arXiv is now an independent nonprofit! Learn more
License: arXiv.org perpetual non-exclusive license
arXiv:2305.01046v1 [math.AP] 01 May 2023

On the existence and structures of almost axisymmetric solutions to 33-D Navier-Stokes equations

Yanlin Liu Y. LiuSchool of Mathematical Sciences, Laboratory of Mathematics and Complex Systems, MOE, Beijing Normal University, 100875 Beijing, China. Email address: liuyanlin@bnu.edu.cn and Li Xu L. XuSchool of Mathematical Sciences, Beihang University, 100191 Beijing, China Email address: xuliice@buaa.edu.cn
Date: August 24, 2026
Abstract.

In this paper, we consider 33-D Navier-Stokes equations with almost axisymmetric initial data, which means that by writing 𝒖0=u0r𝒆r+u0θ𝒆θ+u0z𝒆z\boldsymbol{u}_{0}=u^{r}_{0}\boldsymbol{e}_{r}+u^{\theta}_{0}\boldsymbol{e}_{\theta}+u^{z}_{0}\boldsymbol{e}_{z} in the cylindrical coordinates, then θu0r,θu0θ\partial_{\theta}u^{r}_{0},\,\partial_{\theta}u^{\theta}_{0} and θu0z\partial_{\theta}u^{z}_{0} are small in some sense (recall axisymmetric means these three quantities vanish). Then with additional smallness assumption on u0θu^{\theta}_{0}, we prove the global existence of a unique strong solution 𝒖\boldsymbol{u}, and this solution keeps close to some axisymmetric vector field. We also establish some refined estimates for the integral average in θ\theta variable for 𝒖\boldsymbol{u}.

Moreover, as u0r,u0θu^{r}_{0},\,u^{\theta}_{0} and u0zu^{z}_{0} here depend on θ\theta, it is natural to expand them into Fourier series in θ\theta variable. And we shall consider one special form of 𝒖0\boldsymbol{u}_{0}, with some small parameter ε\varepsilon to measure its swirl part and oscillating part. We study the asymptotic expansion of the corresponding solution, and the influences between different profiles in the asymptotic expansion. In particular, we give some special symmetric structures that will persist for all time. These phenomena reflect some features of the nonlinear terms in Navier-Stokes equations.

Keywords: Navier-Stokes equations, axisymmetric, asymptotic expansions.

1. Introduction

1.1. The general setting

The 3-D incompressible Navier-Stokes equations (N-S) reads:

(1.1) {t𝒖+𝒖𝒖Δ𝒖+P=𝟎,(t,x)+×3div𝒖=0,𝒖|t=0=𝒖0,\left\{\begin{aligned} &\partial_{t}\boldsymbol{u}+\boldsymbol{u}\cdot\nabla\boldsymbol{u}-\Delta\boldsymbol{u}+\nabla P=\boldsymbol{0},\qquad(t,x)\in\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{+}\times\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{3}\\ &\mathop{\rm div}\nolimits\boldsymbol{u}=0,\\ &\boldsymbol{u}|_{t=0}=\boldsymbol{u}_{0},\end{aligned}\right.

where 𝒖\boldsymbol{u} stands for the velocity field and PP the scalar pressure of the fluid. This system describes the motion of viscous incompressible fluid. And it is worth mentioning that except the case for initial data with some special structure, it is still a big open problem whether or not the system (1.1) has a unique global solution with large initial data.

Now let us write 𝒖\boldsymbol{u} in the cylindrical coordinates as

(1.2) 𝒖(t,x)=ur(t,r,θ,z)𝒆r+uθ(t,r,θ,z)𝒆θ+uz(t,r,θ,z)𝒆z,\boldsymbol{u}(t,x)=u^{r}(t,r,\theta,z)\boldsymbol{e}_{r}+u^{\theta}(t,r,\theta,z)\boldsymbol{e}_{\theta}+u^{z}(t,r,\theta,z)\boldsymbol{e}_{z},

where (r,θ,z)(r,\theta,z) denotes the cylindrical coordinates in 3\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{3} so that x=(rcosθ,rsinθ,z)x=(r\cos\theta,r\sin\theta,z), and

𝒆r=(cosθ,sinθ,0),𝒆θ=(sinθ,cosθ,0),𝒆z=(0,0,1),r=x12+x22.\boldsymbol{e}_{r}=(\cos\theta,\sin\theta,0),\ \boldsymbol{e}_{\theta}=(-\sin\theta,\cos\theta,0),\ \boldsymbol{e}_{z}=(0,0,1),\ r=\sqrt{x_{1}^{2}+x_{2}^{2}}.

Notice that in the cylindrical coordinates, there holds

(1.3) =𝒆rr+1r𝒆θθ+𝒆zz,Δ=r2+rr+θ2r2+z2.\nabla=\boldsymbol{e}_{r}\partial_{r}+\frac{1}{r}\boldsymbol{e}_{\theta}\partial_{\theta}+\boldsymbol{e}_{z}\partial_{z},\quad\Delta=\partial_{r}^{2}+\frac{\partial_{r}}{r}+\frac{\partial_{\theta}^{2}}{r^{2}}+\partial_{z}^{2}.

