.1, we know that e π u ε 2 is bounded in L p ( I ) for any p < 1 1 u 0 1 2 , α 2 . This together with elliptic estimates gives that u ε is bounded in I , which contradicts c ε .

We also further claim ( Δ ) 1 4 u ε 2 d x δ 0 in the sense of measure. Otherwise, we can find some r 0 > 0 , B r 0 ( 0 ) I , and a cut-off function φ C 0 ( B r 0 ( 0 ) ) , with 0 φ 1 , and φ = 1 on B r 0 2 ( 0 ) . We have

limsup ε 0 B r 0 ( 0 ) ( Δ ) 1 4 ( φ u ε ) 2 d x < 1 .

By fractional Trudinger-Moser inequality, e ( π ε ) ( φ u ε ) 2 is bounded in L p ( I ) for some p > 1 . Applying elliptic estimates, we obtain that u ε is uniformly bounded on B r 0 2 ( 0 ) , which is a contradiction.

3 Asymptotic behavior of the maximizing sequences u ε

In this section, we will study asymptotic behavior of the maximizing sequences u ε near and far away from the blow-up point.

Set

r ε = λ ε ( π ε ) c ε 2 e ( π ε ) c ε 2 .

Define I ε = { x R : r ε x I } and η ε ( x ) 2 ( π ε ) c ε ( u ε ( r ε x ) c ε ) . If r ε 0 , similar to the proof of Theorem 1.3 in [29], we obtain η ε ( x ) η 0 ( x ) = ln 1 1 + x 2 and

(3.1) R e η 0 ( x ) d x = R 1 1 + x 2 d x = π .

This describes the asymptotic behavior of u ε around origin. Now, we start to analyze the asymptotic behavior of u ε away from the blow-up point 0. For this purpose, we need the following lemma.

Lemma 3.1

For any A > 1 , there holds

(3.2) limsup ε 0 ( Δ ) 1 4 u ε A 2 2 1 A ,

where u ε A min u ε , c ε A .

Proof

As mentioned earlier, we have

1 + α u ε 2 2 = ( Δ ) 1 4 u ε 2 2 = u ˜ ε 2 2

and

( Δ ) 1 4 u ε 2 2 = I u ε ( Δ ) 1 2 u ε d x = I u ε u ε λ ε e ( π ε ) u ε 2 + α u ε d x .

Set u ¯ ε A min u ˜ ε , c ε A , where u ˜ ε is the harmonic extension of u ε to R + 2 = R × ( 0 , + ) given by the Poisson integral:

u ˜ ( x , y ) 1 π R y u ( ξ ) y 2 + ( x ξ ) 2 d ξ , y > 0 .

Obviously, u ¯ ε A is a general extension of u ε A on R + 2 ; by Dirichlet energy principle, we have

( Δ ) 1 4 u ε A 2 2 R + 2 u ¯ ε A 2 d x d y .

Using integration by parts and the harmonicity of u ˜ ε , we obtain

R + 2 u ¯ ε A 2 d x d y = R + 2 u ¯ ε A u ˜ ε d x d y = R u ε A ( x ) u ˜ ε ( x , 0 ) y d x = R u ε A ( Δ ) 1 2 u ε d x .

Denote

v ε A u ε c ε A + = u ε u ε A ,

as ε 0 , we have

lim ε 0 R v ε A ( Δ ) 1 2 u ε d x = lim ε 0 R v ε A u ε λ ε e ( π ε ) u ε 2 + α u ε d x lim R lim ε 0 1 1 A R r ε R r ε u ε c ε λ ε e ( π ε ) u ε 2 ( x ) d x + lim ε 0 R α u ε v ε A d x = lim R lim ε 0 1 1 A R R u ε c ε λ ε r ε e ( π ε ) u ε 2 ( r ε ) d x = lim R lim ε 0 1 1 A R R u ε e ( π ε ) u ε 2 ( r ε ) ( π ε ) c ε e π c ε 2 d x = 1 1 A ,

where we use the fact: u ε 0 in L 2 ( I ) in the last equality.

