We establish Liouville-type theorems for the three-dimensional stationary fractional magnetohydrodynamic (MHD) system with different orders of dissipation. Our first result shows that every smooth solution satisfying the natural homogeneous Sobolev energy conditions is trivial whenever 1≤α≤5/3 and 3≤α+2β≤5, without any additional integrability assumptions on the velocity or magnetic fields. This extends previous results to new parameter regimes, including cases with β<1. Beyond this region, we prove a complementary Liouville theorem under suitable integrability conditions only on the radial components of the velocity and magnetic fields. The proofs rely on the Caffarelli–Silvestre extension and localized energy estimates.
Introduction and main results
The Liouville problem for the stationary Navier–Stokes equations in R3 asks whether a smooth solution must vanish identically under suitable assumptions on its behavior at infinity. A classical version of this problem concerns solutions with finite Dirichlet integral,
∫R3∣∇u∣2dx<∞,
and remains open in its full generality. An important contribution was made by Galdi, who proved that the additional assumption u∈L9/2(R3) is sufficient to guarantee triviality. Since then, a number of Liouville-type criteria have been established under different integrability and regularity assumptions; see, for instance, [1, 8, 11, 16, 17, 20, 21] and the references therein.
A natural extension of this problem is obtained by replacing the Laplacian with a fractional power (−Δ)α/2. This type of dissipation, which goes back to the work of J.-L. Lions [13], allows one to study stationary flows with different orders of dissipation. For the stationary fractional Navier–Stokes equations, Liouville-type results have been obtained in several settings; see, among others, [24, 23, 10, 15, 9, 12, 14]. The relation between the dissipation exponent and the integrability of the velocity field is particularly relevant here. Indeed, the homogeneous Sobolev embedding
H˙α/2(R3)↪L3−α6(R3)
shows that the exponent 9/2 in Galdi’s criterion corresponds precisely to α=5/3. This observation provides a natural reference point for understanding the range of fractional dissipation considered in this paper.
Our main interest is the stationary magnetohydrodynamic (MHD) system, which describes the interaction between the velocity field of an electrically conducting fluid and its magnetic field. In this system, the velocity u and the magnetic field b are coupled through the Lorentz force and the induction equation, while Π denotes the total pressure. For the classical stationary MHD equations, several Liouville-type theorem are available in the literature. See, for instance, [4, 5, 6, 18, 3]. The fractional setting introduces an additional difficulty in that the velocity and magnetic fields may have different dissipation orders, denoted by α and β, respectively. As a consequence, the two fields need not have the same regularity, and the interaction between their dissipative effects becomes an essential part of the analysis.
To the best of our knowledge, relatively few works have addressed Liouville-type theorems for the stationary fractional MHD system. Among the relevant contributions, we mention the results of Zeng [26] and Lee–Lee [12]. These works provide important criteria for the triviality of solutions, but leave room to investigate parameter ranges in which the two dissipation orders interact more directly. Thus, our purpose is to establish such criteria under the natural energy assumptions
u∈H˙α/2(R3),b∈H˙β/2(R3),
without imposing additional integrability assumptions on either field in the parameter ranges covered by our first theorem.
More precisely, we consider the stationary fractional MHD system in R3:
\begin{aligned}
(-\Delta)^{\alpha/2}u + (u \cdot\nabla)u + \nabla\Pi&= (b \cdot\nabla)b,\\
(-\Delta)^{\beta/2}b + (u \cdot\nabla)b &= (b \cdot\nabla)u,\\
\nabla\cdot u &= 0,\qquad\nabla\cdot b = 0,
\end{aligned}
\qquad0 < \alpha,\beta< 2, \tag*{(1)}\end{aligned}
with the uniform decay conditions
u(x)⟶0,b(x)⟶0,as ∣x∣⟶∞.
Here, the fractional Laplacians are defined through the Fourier multipliers with symbols ∣ξ∣α and ∣ξ∣β. The system includes the stationary fractional Navier–Stokes equations when b≡0, while the choice α=β=2 formally recovers the classical stationary MHD system.
Our first result identifies a region in the (α,β)-plane where the energy assumptions alone imply that both fields vanish. To continue, we introduce the set
A:={α,β∈(0,2):1≤α≤35,3≤α+2β≤5}.