Then we can reformulate (1.1) in the cylindrical coordinates as

(1.4) {Dtur(r2+z2+rr+θ2r21r2)ur(uθ)2r+2θuθr2+rP=0,Dtuθ(r2+z2+rr+θ2r21r2)uθ+uruθr2θurr2+θPr=0,Dtuz(r2+z2+rr+θ2r2)uz+zP=0,rur+urr+zuz+θuθr=0,(ur,uθ,uz)|t=0=(u0r,u0θ,u0z),\left\{\begin{aligned} &D_{t}u^{r}-\bigl(\partial_{r}^{2}+\partial_{z}^{2}+\frac{\partial_{r}}{r}+\frac{\partial_{\theta}^{2}}{r^{2}}-\frac{1}{r^{2}}\bigr)u^{r}-\frac{(u^{\theta})^{2}}{r}+\frac{2\partial_{\theta}u^{\theta}}{r^{2}}+\partial_{r}P=0,\\ &D_{t}u^{\theta}-\bigl(\partial_{r}^{2}+\partial_{z}^{2}+\frac{\partial_{r}}{r}+\frac{\partial_{\theta}^{2}}{r^{2}}-\frac{1}{r^{2}}\bigr)u^{\theta}+\frac{u^{r}u^{\theta}}{r}-\frac{2\partial_{\theta}u^{r}}{r^{2}}+\frac{\partial_{\theta}P}{r}=0,\\ &D_{t}u^{z}-\bigl(\partial_{r}^{2}+\partial_{z}^{2}+\frac{\partial_{r}}{r}+\frac{\partial_{\theta}^{2}}{r^{2}}\bigr)u^{z}+\partial_{z}P=0,\\ &\partial_{r}u^{r}+\frac{u^{r}}{r}+\partial_{z}u^{z}+\frac{\partial_{\theta}u^{\theta}}{r}=0,\\ &(u^{r},u^{\theta},u^{z})|_{t=0}=(u_{0}^{r},u^{\theta}_{0},u^{z}_{0}),\end{aligned}\right.

where Dt=deft+𝒖=t+(urr+uθθr+uzz)D_{t}\mathrel{\mathop{\kern 0.0pt=}\limits^{\hbox{\footnotesize def}}}\partial_{t}+\boldsymbol{u}\cdot\nabla=\partial_{t}+\bigl(u^{r}\partial_{r}+u^{\theta}\frac{\partial_{\theta}}{r}+u^{z}\partial_{z}\bigr) denotes the material derivative.

For the special case when all the components in (1.2) do not depend on θ\theta, precisely

𝒖(t,x)=ur(t,r,z)𝒆r+uθ(t,r,z)𝒆θ+uz(t,r,z)𝒆z\displaystyle\boldsymbol{u}(t,x)=u^{r}(t,r,z)\boldsymbol{e}_{r}+u^{\theta}(t,r,z)\boldsymbol{e}_{\theta}+u^{z}(t,r,z)\boldsymbol{e}_{z}

then this 𝒖\boldsymbol{u} will be called axisymmetric. It is a celebrated result that for the more special axisymmetric without swirl case, which means uθ=0u^{\theta}=0, Ladyzhenskaya [6] and independently Ukhovskii and Yudovich [11] proved the existence of weak solutions along with the uniqueness and regularities of such solutions. And later Nečas et al. [8] gave a simpler proof. Their proofs deeply rely on the fact that ωθ/r\omega^{\theta}/r satisfies

(1.5) tωθr+(urr+uzz)ωθr(Δ+2rr)ωθr=0,\partial_{t}\frac{\omega^{\theta}}{r}+(u^{r}\partial_{r}+u^{z}\partial_{z})\frac{\omega^{\theta}}{r}-(\Delta+\frac{2}{r}\partial_{r})\frac{\omega^{\theta}}{r}=0,

so that any LpL^{p} norm of ωθ/r\omega^{\theta}/r is conserved.

However, for the arbitrary axisymmetric initial data whose swirl part is non-trivial, we do not have the structure as that in (1.5) any more. To the best of our knowledge, so far we can only establish the global existence of strong solutions when u0θu^{\theta}_{0} is sufficiently small, and this smallness needs to depend on other components of 𝒖0\boldsymbol{u}_{0} or 𝒖0\nabla\boldsymbol{u}_{0}, as the strategy is to view this case as a small perturbation of the no swirl case. There are numerous works concerning this situation, here we only list [1, 2, 3, 4, 7, 9, 12, 13] for example.