Since u ε 1 2 , α = 1 , we obtain that

lim ε 0 R ( v ε A ( Δ ) 1 2 u ε + u ε A ( Δ ) 1 2 u ε ) d x = lim ε 0 R u ε ( Δ ) 1 2 u ε d x = 1 + lim ε 0 α u ε 2 2 = 1 .

Combining the aforementioned estimates, we deduce that

R u ε A ( Δ ) 1 2 u ε d x 1 A .

Then, we conclude (3.2).□

Lemma 3.2

We have

(3.3) lim ε 0 I e ( π ε ) u ε 2 d x = limsup ε 0 λ ε c ε 2 + I .

Moreover,

(3.4) lim ε 0 c ε λ ε = 0 .

Proof

We split

I e ( π ε ) u ε 2 d x = I u ε c ε A e ( π ε ) u ε 2 d x + I u ε > c ε A e ( π ε ) u ε 2 d x I 1 + I 2 .

As the consequence of Lemma 3.1, we have ( π ε ) u ε A 2 2 < π as ε 0 . This together with fractional Trudinger-Moser inequality, for some p > 1 , we can deduce that

I exp ( π ε ) u ε A 2 2 p ( u ε A ) 2 u ε A 2 2 d x C .

With the help of Vitali convergence theorem, we obtain

(3.5) lim ε 0 I 1 = I e π u 0 2 d x = I .

A similar calculation together with Lemma 3.1 leads to

(3.6) lim ε 0 I 2 lim ε 0 λ ε A 2 c ε 2 I u ε > c ε A u ε 2 λ ε e ( π ε ) u ε 2 d x = lim ε 0 λ ε A 2 c ε 2 .

Let A approach to 1 from the aforementioned equation, we have that

lim ε 0 I 2 lim ε 0 λ ε c ε 2 ,

together with the estimate of I 1 , yields that lim ε 0 I e ( π ε ) u ε 2 d x I + lim ε 0 λ ε c ε 2 . To finish the proof of Lemma 3.2, it remains to prove that:

lim ε 0 I e ( π ε ) u ε 2 d x limsup ε 0 λ ε c ε 2 + I .

Indeed, this is a consequence of the following calculation as ε 0 and L ,

lim L lim ε 0 I e ( π ε ) u ε 2 d x = lim L lim ε 0 B L r ε e ( π ε ) u ε 2 d x + I \ B L r ε e ( π ε ) u ε 2 d x lim L lim ε 0 B L r ε e ( π ε ) u ε 2 d x + I \ B L r ε = lim L lim ε 0 λ ε c ε 2 + I .

Therefore, we conclude that

lim ε 0 I e ( π ε ) u ε 2 d x = limsup ε 0 λ ε c ε 2 + I ,

together with lim ε 0 C ε > I , obtain lim ε 0 c ε λ ε = 0 . Then, we finish the proof of Lemma 3.2.□

Lemma 3.3

Set f ε c ε λ ε u ε e ( π ε ) u ε 2 , then for any ϕ C ( I ¯ ) ,

lim ε 0 I f ε ϕ d x = ϕ ( 0 ) .

Proof

Divide

I = u ε > c ε A \ ( R r ε , R r ε ) ( R r ε , R r ε ) u ε c ε A .

Using the change of variables, we have

lim R lim ε 0 R r ε R r ε u ε 2 λ ε e ( π ε ) u ε 2 d x = lim R lim ε 0 R R u ε 2 ( r ε ) λ ε r ε e ( π ε ) u ε 2 ( r ε ) d x = lim R lim ε 0 1 π ε R R u ε 2 ( r ε ) c ε 2 e ( π ε ) [ u ε 2 ( r ε ) c ε 2 ] d x = 1 π lim R R R e η 0 d x = 1 ,

then

lim R lim ε 0 u ε > c ε A \ ( R r ε , R r ε ) f ε ϕ d x lim R lim ε 0 A ϕ L ( I ) u ε > c ε A \ ( R r ε , R r ε ) u ε 2 λ ε e ( π ε ) u ε 2 d x = lim R lim ε 0 A ϕ L ( I ) I u ε 2 λ ε e ( π ε ) u ε 2 d x R r ε R r ε u ε 2 λ ε e ( π ε ) u ε 2 d x = A ϕ L ( I ) 1 lim R lim ε 0 R r ε R r ε u ε 2 λ ε e ( π ε ) u ε 2 d x = 0 .