The significance of this region is that the admissible dissipation orders are not restricted to zones of the plane where β≥1. Instead, the mixed interaction between the velocity and magnetic fields leads to a more flexible condition which exploits the combination α+2β.
Theorem 1.1. Let (u,b) be a smooth solution of (1) such that
u∈H˙α/2(R3),b∈H˙β/2(R3),
with (α,β)∈A. Then
u≡0,b≡0.
Remark 1.1. The parameter region in Theorem 1.1 strictly contains the parameter regions obtained by Zeng [26] and Lee–Lee [12], which are given, respectively, by
BZeng={(α,β):1≤α,β≤35}
and
BLee−Lee={(α,β):1≤α<35,35<β<2,α+2β<5}.
In particular, our result covers points on the line α+2β=5 with 1≤α<5/3, as well as a triangular region in which β<1. In this latter range, the Sobolev embedding for the magnetic field gives an exponent below 3, so the theorem applies even when the magnetic field does not belong to the Lebesgue spaces required by the previous criteria. The key point is that we retain the mixed terms involving u and b in the energy-flux estimates, rather than estimating them separately by purely cubic terms. This preserves the interaction between the two dissipation orders and allows us to work under the single balance condition 3≤α+2β≤5, without requiring an independent lower bound on β. In the following figure we sketch these sets alongside A to provide the reader with a graphical comparison.
Figure 1. The sets A, BLee−Lee and BZeng in the common window (0,2)1. Solid edges belong to the set, while black dashed edges do not. The gray dashed lines are the reference lines α=1, α=35, β=35, α+2β=3 and α+2β=5, common to the three panels.
An immediate consequence of Theorem 1.1 is a Liouville theorem for the stationary fractional Navier–Stokes equations. In fact, by setting b≡0, the MHD system reduces to the fractional Navier–Stokes system, and the magnetic dissipation exponent β can be chosen freely, provided that (α,β)∈A. This observation allows us to obtain the following result throughout the range 1≤α≤5/3, without any additional integrability assumption on the velocity field. To the best of our knowledge, Zeng was the first to establish this conclusion in the same range; see [26 Corollary 1.5]. Our proof, however, follows a different approach.
Corollary 1.1. Let 1≤α≤35, and let u∈H˙2α(R3) be a smooth solution of
(−Δ)2αu+(u⋅∇)u+∇Π=0,∇⋅u=0in R3.
Then u≡0.
We next consider the parameter ranges outside A. In this setting, we show that triviality can still be obtained by imposing suitable integrability assumptions on the radial components of the velocity and magnetic fields,
uρ:=u⋅∣x∣x,bρ:=b⋅∣x∣x.
This approach is motivated by recent Liouville-type theorems for the classical and fractional stationary Navier–Stokes equations [9, 22]. In contrast to conditions imposed on individual Cartesian components, assumptions on radial components are invariant under rotations about the origin. Moreover, they do not require additional integrability of the tangential components of either field.
Our second result extends this perspective to the stationary fractional MHD system. It covers the parameter region outside A, except for a region where the requirements arising from the velocity and magnetic fluxes are incompatible within our method. In particular, our theorem distinguishes the cases in which the radial integrability assumptions are needed for the velocity field, for the magnetic field, or for both. We present the result below.
Theorem 1.2. Let 0<α,β<2, and let (u,b) be a smooth solution of (1) satisfying u∈H˙α/2(R3), b∈H˙β/2(R3). Assume that uρ∈Lr1(R3) and bρ∈Lr2(R3) for r1,r2∈[1,∞] such that
(R1)r1≥α3if α<1,r1≤α−13if α>35,
(R2)r1≥β3if α+2β<3,r1≤β−13if α+2β>5,
(R3)r2≥α+β6if α+2β<3,r2≤α+β−26if α+2β>5.
Then u≡0 and b≡0.
Some remarks are in order.
Remark 1.2. We stress that Theorem 1.2 requires additional integrability assumptions only on the radial components of the velocity and magnetic fields, namely uρ and bρ, without imposing any further integrability conditions on their tangential components of u and of b. In particular, the criterion depends only on these two components, while the remaining components are constrained only by the Sobolev regularity assumed in the statement of the theorem.