Here we do not limit us in considering axisymmetric solutions, but this geometric symmetry still plays a crucial role. Let us also introduce u¯(t,x)=u¯r(t,r,z)er+u¯θ(t,r,z)eθ+u¯z(t,r,z)ez\bar{u}(t,x)=\bar{u}^{r}(t,r,z)e_{r}+\bar{u}^{\theta}(t,r,z)e_{\theta}+\bar{u}^{z}(t,r,z)e_{z} satisfying the following axisymmetric N-S:

(1.6) {tu¯r+(u¯rr+u¯zz)u¯r(r2+z2+1rr1r2)u¯r(u¯θ)2r+rP¯=0,tu¯θ+(u¯rr+u¯zz)u¯θ(r2+z2+1rr1r2)u¯θ+u¯ru¯θr=0,tu¯z+(u¯rr+u¯zz)u¯z(r2+z2+1rr)u¯z+zP¯=0,ru¯r+1ru¯r+zu¯z=0,u¯r|t=0=u¯r0=(u0r),u¯θ|t=0=u¯θ0=(u0θ),u¯z|t=0=u¯z0=(u0z),\left\{\begin{aligned} &\partial_{t}\bar{u}^{r}+(\bar{u}^{r}\partial_{r}+\bar{u}^{z}\partial_{z})\bar{u}^{r}-(\partial_{r}^{2}+\partial_{z}^{2}+\frac{1}{r}\partial_{r}-\frac{1}{r^{2}})\bar{u}^{r}-\frac{(\bar{u}^{\theta})^{2}}{r}+\partial_{r}\bar{P}=0,\\ &\partial_{t}\bar{u}^{\theta}+(\bar{u}^{r}\partial_{r}+\bar{u}^{z}\partial_{z})\bar{u}^{\theta}-(\partial_{r}^{2}+\partial_{z}^{2}+\frac{1}{r}\partial_{r}-\frac{1}{r^{2}})\bar{u}^{\theta}+\frac{\bar{u}^{r}\bar{u}^{\theta}}{r}=0,\\ &\partial_{t}\bar{u}^{z}+(\bar{u}^{r}\partial_{r}+\bar{u}^{z}\partial_{z})\bar{u}^{z}-(\partial_{r}^{2}+\partial_{z}^{2}+\frac{1}{r}\partial_{r})\bar{u}^{z}+\partial_{z}\bar{P}=0,\\ &\partial_{r}\bar{u}^{r}+\frac{1}{r}\bar{u}^{r}+\partial_{z}\bar{u}^{z}=0,\\ &\bar{u}^{r}|_{t=0}=\bar{u}^{r}_{0}={\mathcal{M}}(u_{0}^{r}),\ \bar{u}^{\theta}|_{t=0}=\bar{u}^{\theta}_{0}={\mathcal{M}}(u_{0}^{\theta}),\ \bar{u}^{z}|_{t=0}=\bar{u}^{z}_{0}={\mathcal{M}}(u_{0}^{z}),\end{aligned}\right.

where (f){\mathcal{M}}(f) is the integral average of ff in θ\theta variable, precisely

(1.7) (f)(r,z)=def12π02πf(r,θ,z)𝑑θ.{\mathcal{M}}(f)(r,z)\mathrel{\mathop{\kern 0.0pt=}\limits^{\hbox{\footnotesize def}}}\frac{1}{2\pi}\int_{0}^{2\pi}f(r,\theta,z)\,d\theta.

By definition, there holds (θf)=0{\mathcal{M}}(\partial_{\theta}f)=0 for any smooth function ff. Then one has

div𝒖¯0=ru¯0r+1ru¯0r+zu¯0z=(ru0r+u0rr+zu0z+θu0θr)=(div𝒖0)=0.\mathop{\rm div}\nolimits\bar{\boldsymbol{u}}_{0}=\partial_{r}\bar{u}^{r}_{0}+\frac{1}{r}\bar{u}^{r}_{0}+\partial_{z}\bar{u}^{z}_{0}={\mathcal{M}}(\partial_{r}u^{r}_{0}+\frac{u^{r}_{0}}{r}+\partial_{z}u^{z}_{0}+\frac{\partial_{\theta}u^{\theta}_{0}}{r})={\mathcal{M}}(\mathop{\rm div}\nolimits\boldsymbol{u}_{0})=0.

This guarantees the initial data in (1.6) is indeed compatible with the divergence-free condition.

1.2. Main results.

There are three main results in this paper. The first one concerns the global well-posedness of (1.4) with initial data that are close to some axisymmetric vector fields in some sense. To state this precisely, let us introduce the following norms:

(1.8) fH˙axi12=def~fL22+f/rL22,andfHaxi12=deffL22+fH˙axi12,\|f\|_{\dot{H}^{1}_{\rm axi}}^{2}\mathrel{\mathop{\kern 0.0pt=}\limits^{\hbox{\footnotesize def}}}\|\widetilde{\nabla}f\|_{L^{2}}^{2}+\|f/r\|_{L^{2}}^{2},\quad\hbox{and}\quad\|f\|_{H^{1}_{\rm axi}}^{2}\mathrel{\mathop{\kern 0.0pt=}\limits^{\hbox{\footnotesize def}}}\|f\|_{L^{2}}^{2}+\|f\|_{\dot{H}^{1}_{\rm axi}}^{2},

where ~=def𝒆rr+𝒆zz\widetilde{\nabla}\mathrel{\mathop{\kern 0.0pt=}\limits^{\hbox{\footnotesize def}}}\boldsymbol{e}_{r}\partial_{r}+\boldsymbol{e}_{z}\partial_{z} is a part of the whole gradient given by (1.3).