Similarly,

lim R lim ε 0 R r ε R r ε f ε ϕ d x = lim R lim ε 0 R R u ε c ε λ ε ϕ ( r ε x ) r ε e ( π ε ) u ε 2 ( r ε x ) d x = ϕ ( 0 ) π lim R R R e η 0 d x = ϕ ( 0 ) .

By Vitali convergence theorem and Lemma 3.2,

lim ε 0 u ε c ε A f ε ϕ d x lim ε 0 c ε λ ε ϕ L ( I ) I u ε A e ( π ε ) ( u ε A ) 2 d x lim ε 0 c ε λ ε ϕ L ( I ) I e A ( π ε ) ( u ε A ) 2 d x 1 A I ( u ε A ) A d x 1 A = 0 ,

where 1 A + 1 A = 1 .

Finally, we deduce I f ε ϕ d x ϕ ( 0 ) as ε 0 .□

Next, we are in position to show that the asymptotic behavior of u ε away from origin; we claim that the following lemmas hold.

Lemma 3.4

As ε 0 , we have v ε c ε u ε G 0 0 in L loc ( I ¯ \ { 0 } ) L 1 ( I ) , where G 0 ( y ) = G x ( y ) x = 0 and G x ( y ) = 1 π ln x y + A + g x ( y ) is the Green’s function of ( Δ ) 1 2 on I with singularity at x, which satisfies the following equations:

(3.7) ( Δ ) 1 2 G x ( y ) α G x ( y ) = δ x , x I G x ( y ) = 0 , x R \ I .

Proof

By equation (2.5), c ε u ε satisfies ( Δ ) 1 2 α ( c ε u ε ) = f ε . Arguing as what we did in Lemma 3.3, we obtain f ε L 1 ( R ) 1 as ε 0 . On the other hand, for any K I \ { 0 } , by Lemma 3.1 and fractional Trudinger-Moser inequality, we derive that u ε λ ε e ( π ε ) u ε 2 L p ( K ) for some p > 1 .

According to elliptic regularity theorem for fractional equation, we have u ε u 0 = 0 in L ( K ) . Then, it follows from the definition of f ε and (3.4) of Lemma 3.2 that f ε 0 in L ( K ) as ε 0 . Using Green’s representation formula, we deduce that

v ε ( x ) = I G x ( y ) f ε ( y ) d y G 0 ( y ) I G x ( y ) G 0 ( y ) f ε ( y ) d y + f ε L 1 ( I ) 1 G 0 ( y )

where the expression of G x (y) can refer to [29].

Given x ,

G x ( y ) G 0 ( y ) = 1 π ln y x y + g x ( y ) g 0 ( y ) 1 π ln y x y + g x ( y ) g 0 ( y ) 1 π ln x y y y + C ( δ ) y β 1 π y x + C ( δ ) y β ,

where g x ( y ) C β for some β ( 0 , 1 ) . Then, for any ε 0 , σ 2 and x σ , we can write

lim ε 0 v ε ( x ) lim ε 0 B δ x G x ( y ) G 0 ( y ) f ε ( y ) d y + I \ B δ x G x ( y ) G 0 ( y ) f ε ( y ) d y + o ε ( 1 ) lim ε 0 δ π + δ β x β f ε ( y ) L 1 ( B δ x ) + 1 π x + C ( δ ) f ε ( y ) L 1 ( I \ B δ x ) lim ε 0 δ π + δ β x β + 1 π σ + C ( δ ) f ε ( y ) L 1 ( I \ B δ x ) .

Since δ can be arbitrarily small, we derive that lim ε 0 sup x K v ε ( x ) = 0 . Now, we will show that lim ε 0 v ε ( y ) L 1 ( I ) = 0 . In fact, we just need to prove that lim δ 0 lim ε 0 v ε ( y ) L 1 ( B δ ) = 0 since we have deduced that lim ε 0 v ε ( x ) = 0 in L loc ( I \ { 0 } ) . By Green’s representation formula, we have

lim δ 0 lim ε 0 B δ v ε ( x ) d x lim δ 0 lim ε 0 B δ I G x ( y ) G 0 ( y ) f ε ( y ) d y d x = lim δ 0 lim ε 0 B δ f ε ( y ) B δ G x ( y ) G ( x ) d x d y lim δ 0 C ( δ ) = 0 .□

Since u ˜ ε is the harmonic extension for u ε , with the help of Lemma 3.4, we can obtain the asymptotic estimate u ˜ ε in R + 2 ¯ \ { ( 0 , 0 ) } .