Remark 1.3. For comparison, Zeng’s Liouville theorem for the stationary fractional MHD system in [26] is based on the assumption that
(uj,bj)∈Lpj(R3)×Lqj(R3),j=1,2,3,
where pj=(pj,1,pj,2,pj,3) and qj=(qj,1,qj,2,qj,3), with pj,l,qj,l∈[3,∞) satisfying
l=1∑3pj,l1≥32,l=1∑3qj,l1≥32,j=1,2,3.
Thus, Zeng’s result imposes anisotropic integrability conditions on each Cartesian component of both fields, combining different integrability requirements along the coordinate directions to ensure the triviality of the solution. By contrast, Theorem 1.2 assumes only
uρ∈Lr1(R3),bρ∈Lr2(R3),
for exponents r1,r2∈[1,∞] satisfying (R1)–(R3). These restrictions depend on the fractional orders α and β and allow us to formulate the Liouville criterion entirely in terms of the radial components, rather than imposing additional integrability conditions on each Cartesian component of the two fields.
Remark 1.4. The conditions (R1)–(R3) are active only in some parts of (0,2)2. Thus, writing them, one finds the following list, where the Roman numerals refer to Figure 2.
Figure 2. The region A (shaded in blue), where no radial hypothesis is needed, and the regions I–VI and G of Remark 1.4 in the square (0,2)2. The dashed lines are α=1, α=35, α+2β=3 (from (0,23) to (2,21)) and α+2β=5.
region
condition on uρ
condition on bρ
A
1≤α≤35,3≤α+2β≤5
none
none
I
α<1,α+2β<3
r1≥min{α,β}3
r2≥α+β6
II
α<1,α+2β≥3
r1≥α3
none
III
1≤α≤35,α+2β<3
r1≥β3
r2≥α+β6
IV
1≤α≤35,α+2β>5
r1≤β−13
r2≤α+β−26
V
α>35,3≤α+2β≤5
r1≤α−13
none
VI
α>35,α+2β>5
r1≤max{α,β}−13
r2≤α+β−26
G
α>35,α+2β<3
incompatible requirements
—
Table 1.
In particular, on A, Theorem 1.2 contains no radial hypothesis and reduces to Theorem 1.1, whereas on each of the regions I–VI it provides a result with a one-sided condition.
Remark 1.5.The region G. For α>35 and α+2β<3 (so that β<32) the requirements coming from the terms ∣u∣2uρ and ∣b∣2uρ push r1 in opposite directions. The former asks for r1≤α−13 and the latter for r1≥β3, and β3>α−13 because α−β>1 there.
Remark 1.6.The case b≡0. If b≡0, the second equation in (1) is trivially satisfied and the first one is the stationary fractional Navier–Stokes system with dissipation (−Δ)α/2. Only the terms ∣u∣2uρ and Πuuρ appear in the flux, so only (R1) is used. It requires r1≥α3 if α<1, nothing if 1≤α≤35, and r1≤α−13 if 35<α<2. For 35<α<2, the range treated in [9], this contains the condition α3≤r1≤α−13 of that paper.
The paper is organized as follows. In Section 2, we recall the Caffarelli–Silvestre extension and its main properties. Sections 3 and 4 contain the proofs of Theorems 1.1 and 1.2, respectively.
Given R>1, in what follows, and throughout this paper, we use the notation
CR:={x∈R3:R<∣x∣<2R}.
We let ψ∈C∞(R3) be a smooth radial non-increasing cut-off function such that 0≤ψ≤1, ψ(x)=1 for ∣x∣≤1, and ψ(x)=0 for ∣x∣≥2. Given R>1, set ψR(x)=ψ(Rx).
We also consider a non-increasing function χ∈C∞([0,∞)) such that χ(y)=1 for y≤1 and χ(y)=0 for y≥2. Given R>1, we define χR(y)=χ(Ry). Note that ∣∇ψR∣≤CR−1, ∣ΔψR∣≤CR−2, ∣χR′∣≤CR−1 and ∣χR′′∣≤CR−2, for some absolute constant C>0.
Preliminaries
Since the operators (−Δ)α/2 and (−Δ)β/2 are nonlocal, some of the classical arguments used to prove Liouville type theorems for the stationary Navier–Stokes and MHD equations cannot be carried over directly. Instead, we make use of the Caffarelli–Silvestre extension, which allows one to represent a fractional Laplacian on R3 as the boundary trace of a local problem involving the operator Δˉ in the half-space R+4. In the following, we shall write ∇ˉ, div and Δˉ for the differential operators associated with the extended variables in R+4. Since the two equations in (1) involve different fractional Laplacians, we will need two extensions, one for u and one for b, with different weights. For this reason we state the result for a generic exponent σ.