Theorem 1.1.

Let 𝒖0H2\boldsymbol{u}_{0}\in H^{2} with div𝒖0=0\mathop{\rm div}\nolimits\boldsymbol{u}_{0}=0 and 𝖀0=def(θu0r,θu0θ,θu0z)Haxi1\boldsymbol{\mathfrak{U}}_{0}\mathrel{\mathop{\kern 0.0pt=}\limits^{\hbox{\footnotesize def}}}(\partial_{\theta}u^{r}_{0},\partial_{\theta}u^{\theta}_{0},\partial_{\theta}u^{z}_{0})\in H^{1}_{\rm axi}. If there exists some small positive constant ϵ\epsilon such that the following two smallness conditions hold:

(1.9) u0θL2u0θH˙axi1exp(C𝒖0L26𝒖0H˙22)<ϵ,\|u^{\theta}_{0}\|_{L^{2}}\|u^{\theta}_{0}\|_{\dot{H}^{1}_{\rm axi}}\exp\bigl(C\|{\boldsymbol{u}}_{0}\|_{L^{2}}^{6}\|{\boldsymbol{u}}_{0}\|_{\dot{H}^{2}}^{2}\bigr)<\epsilon,
(1.10) 𝖀0L2𝖀0H˙axi1exp(exp(C𝒖0L26𝒖0H˙22))<ϵ,\|\boldsymbol{\mathfrak{U}}_{0}\|_{L^{2}}\|\boldsymbol{\mathfrak{U}}_{0}\|_{\dot{H}^{1}_{\rm axi}}\exp\bigl(\exp(C\|{\boldsymbol{u}}_{0}\|_{L^{2}}^{6}\|{\boldsymbol{u}}_{0}\|_{\dot{H}^{2}}^{2})\bigr)<\epsilon,

then both (1.4) and (1.6) have unique global strong solutions 𝒖\boldsymbol{u} and 𝒖¯\bar{\boldsymbol{u}} in C(+;H1)L2(+;H˙1H˙2)C(\mathop{\mathbb{R}\kern 0.0pt}\nolimits_{+};H^{1})\cap L^{2}(\mathop{\mathbb{R}\kern 0.0pt}\nolimits_{+};\dot{H}^{1}\cap\dot{H}^{2}) such that for any t>0t>0, there holds

(1.11) 𝒖𝒖¯Lt(L2)2+(𝒖𝒖¯)Lt2(L2)2𝖀0L22exp(exp(C𝒖0L26𝒖0H˙22))=def𝒜,\displaystyle\|\boldsymbol{u}-\bar{\boldsymbol{u}}\|_{L^{\infty}_{t}(L^{2})}^{2}+\|\nabla(\boldsymbol{u}-\bar{\boldsymbol{u}})\|_{L^{2}_{t}(L^{2})}^{2}\lesssim\|\boldsymbol{\mathfrak{U}}_{0}\|_{L^{2}}^{2}\exp\bigl(\exp(C\|{\boldsymbol{u}}_{0}\|_{L^{2}}^{6}\|{\boldsymbol{u}}_{0}\|_{\dot{H}^{2}}^{2})\bigr)\mathrel{\mathop{\kern 0.0pt=}\limits^{\hbox{\footnotesize def}}}{\mathcal{A}},
𝒖𝒖¯Lt(H˙1)2+(𝒖𝒖¯)Lt2(H˙1)2𝖀0H˙axi12exp(exp(C𝒖0L26𝒖0H˙22))=def.\displaystyle\|\boldsymbol{u}-\bar{\boldsymbol{u}}\|_{L^{\infty}_{t}(\dot{H}^{1})}^{2}+\|\nabla(\boldsymbol{u}-\bar{\boldsymbol{u}})\|_{L^{2}_{t}(\dot{H}^{1})}^{2}\lesssim\|\boldsymbol{\mathfrak{U}}_{0}\|_{\dot{H}^{1}_{\rm axi}}^{2}\exp\bigl(\exp(C\|{\boldsymbol{u}}_{0}\|_{L^{2}}^{6}\|{\boldsymbol{u}}_{0}\|_{\dot{H}^{2}}^{2})\bigr)\mathrel{\mathop{\kern 0.0pt=}\limits^{\hbox{\footnotesize def}}}{\mathcal{B}}.