Lemma 3.5

c ε u ˜ ε G ˜ in C loc 0 ( R ¯ + 2 \ { ( 0 , 0 ) } ) C loc 1 ( R ¯ + 2 ) , where

(3.8) G ˜ ( x , y ) = 1 π ln x 2 + y 2 + A + h ( x , y ) , h ( 0 , 0 ) = 0 .

Proof

Denote v ˜ ε c ε u ˜ ε G ˜ ; obviously, v ˜ ε is the harmonic extension for v ε . Hence, for any K R ¯ + 2 \ { ( 0 , 0 ) } and δ < d i s t ( K , ( 0 , 0 ) ) 2 d , we have

sup ( x , y ) K v ˜ ε ( x , y ) 1 π δ δ y v ε ( ξ ) ( x ξ ) 2 + y 2 d ξ + 1 π I \ ( δ , δ ) y v ε ( ξ ) ( x ξ ) 2 + y 2 d ξ I 1 + I 2 .

For I 1 , applying v ε 0 in L 1 ( I ) from Lemma 3.4, we obtain

lim ε 0 I 1 lim ε 0 1 π B δ y v ε ( ξ ) ( x ξ ) 2 + y 2 d ξ lim ε 0 4 diam ( K ) π d 2 B δ v ε ( ξ ) d ξ = 0 .

For I 2 , since v ε 0 in L loc ( I ¯ \ { 0 } ) , we derive that

lim ε 0 I 2 1 π lim ε 0 v ε L ( I \ ( δ , δ ) ) R y ( x ξ ) 2 + y 2 d ξ = lim ε 0 v ε L ( I \ ( δ , δ ) ) = 0 .

Combining the estimates of I 1 and I 2 , we accomplish the proof of Lemma 3.5.□

4 Upper-bound estimate for C π when the concentration-compactness phenomenon arises

In this part, we try to eliminate the concentration-compactness phenomenon of u ε . We will carry out the capacity estimates to derive an upper bound for inequality (1.8).

Lemma 4.1

If c ε , there holds

sup u W 0 1 2 , 2 ( I ) , u 1 2 , α 2 1 I e π u 2 d x I + 2 π e π A .

Proof

Given a large enough L > 0 and a small enough δ > 0 , set

a ε inf B L r ε R + 2 u ˜ ε , b ε sup B δ R + 2 u ˜ ε , υ ε ( u ˜ ε a ε ) b ε .

Due to u ˜ ε 2 2 α u ε 2 2 = 1 , we have

(4.1) ( B δ \ B L r ε ) R + 2 u ˜ ε 2 d x d y = 1 + α u ε 2 2 R + 2 \ B δ + R + 2 B L r ε u ˜ ε 2 d x d y .

The left-hand side is not less than

inf u ˜ R + 2 B L r ε = a ε u ˜ R + 2 B δ = b ε ( B δ \ B L r ε ) R + 2 u ˜ 2 d x d y = ( B δ \ B L r ε ) R + 2 Φ ˜ ε 2 d x d y = π ( a ε b ε ) 2 ln δ ln ( L r ε ) ,

where

Φ ˜ ε = b ε a ε ln δ ln ( L r ε ) ln x 2 + y 2 2 + a ε ln δ b ε ln ( L r ε ) ln δ ln ( L r ε )

is the solution to set of equations

Δ Φ ˜ ε = 0 in R + 2 B δ \ B L r ε Φ ˜ ε = a ε in R + 2 B L r ε Φ ˜ ε = b ε in R + 2 B δ Φ ˜ ε y = 0 in R + 2 ( B δ \ B L r ε ) .

From Proposition 2.2 in [29],

a ε = c ε + 1 π ln L + O ( L 1 ) + o ( 1 ) c ε .