Theorem 2.1.[7] Given σ∈(0,2), consider v∈H˙σ/2(R3), μ=1−σ, and the weighted homogeneous energy space H˙1(R+4,yμ), obtained as the completion of Cc∞(R+4) with respect to the seminorm
∥w∥H˙1(R+4,yμ):=(∫R+4yμ∣∇ˉw∣2dxdy)1/2.
Then v admits a unique extension v∗∈H˙1(R+4,yμ) satisfying
Δˉμv∗(x,y):=Δˉv∗+yμ∂yv∗=yμ1div(yμ∇ˉv∗)=0,
and
v∗(x,0)=v(x).
In addition, there exists Cσ>0, depending only on σ, such that:
(1) the operator (−Δ)2σv is given by
(−Δ)2σv(x)=−y→0limCσ(yμ∂yv∗(x,y)),
(2) and, the energy equality
∫R3∣(−Δ)4σv∣2dx=Cσ∫R+4yμ∣∇ˉv∗∣2dxdy.
Moreover, v∗(⋅,y)=Py(σ)∗v, where Py(σ)(x)=c3,σyσ(∣x∣2+y2)−23+σ is the fractional Poisson kernel and c3,σ>0 is chosen so that ∥Py(σ)∥L1(R3)=1.
In what follows we write
μ:=1−α,ν:=1−β,p:=3−α6,q:=3−β6,
so that, by the Sobolev embedding, u∈Lp(R3) and b∈Lq(R3). We denote by u∗ and b∗ the Caffarelli–Silvestre extensions of u and b, associated with the weights yμ and yν respectively, and by Cα, Cβ the corresponding constants given by Theorem 2.1. Note that μ,ν>−1 because α,β<2.
Proof of Theorem 1.1
We begin with two lemmas that will be used in the proof of Theorem 1.1. The first is stated for a generic exponent, so that it can be applied both to u and to b. Its proof is analogous to that of [9]; we include it here for completeness. The proof of the second is postponed to the end of this section.
Lemma 3.1. Let σ∈(0,2), v∈H˙σ/2(R3) and let v∗ be its Caffarelli–Silvestre extension. For every R>1 let ER⊆B2R be a measurable set. Then
R21∫02R∫ERy1−σ∣v∗∣2dxdyR→∞0.
Lemma 3.2. Let (α,β)∈A, u∈H˙α/2(R3), b∈H˙β/2(R3). Let Π be the pressure defined in (3) below. Then
Proof of Theorem 1.1. To begin, note that, since u∈H˙α/2(R3) and b∈H˙β/2(R3), the Sobolev embedding gives u∈Lp(R3) and b∈Lq(R3). Since α,β>0 we have p,q>2, and therefore uiuj∈Lp/2(R3) and bibj∈Lq/2(R3) with 1<2p,2q<+∞. Then, taking the divergence of the momentum equation and using ∇⋅u=∇⋅b=0, we obtain the elliptic equation
−ΔΠ=∂i∂j(uiuj−bibj)=:f.(2)
Now, since (2) determines Π only up to an additive harmonic function, we fix the pressure through the Calderón–Zygmund representation
We claim that this is the only solution of (2) in L2p(R3)+L2q(R3). Indeed, if Π is another solution in this space, then h:=Π−Π=h1+h2 is harmonic on R3, with h1∈L2p(R3) and h2∈L2q(R3). Thus, considering the mean value property and Hölder’s inequality, for every x∈R3 and ρ>0,
thus, we get h≡0. Throughout the paper, Π always denotes this normalized pressure. On the other hand, since u and b are smooth, by using elliptic regularity theory on (2), we conclude that the pressure term Π is also smooth.