Moreover, for 𝒖=def(ur)𝒆r+(uθ)𝒆θ+(uz)𝒆z{\mathcal{M}}{\boldsymbol{u}}\mathrel{\mathop{\kern 0.0pt=}\limits^{\hbox{\footnotesize def}}}{\mathcal{M}}(u^{r})\boldsymbol{e}_{r}+{\mathcal{M}}(u^{\theta})\boldsymbol{e}_{\theta}+{\mathcal{M}}(u^{z})\boldsymbol{e}_{z}, there holds

(1.12) (𝒖𝒖¯)Lt(L2)2+(𝒖𝒖¯)Lt2(L2)2ϵ𝒜,\displaystyle\|{\mathcal{M}}({\boldsymbol{u}}-\bar{\boldsymbol{u}})\|_{L^{\infty}_{t}(L^{2})}^{2}+\|\nabla{\mathcal{M}}({\boldsymbol{u}}-\bar{\boldsymbol{u}})\|_{L^{2}_{t}(L^{2})}^{2}\lesssim\epsilon{\mathcal{A}},
(𝒖𝒖¯)Lt(H˙1)2+(𝒖𝒖¯)Lt2(H˙1)2ϵ.\displaystyle\|{\mathcal{M}}({\boldsymbol{u}}-\bar{\boldsymbol{u}})\|_{L^{\infty}_{t}(\dot{H}^{1})}^{2}+\|\nabla{\mathcal{M}}({\boldsymbol{u}}-\bar{\boldsymbol{u}})\|_{L^{2}_{t}(\dot{H}^{1})}^{2}\lesssim\epsilon{\mathcal{B}}.
Remark 1.1.

(i) We mention that 𝐮0\boldsymbol{u}_{0} is axisymmetric when 𝖀0\boldsymbol{\mathfrak{U}}_{0} vanishes, and it is well-known that in this situation, the corresponding solution 𝐮\boldsymbol{u} persists axial symmetry for all time.

In view of this, the smallness condition (1.10) actually tells us that 𝐮0\boldsymbol{u}_{0} is close to some axisymmetric vector field. That is what we mean “almost axisymmetric”. Moreover, it is reasonable to expect that this solution 𝐮\boldsymbol{u} keeps close to some axisymmetric vector field for all time.

To verify this feature quantitatively, we mention that one natural way to axisymmetrize a solution 𝐮\boldsymbol{u} to N-S, is to axisymmetrize the initial data, and then solve N-S with this axisymmetrized initial data, in this way we get 𝐮¯\bar{\boldsymbol{u}}. Then in view of the smallness condition (1.10), interpolating between the two estimates in (1.11) gives

𝒖𝒖¯Lt(H˙12)2+(𝒖𝒖¯)Lt2(H˙12)2𝖀0L2𝖀0H˙axi1exp(exp(C𝒖0L26𝒖0H˙22))<ϵ,\|\boldsymbol{u}-\bar{\boldsymbol{u}}\|_{L^{\infty}_{t}(\dot{H}^{\frac{1}{2}})}^{2}+\|\nabla(\boldsymbol{u}-\bar{\boldsymbol{u}})\|_{L^{2}_{t}(\dot{H}^{\frac{1}{2}})}^{2}\lesssim\|\boldsymbol{\mathfrak{U}}_{0}\|_{L^{2}}\|\boldsymbol{\mathfrak{U}}_{0}\|_{\dot{H}^{1}_{\rm axi}}\exp\bigl(\exp(C\|{\boldsymbol{u}}_{0}\|_{L^{2}}^{6}\|{\boldsymbol{u}}_{0}\|_{\dot{H}^{2}}^{2})\bigr)<\epsilon,

which means that 𝐮\boldsymbol{u} is indeed close to the axisymmetric vector field 𝐮¯\bar{\boldsymbol{u}}.

(ii) Furthermore, (1.12) shows that after taking average in θ\theta, 𝐮𝐮¯\boldsymbol{u}-\bar{\boldsymbol{u}} will become much smaller. Hence there must be some cancellations in this process, precisely the positive part of 𝐮𝐮¯\boldsymbol{u}-\bar{\boldsymbol{u}} almost balance its negative part. This provides us more details on how 𝐮\boldsymbol{u} approaches 𝐮¯\bar{\boldsymbol{u}}. One can see this more clearly by expanding 𝐮\boldsymbol{u} into Fourier series in θ\theta variable, see Remark 1.3 below.

With Theorem 1.1 at hand, now let us turn to study the asymptotic expansion of solutions to N-S with almost axisymmetric initial data. As we know, a regular enough function can be expanded into Fourier series in θ\theta variable. And by virtue of the assumptions of Theorem 1.1, here we only consider initial data 𝒖(0,x)\boldsymbol{u}(0,x) in the following special form 11 1 In this part, we use 𝒂0,𝒂k\boldsymbol{a}_{0},\,\boldsymbol{a}_{k} and 𝒃k\boldsymbol{b}_{k} to denote the profiles of the initial data, while the subscript 00 is used to denote the 00-th Fourier coefficients, so that there would be no confusion.:

(1.13) {ur(0,x)=a0r(r,z)+εk=1(akr(r,z)coskθ+bkr(r,z)sinkθ),uθ(0,x)=εa0θ(r,z)+εk=1(akθ(r,z)coskθ+bkθ(r,z)sinkθ),uz(0,x)=a0z(r,z)+εk=1(akz(r,z)coskθ+bkz(r,z)sinkθ),\left\{\begin{aligned} &u^{r}(0,x)=a^{r}_{0}(r,z)+\varepsilon\sum_{k=1}^{\infty}\Bigl(a^{r}_{k}(r,z)\cos k\theta+b^{r}_{k}(r,z)\sin k\theta\Bigr),\\ &u^{\theta}(0,x)=\varepsilon a^{\theta}_{0}(r,z)+\varepsilon\sum_{k=1}^{\infty}\Bigl(a^{\theta}_{k}(r,z)\cos k\theta+b^{\theta}_{k}(r,z)\sin k\theta\Bigr),\\ &u^{z}(0,x)=a^{z}_{0}(r,z)+\varepsilon\sum_{k=1}^{\infty}\Bigl(a^{z}_{k}(r,z)\cos k\theta+b^{z}_{k}(r,z)\sin k\theta\Bigr),\end{aligned}\right.

where ε>0\varepsilon>0 is some small positive constant to be determined later, and the profiles satisfy

(1.14) j=02(i=02jri~j(a0r,a0θ)L22+~ja0zL22+k=1i=02jk2max{i,1}ri~j(𝒂k,𝒃k)L22)<,\begin{split}\sum_{j=0}^{2}\Bigl(\sum_{i=0}^{2-j}\bigl\|r^{-i}\widetilde{\nabla}^{j}(a^{r}_{0},a^{\theta}_{0})\bigr\|_{L^{2}}^{2}+\|\widetilde{\nabla}^{j}a_{0}^{z}\|_{L^{2}}^{2}+\sum_{k=1}^{\infty}\sum_{i=0}^{2-j}k^{2\max\{i,1\}}\bigl\|r^{-i}\widetilde{\nabla}^{j}(\boldsymbol{a}_{k},\boldsymbol{b}_{k})\bigr\|_{L^{2}}^{2}\Bigr)<\infty,\end{split}

and

(1.15) ra0r+a0rr+za0z=0,\partial_{r}a^{r}_{0}+\frac{a^{r}_{0}}{r}+\partial_{z}a^{z}_{0}=0,
(1.16) rark+akrr+zazk+kbkθr=0,rbrk+bkrr+zbzkkakθr=0,k.\partial_{r}a^{r}_{k}+\frac{a^{r}_{k}}{r}+\partial_{z}a^{z}_{k}+\frac{kb^{\theta}_{k}}{r}=0,\quad\partial_{r}b^{r}_{k}+\frac{b^{r}_{k}}{r}+\partial_{z}b^{z}_{k}-\frac{ka^{\theta}_{k}}{r}=0,\quad\forall\ k\in\mathop{\mathbb{N}\kern 0.0pt}\nolimits.

It is not difficult to verify that the constraints (1.15), (1.16) meet the divergence-free condition div𝒖(0)=0\mathop{\rm div}\nolimits\boldsymbol{u}(0)=0. And thanks to Parseval’s identity, (1.14) guarantees that 𝒖(0)H2\boldsymbol{u}(0)\in H^{2} and 𝖀(0)Haxi1\boldsymbol{\mathfrak{U}}(0)\in H^{1}_{\rm axi}. Precisely, we have

𝖀(0)L22ε2k=1k2(𝒂k,𝒃k)L22,𝖀(0)H˙axi12ε2k=1i+j=1k2ri~j(𝒂k,𝒃k)L22,\|\boldsymbol{\mathfrak{U}}(0)\|_{L^{2}}^{2}\sim\varepsilon^{2}\sum_{k=1}^{\infty}k^{2}\bigl\|(\boldsymbol{a}_{k},\boldsymbol{b}_{k})\bigr\|_{L^{2}}^{2},\quad\|\boldsymbol{\mathfrak{U}}(0)\|_{\dot{H}^{1}_{\rm axi}}^{2}\sim\varepsilon^{2}\sum_{k=1}^{\infty}\sum_{i+j=1}k^{2}\bigl\|r^{-i}\widetilde{\nabla}^{j}(\boldsymbol{a}_{k},\boldsymbol{b}_{k})\bigr\|_{L^{2}}^{2},

and the other norms can be derived similarly. In particular, this implies that the smallness conditions in Theorem 1.1 can be satisfied provided ε\varepsilon is sufficiently small, and this smallness needs to rely on the norms of profiles appearing in (1.14).