By Lemma 3.5 and the denotation of G ˜ ( x , y ) , we obtain

b ε = 1 π ln δ + A + O ( δ ) + o ( 1 ) c ε .

Next, we start to calculate the right hand of equality (4.1); applying η ε ( x ) η 0 ( x ) = ln 1 1 + x 2 , we have

lim ε 0 c ε 2 R + 2 B L r ε u ˜ ε 2 d x d y = 1 π ln L 2 + O ln L L .

For the integral R + 2 \ B δ u ˜ ε 2 d x d y , we can write

liminf ε 0 R + 2 \ B δ u ˜ ε 2 d x d y 1 c ε 2 R + 2 \ B δ G ˜ 2 d x d y = 1 c ε 2 R + 2 \ B δ G ˜ n G ˜ d σ + ( R × 0 ) \ B δ G ˜ ( x , y ) y y = 0 G ( x ) d x d y = 1 c ε 2 R + 2 \ B δ 1 π δ + O ( 1 ) ln δ π + A + O ( δ ) d σ + α G ( x ) 2 2 = ln δ π + A + O ( δ ln δ ) + α c ε 2 G ( x ) 2 2 .

Gathering the aforementioned estimates, we conclude that

π ( a ε b ε ) 2 ln δ ln ( L r ε ) 1 + α u ε 2 2 ln δ π + A + O ( δ ln δ ) + α G ( x ) 2 2 + 1 π ln L 2 + O ln L L c ε 2 .

Taking the estimates of a ε and b ε into the last equality, we obtain

π ( a ε b ε ) 2 = π c ε 2 2 ln L + O ( L 1 ) + 2 ln δ 2 π A + O ( δ ) + o ( 1 ) + O ( ln 2 δ + ln 2 L ) c ε 2 ln δ L + ln c ε 2 λ ε + ln ( π ε ) + ( π ε ) c ε 2 × 1 ln δ π + A + O ( δ ln δ ) + 1 π ln L 2 + O ln L L c ε 2 = ln δ ln L + ln c ε 2 λ ε + ln ( π ε ) + ( π ε ) c ε 2 + ( π ε ) ln δ π A 1 π ln L 2 + O ( δ ln δ ) + O ln L L + O ( ln 2 δ ) + O ( ln 2 L ) + O ( 1 ) c ε 2 ,

which implies that

ln λ ε c ε 2 π A + ln 2 π + O ( δ ln δ ) + O ln L L + o ε ( 1 ) .

Then, letting ε 0 and L , we obtain

limsup ε 0 ln λ ε c ε 2 π A + ln 2 π ,

together with Lemma 3.2 ends the proof of Lemma 4.1.□

5 Existence of the extremals

In this section, we construct a test function whose energy can exceed the upper bound I + 2 π e π A to show the existence of extremals for the fractional Trudinger-Moser inequality of Tintarev type (1.8).

Lemma 5.1

There exists a sequence of function ϕ ε W 0 1 2 , 2 ( I ) with ϕ ε 1 2 , α 2 1 such that

(5.1) I e π ϕ ε 2 d x > I + 2 π e π A ,

when ε is small enough.

Proof

Define

Γ L ε { ( x , y ) R + 2 : G ˜ ( x , y ) = γ L ε min R + 2 B L ε G ˜ } ,

and I L ε { ( x , y ) R + 2 : G ˜ ( x , y ) > γ L ε } . The accurate formula of G ˜ gives

(5.2) γ L ε = ln L ε π + A + O ( L ε ) .

Let

Ψ ε ( x , y ) = c ln 1 + y ε 2 + x 2 ε 2 + B 2 π c , ( x , y ) R + 2 B L ε ( 0 , ε ) γ L ε c , ( x , y ) I L ε \ B L ε ( 0 , ε ) G ˜ ( x , y ) c , ( x , y ) R + 2 \ I L ε ,

where c , B , and L depend only on ε and will be determined later. The choice of B is to make sure the continuity on R + 2 B L ε ( 0 , ε ) , so

c ln L 2 + B 2 π c = γ L ε c .

In view of (5.2), one can deduce that

(5.3) B = 2 π c 2 + 2 ln ε 2 π A + O ( L ε ) .