Then, testing the first equation of (1) with ψRu and the second one with ψRb, using ∇⋅u=∇⋅b=0 and integrating by parts, we get
We next treat the fractional dissipation terms on the left-hand side by means of the Caffarelli–Silvestre extension. For this purpose, we consider Φ(x,y):=ψR(x)χR(y) and the identity (see [23 Eq. (3.2)]), applied to each component of u with σ=α and to each component of b with σ=β,
where C depends on κ but not on R. Take (v,κ)=(u,μ) and (v,κ)=(b,ν). Then, applying Lemma 3.1 (with σ=α, respectively σ=β) with ER=CR, we conclude that the first term on the right-hand side tends to zero as R→∞. On the other hand, since yκ∣v∗∣2≥0, we can write
∫R2R∫B2Ryκ∣v∗∣2dxdy≤∫02R∫B2Ryκ∣v∗∣2dxdy.
therefore, considering Lemma 3.1 with ER=B2R we obtain that the second term tends to zero also. Considering the same approach for b∗, we conclude
where we used ∣(u⋅b)(b⋅∇ψR)∣≤∣u∣∣b∣2∣∇ψR∣. By Lemma 3.2, the right-hand side tends to zero as R→∞.
Thus, provided with these results, we take the limit as R→∞ in (8). Since ψ is radial and non-increasing, and χ is non-increasing, Φ=ΦR increases pointwise to 1 as R→∞, and the monotone convergence theorem applied to the left-hand side of (8) yields
Cα∫R+4yμ∣∇u∗∣2dxdy+Cβ∫R+4yν∣∇b∗∣2dxdy=0.
Thus, since Cα,Cβ>0, the both integrals above vanish. Hence, we conclude that u∗ and b∗ are constant in R+4, and so are their traces u(x)=u∗(x,0) and b(x)=b∗(x,0). Then, considering that u∈Lp(R3) and b∈Lq(R3), and the fact that the only constant function belonging to Lr(R3), r<∞, is the zero function, we conclude that u≡0 and b≡0. This finishes the proof. □
Proof of Lemma 3.1. In the following we denote by qσ the Sobolev exponent, i.e. qσ:=3−σ6>2, and we write κ:=1−σ∈(−1,1).
By Theorem 2.1, the Caffarelli–Silvestre extension can be written as
v∗(x,y)=Py(σ)∗v(x).
By Young’s inequality,
∥v∗(⋅,y)∥Lqσ(R3)≤∥v∥Lqσ(R3).(9)
Now, considering Hölder inequality with qσ/21+qσ/(qσ−2)1=1, we get
Let ε>0. Now considering that Cc∞(R3) is dense in Lqσ(R3), we can choose vε∈Cc∞(R3)⊂L1∩Lqσ(R3) such that ∥v−vε∥Lqσ<ε/2. Then, considering Young inequality, we can write
∥Py(σ)∗vε∥Lqσ≤∥Py(σ)∥Lqσ∥vε∥L1.
Now, note that, by rescaling we have Py(σ)(x)=y−3P1(σ)(x/y), and then we obtain
On the other hand, considering (9) and the fact that κ=1−σ>−1 (since σ<2) we have
tκ∥v∗(⋅,Rt)∥Lqσ2≤tκ∥v∗∥Lqσ2∈Lt1(0,2).
Moreover, using (11), for all t∈(0,2) we have ∥v∗(⋅,Rt)∥Lqσ2→0 as R→∞. Then, considering the Dominated Convergence Theorem and (10), we conclude the claim of the lemma. □
Proof of Lemma 3.2. To begin, recall that p=3−α6 and q=3−β6. Then, since u∈H˙2α(R3) and b∈H˙2β(R3), by the Sobolev embedding we have u∈Lp(R3) and b∈Lq(R3), and 3≤p≤29 because 1≤α≤35.
We first record an elementary scaling estimate. Let ρ1,ρ2,ρ3∈[1,∞] be such that
θ:=1−ρ11−ρ21−ρ31∈[0,1).
Then, by Hölder’s inequality with exponents ρ1,ρ2,ρ3,θ1, and using that ∥∇ψR∥L∞≤CR−1 and ∣CR∣≤CR3, we have, for all R>1 that
where I1(R) contains ∣u∣3, I2(R) contains ∣b∣2∣u∣, and I3(R) contains the pressure. With this in hand, we aim to prove
R→+∞limI1(R)=R→+∞limI2(R)=R→+∞limI3(R)=0.
The term I1. We apply (12) with (ρ1,ρ2,ρ3)=(p,p,p), for which θ1=1−p3=2α−1∈[0,31]. Then 3θ1−1=23α−5≤0, since α≤35, and we obtain
I1(R)≤C∥u∥Lp(CR)3.
Thus, considering that limR→∞∥u∥Lp(CR)=0, we conclude I1(R)→0 as R→+∞.