Then Theorem 1.1 guarantees the existence of a unique global strong solution to N-S with initial data (1.13). As we know, a strong solution to N-S would become analytic for any positive time, thus can be expanded into Fourier series in θ\theta variable in the following form:

(1.17) u(t,x)=j=0εju(j),0(t,r,z)+j=0k=1εj(u(j),k(t,r,z)coskθ+v(j),ksinkθ).\begin{split}u^{\lozenge}(t,x)=\sum_{j=0}^{\infty}\varepsilon^{j}u^{\lozenge}_{(j),0}(t,r,z)+\sum_{j=0}^{\infty}\sum_{k=1}^{\infty}\varepsilon^{j}\Bigl(u^{\lozenge}_{(j),k}(t,r,z)\cos k\theta+v^{\lozenge}_{(j),k}\sin k\theta\Bigr).\end{split}

where \lozenge can be r,θr,\,\theta or zz, and the profiles do not rely on ε\varepsilon.

Unlike the Euclidean coordinates, 𝒆r\boldsymbol{e}_{r} and 𝒆θ\boldsymbol{e}_{\theta} are not constant vectors. As a result, the convergence of 𝒖\boldsymbol{u} in Sobolev spaces is in general not equivalent to the convergence of each component of 𝒖\boldsymbol{u}. In view of this, it is optimal to verify the validity of the expansion (1.17) in L(+;L2L)L^{\infty}(\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{+};L^{2}\cap L^{\infty}) sense. And our first result concerning the asymptotic expansion states as follows:

Theorem 1.2.

Let 𝒖(0,x)\boldsymbol{u}(0,x) be given by (1.13) satisfying (1.14)-(1.16). Then there exists some ε0>0\varepsilon_{0}>0 such that for any ε(0,ε0)\varepsilon\in(0,\varepsilon_{0}), (1.1) has a unique global solution 𝒖C(+;H1)L2(+;H˙1H˙2)\boldsymbol{u}\in C(\mathop{\mathbb{R}\kern 0.0pt}\nolimits_{+};H^{1})\cap L^{2}(\mathop{\mathbb{R}\kern 0.0pt}\nolimits_{+};\dot{H}^{1}\cap\dot{H}^{2}). Moreover, this solution can be expanded as

(1.18) {ur(t,x)=u(0),0r(t,r,z)+εk=1(u(1),kr(t,r,z)coskθ+v(1),kr(t,r,z)sinkθ)+𝒪(ε2),uθ(t,x)=εu(1),0θ(t,r,z)+εk=1(u(1),kθ(t,r,z)coskθ+v(1),kθ(t,r,z)sinkθ)+𝒪(ε2),uz(t,x)=u(0),0z(t,r,z)+εk=1(u(1),kz(t,r,z)coskθ+v(1),kz(t,r,z)sinkθ)+𝒪(ε2)\left\{\begin{aligned} &u^{r}(t,x)=u^{r}_{(0),0}(t,r,z)+\varepsilon\sum_{k=1}^{\infty}\Bigl(u^{r}_{(1),k}(t,r,z)\cos k\theta+v^{r}_{(1),k}(t,r,z)\sin k\theta\Bigr)+{\mathcal{O}}(\varepsilon^{2}),\\ &u^{\theta}(t,x)=\varepsilon u^{\theta}_{(1),0}(t,r,z)+\varepsilon\sum_{k=1}^{\infty}\Bigl(u^{\theta}_{(1),k}(t,r,z)\cos k\theta+v^{\theta}_{(1),k}(t,r,z)\sin k\theta\Bigr)+{\mathcal{O}}(\varepsilon^{2}),\\ &u^{z}(t,x)=u^{z}_{(0),0}(t,r,z)+\varepsilon\sum_{k=1}^{\infty}\Bigl(u^{z}_{(1),k}(t,r,z)\cos k\theta+v^{z}_{(1),k}(t,r,z)\sin k\theta\Bigr)+{\mathcal{O}}(\varepsilon^{2})\end{aligned}\right.

in L(+;L2L)L^{\infty}(\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{+};L^{2}\cap L^{\infty}) sense.

Remark 1.2.

We can see that up to ε\varepsilon order, this expansion (1.18) has the same form as the initial state (1.13). In particular, the coefficients u(1),0ru^{r}_{(1),0} and u(1),0zu^{z}_{(1),0} vanish for all time.

The following result concerns the odevity in this asymptotic expansion. We mention that this persistence of odevity deeply reflects some nonlinear structures of N-S.

Theorem 1.3.

Under the assumptions of Theorem 1.2, let us consider the special case of (1.13) that ur(0,x)u^{r}(0,x) and uz(0,x)u^{z}(0,x) are even in θ\theta, while uθ(0,x)u^{\theta}(0,x) is odd in θ\theta, precisely:

(1.19) {ur(0,x)=a0r(r,z)+εk=1akr(r,z)coskθ,uθ(0,x)=εk=1bkθ(r,z)sinkθ,uz(0,x)=a0z(r,z)+εk=1akz(r,z)coskθ.\left\{\begin{aligned} &u^{r}(0,x)=a^{r}_{0}(r,z)+\varepsilon\sum_{k=1}^{\infty}a^{r}_{k}(r,z)\cos k\theta,\\ &u^{\theta}(0,x)=\varepsilon\sum_{k=1}^{\infty}b^{\theta}_{k}(r,z)\sin k\theta,\\ &u^{z}(0,x)=a^{z}_{0}(r,z)+\varepsilon\sum_{k=1}^{\infty}a^{z}_{k}(r,z)\cos k\theta.\end{aligned}\right.