Choosing suitable constant c such that Ψ ε 2 2 α ϕ ε 2 2 = 1 , where ϕ ε ( x ) Ψ ε ( x , 0 ) . Direct calculation leads to

R + 2 B L ε ( 0 , ε ) Ψ ε 2 d x d y = 1 ( 2 π c ) 2 R + 2 B L ε ( 0 , ε ) ln 1 + y ε 2 + x 2 ε 2 2 d x d y = 1 ( 2 π c ) 2 R + 2 B L ( 0 , 1 ) ln ( ( 1 + y ) 2 + x 2 ) 2 d x d y = 1 c 2 1 π ln L 2 + O ln L L ,

R + 2 I L ε Ψ ε 2 d x d y = 1 c 2 R + 2 I L ε G ˜ 2 d x d y = 1 c 2 R + 2 I L ε G ˜ n G ˜ d σ + 1 c 2 ( R × { 0 } ) \ I ¯ L ε G ˜ ( x , y ) y y = 0 G ( x ) d x = 1 c 2 ln L ε π + A + O ( L ε ln L ε ) + α G ( x ) 2 2

and

I ϕ ε 2 d x = B ε L 2 1 c ln 1 + x 2 ε 2 + B 2 π c 2 d x + I \ B ε L 2 1 G 2 c 2 d x = B ε L 2 1 c ln 1 + x 2 ε 2 + 2 π c 2 + 2 ln ε 2 π A + O ( L ε ) 2 π c 2 d x + I \ B ε L 2 1 G 2 c 2 d x = B ε L 2 1 2 π G + O ( L ε ln L ε ) 2 π c 2 d x + I \ B ε L 2 1 G 2 c 2 d x = 1 c 2 I G 2 d x + O ( L ε ln L ε ) .

Then, it holds

(5.4) ln 2 ε + π A + O ( L ε ln L ε ) + O ln L L = π c 2

and c + as ε 0 . Combining this with (5.3), we derive that

(5.5) B = 2 ln 2 + O ( L ε ln L ε ) + O ln L L .

Using the definition of ϕ ε , together with (5.4) and (5.5), yields that

B ε L 2 1 e π ϕ ε 2 d x = ε B L 2 1 exp π ( c ln ( 1 + x 2 ) + B 2 π c ) 2 d x > ε B L 2 1 e π c 2 B 1 1 + x 2 d x = 2 e π A + O ( L ε ln L ε ) + O ln L L π ( 1 + O ( L 1 ) ) = 2 π e π A + O ( L ε ln L ε ) + O ln L L

and

I \ B ε L 2 1 e π ϕ ε 2 d x I \ B ε L 2 1 ( 1 + π ϕ ε 2 ) d x = I \ B ε L 2 1 + 1 c 2 I \ B ε L 2 1 π G 2 d x > I 2 ε L + 1 c 2 I \ B ε L 2 1 π G 2 d x I 2 ε L + ν L ε c 2 ,

with ν L ε > ν 1 2 > 0 for L ε < 1 2 . We can see that π c 2 = ln ε + O ( 1 ) by equality (5.4), and when we choose L = ln 2 ε ,

O ( L ε ln L ε ) + O ln L L 2 ε L = O ln ln ε ln 2 ε = o 1 c 2 ,

which can conclude that

I e π ϕ ε 2 d x > I + 2 π e π A + ν 1 2 c 2 + o 1 c 2 > I + 2 π e π A .

Dirichlet energy principle gives ϕ ˜ ε 2 2 Ψ ε 2 2 , that is to say,

ϕ ε 1 2 , α 2 Ψ ε 2 2 α ϕ ε 2 2 = 1 .

Hence, the proof of Lemma 5.1 is accomplished when ε is small enough.□

  1. Funding information: Lu Chen was partly supported by the National Natural Science Foundation of China (No. 12271027) and a grant from Beijing Institute of Technology (No. 2022CX01002). Maochun Zhu was supported by Natural Science Foundation of China (No. 12071185).

  2. Conflict of interest: The authors state that there is no conflict of interest.

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Received: 2022-08-31
Revised: 2023-04-08
Accepted: 2023-04-16
Published Online: 2023-05-29

© 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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