The term I2. We apply (12) with (ρ1,ρ2,ρ3)=(p,q,q), for which
θ2=1−p1−q2=1−63−α−33−β=6α+2β−3≥0,(13)
and 3θ2−1=2α+2β−5≤0, by the assumption 3≤α+2β≤5. Hence
I2(R)≤C∥u∥Lp(CR)∥b∥Lq(CR)2→0as R→+∞,
since ∥b∥Lq(CR)≤∥b∥Lq(R3)<+∞ and ∥u∥Lp(CR)→0.
The term I3. We split Π=Π1+Π2 as in (3). For Π1 we apply (12) with (ρ1,ρ2,ρ3)=(2p,p,∞) and f3≡1, which gives the same θ1=1−p2−p1=2α−1 as before. Note that ∥f3∥L∞(CR)=1, so no volume factor appears, the only power of R is R3θ1−1≤1, coming from ∥∇ψR∥L1/θ1(CR). Hence, by (4), we can write
Hence, we conclude that I3(R)→0 as R→+∞. Then, by gathering together the limits for I1(R), I2(R) and I3(R), we deduce the desired limit. □
Proof of Theorem 1.2
We begin with the lemma that will be used in the proof of Theorem 1.2, whose proof is presented in Subsection 4.1. The other tool we need, namely Lemma 3.1, was already stated and proved in § 3 for a generic exponent.
Lemma 4.1.Assume the hypotheses of Theorem 1.2. Then
Proof of Theorem 1.2. The proof follows the lines of that of Theorem 1.1, and we only indicate the changes. We use the pressure Π=Π1+Π2 of (3) and the cut-offs ψR, χR and ΦR applied there. In this section we also write Πu:=Π1 and Πb:=−Π2, so that Π=Πu−Πb and, by (4),
Since ψR is radial, we have ∇ψR(x)=∂ρψR(x)∣x∣x, with ∣∂ρψR∣=∣∇ψR∣≤CR−1. Hence, we can write
u⋅∇ψR=uρ∂ρψR,b⋅∇ψR=bρ∂ρψR.
Testing the equations with ψRu and ψRb, using the Caffarelli–Silvestre extension and arguing exactly as in the proof of Theorem 1.1, we arrive at (8), and the two terms on the right-hand side of (8) involving u∗ and b∗ tend to zero as R→∞, by Lemma 3.1. The only difference is the treatment of the flux term, which now we write using u⋅∇ψR=uρ∂ρψR, b⋅∇ψR=bρ∂ρψR, Π=Πu−Πb and ∣u⋅b∣≤∣u∣∣b∣:
By Lemma Lemma 4.1, the right-hand side tends to zero as R→∞. Thus, taking the limit as R→∞ in (8), and using the monotone convergence theorem as in the proof of Theorem Theorem 1.1, we get
Cα∫R+4yμ∣∇u∣2dxdy+Cβ∫R+4yν∣∇b∣2dxdy=0.
Hence u and b are constant, and then, since u∈Lpα(R3) and b∈Lpβ(R3) by the Sobolev embedding, and the only constant function belonging to Lp(R3), p<∞, is the zero function, we conclude that u≡0 and b≡0. This finishes the proof. □
Proof of Lemma 4.1
To begin, we stress the fact that each term in the proof below is estimated by Hölder’s inequality. This requires an exponent σ for uρ or bρ such that
0≤τ−σ1≤31.
for a suitable τ. The following elementary lemma gives a criterion for the existence of such an exponent.
Lemma 4.2. Let τ∈(0,1), p∈(1,∞), r∈[1,∞], and
g∈Lp(R3)∩Lr(R3).
Assume that
r1≤τifp1>τ,r1≥τ−31ifp1<τ−31.(14)
Then there exists σ∈(1,∞) such that
g∈Lσ(R3),0≤τ−σ1≤31.
Proof. By interpolation, g∈Lσ(R3) whenever 1/σ lies between 1/p and 1/r. We choose 1/σ by projecting 1/p onto the interval [τ−31,τ], more precisely
σ1=min{max{p1,τ−31},τ}.
In the following we distinguish three cases. If
τ−31≤p1≤τ,
we take σ=p, and the conclusion follows. If 1/p>τ, then 1/σ=τ. The first condition in (13) gives 1/r≤τ<1/p, thus 1/σ lies between 1/r and 1/p, and then g∈Lσ(R3). Finally, if 1/p<τ−31, then 1/σ=τ−31. The second condition in (13) gives
p1<τ−31≤r1,
and thus, considering again interpolation, we get g∈Lσ(R3). In particular, note that in all three cases we have
0≤σ1≤τ<1.
Thus, we conclude that 1<σ<∞, and 0≤τ−σ1≤31. This finishes the proof. □
In the next, we apply this lemma with ∣uρ∣≤∣u∣ and ∣bρ∣≤∣b∣. At this point is convenient to recall that
Proof of Lemma 4.1. To begin, recall that pα=3−α6 and pβ=3−β6. Then, since u∈H˙2α(R3) and b∈H˙2β(R3), by the Sobolev embedding we have u∈Lpα(R3) and b∈Lpβ(R3), and by the Calderón–Zygmund estimate (4) we have Πu∈L2pα(R3) and Πb∈L2pβ(R3). Moreover, let σ1,σ2,σ3∈[1,∞] be the exponents constructed in the previous subsection, so that
uρ∈Lσ1(R3)∩Lσ2(R3),bρ∈Lσ3(R3),
and the numbers θ1,θ2,θ3 defined in (15) belong to [0,31].
We first record an elementary estimate. Let ϱ1,ϱ2,ϱ3∈[1,∞] be such that
θ:=1−ϱ11−ϱ21−ϱ31∈[0,31].
Then, by Hölder’s inequality with exponents ϱ1,ϱ2,ϱ3,θ1, and using that ∥∂ρψR∥L∞≤CR−1 and ∣CR∣≤CR3, we have, for all R>1,
where I1 contains ∣u∣2∣uρ∣, I2 contains ∣b∣2∣uρ∣, I3 and I4 contain ∣Πu∣∣uρ∣ and ∣Πb∣∣uρ∣ respectively, and I5 contains ∣u∣∣b∣∣bρ∣. With this in hand, we aim to prove that limR→+∞Ik(R)=0 for k=1,…,5.
The term I1. Since ∣uρ∣≤∣u∣ and pα1=21−6α, we apply (16) with (ϱ1,ϱ2,ϱ3)=(pα,pα,σ1), for which
θ=1−pα2−σ11=3α−σ11=θ1∈[0,31].
Hence
I1(R)≤C∥u∥Lpα(R3)2∥uρ∥Lσ1(CR).
The term I2. We apply (16) with (ϱ1,ϱ2,ϱ3)=(pβ,pβ,σ2), for which θ=1−pβ2−σ21=3β−σ21=θ2∈[0,31]. Hence
I2(R)≤C∥b∥Lpβ(R3)2∥uρ∥Lσ2(CR).
The terms I3 and I4. We apply (16) with f3≡1 and ϱ3=∞, so that no volume factor appears and the only power of R is the one in (16). For I3 we take (ϱ1,ϱ2,ϱ3)=(2pα,σ1,∞), which gives θ=1−pα2−σ11=θ1, and for I4 we take (ϱ1,ϱ2,ϱ3)=(2pβ,σ2,∞), which gives θ=θ2. Then, by (4),
The term I5. We apply (16) with (ϱ1,ϱ2,ϱ3)=(pα,pβ,σ3), for which θ=1−pα1−pβ1−σ31=6α+β−σ31=θ3∈[0,31]. Hence
I5(R)≤C∥u∥Lpα(R3)∥b∥Lpβ(R3)∥bρ∥Lσ3(CR).
Finally, since uρ∈Lσ1∩Lσ2 and bρ∈Lσ3 with σ1,σ2,σ3<∞, we have ∥uρ∥Lσi(CR)→0 for i=1,2 and ∥bρ∥Lσ3(CR)→0 as R→+∞, being tails of convergent integrals. Since ∥u∥Lpα and ∥b∥Lpβ are finite, we get limR→+∞Ik(R)=0 for k=1,…,5. Then, by gathering together these limits, we deduce the desired limit. □
Datasets. Data sharing does not apply to this article as no datasets were generated or analyzed during the current study.
Conflict of interest. In addition, the authors declare no conflict of interest and confirm that they contributed equally to this paper.
References
Beijing International Center for Mathematical Research, Peking University, No. 5 Yiheyuan Road Haidian District, Beijing 100871, People’s Republic of China
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