Then this odevity will persist for all time. Precisely, the following expansion

(1.20) {ur(t,x)=(u(0),0r+j=2εju(j),0r)(t,r,z)+j=1k=1εju(j),kr(t,r,z)coskθ,uθ(t,x)=j=1k=1εjv(j),kθ(t,r,z)sinkθ,uz(t,x)=(u(0),0z+j=2εju(j),0z)(t,r,z)+j=1k=1εju(j),kz(t,r,z)coskθ\left\{\begin{aligned} u^{r}(t,x)=&\Bigl(u^{r}_{(0),0}+\sum_{j=2}^{\infty}\varepsilon^{j}u^{r}_{(j),0}\Bigr)(t,r,z)+\sum_{j=1}^{\infty}\sum_{k=1}^{\infty}\varepsilon^{j}u^{r}_{(j),k}(t,r,z)\cos k\theta,\\ u^{\theta}(t,x)=&\sum_{j=1}^{\infty}\sum_{k=1}^{\infty}\varepsilon^{j}v^{\theta}_{(j),k}(t,r,z)\sin k\theta,\\ u^{z}(t,x)=&\Bigl(u^{z}_{(0),0}+\sum_{j=2}^{\infty}\varepsilon^{j}u^{z}_{(j),0}\Bigr)(t,r,z)+\sum_{j=1}^{\infty}\sum_{k=1}^{\infty}\varepsilon^{j}u^{z}_{(j),k}(t,r,z)\cos k\theta\end{aligned}\right.

holds in L(+;L2L)L^{\infty}(\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{+};L^{2}\cap L^{\infty}) sense.

Remark 1.3.

One can see from the proof in Section 5 that, u(0),0r𝐞r+u(0),0z𝐞zu^{r}_{(0),0}\boldsymbol{e}_{r}+u^{z}_{(0),0}\boldsymbol{e}_{z} here actually satisfies axisymmetric N-S with initial data a0r𝐞r+a0z𝐞z=(𝐮(0,x))a_{0}^{r}\boldsymbol{e}_{r}+a_{0}^{z}\boldsymbol{e}_{z}={\mathcal{M}}(\boldsymbol{u}(0,x)). Thus u(0),0r𝐞r+u(0),0z𝐞zu^{r}_{(0),0}\boldsymbol{e}_{r}+u^{z}_{(0),0}\boldsymbol{e}_{z} corresponds to the 𝐮¯\bar{\boldsymbol{u}} in Theorem 1.1, and we can obtain from the expression (1.20) that

𝒖𝒖¯=j=2εj𝒖(j),0+j=1k=1εj(𝒖(j),kcoskθ+𝒗(j),ksinkθ)=𝒪(ε),\boldsymbol{u}-\bar{\boldsymbol{u}}=\sum_{j=2}^{\infty}\varepsilon^{j}\boldsymbol{u}_{(j),0}+\sum_{j=1}^{\infty}\sum_{k=1}^{\infty}\varepsilon^{j}\Bigl(\boldsymbol{u}_{(j),k}\cos k\theta+\boldsymbol{v}_{(j),k}\sin k\theta\Bigr)={\mathcal{O}}(\varepsilon),

and

(𝒖𝒖¯)=j=2εj𝒖(j),0=𝒪(ε2),{\mathcal{M}}(\boldsymbol{u}-\bar{\boldsymbol{u}})=\sum_{j=2}^{\infty}\varepsilon^{j}\boldsymbol{u}_{(j),0}={\mathcal{O}}(\varepsilon^{2}),

which indicates that (𝐮𝐮¯){\mathcal{M}}(\boldsymbol{u}-\bar{\boldsymbol{u}}) is in general much smaller than 𝐮𝐮¯\boldsymbol{u}-\bar{\boldsymbol{u}}, just as what we have mentioned at the end of Remark 1.1. Here we can see that the reason is the cancellations of the oscillating terms, which is the main terms in 𝐮𝐮¯\boldsymbol{u}-\bar{\boldsymbol{u}}.

Roughly speaking, here we have (𝐮𝐮¯)|𝐮𝐮¯|2.{\mathcal{M}}(\boldsymbol{u}-\bar{\boldsymbol{u}})\sim|\boldsymbol{u}-\bar{\boldsymbol{u}}|^{2}. To see this more clearly, we refer the readers to Section 5 to find the derivations of the profiles in (1.20).

Let us end this section with some notations which will be used throughout this paper.

Notations. We shall use CC to denote an universal constant which may change from line to line. The notation aba\lesssim b means aCba\leq Cb, and fgf\sim g means both aba\lesssim b and bab\lesssim a hold. For a Banach space B, we shall use the shorthand LTp(B)L^{p}_{T}(B) for BLp(0,T,dt)\bigl\|\|\cdot\|_{B}\bigr\|_{L^{p}(0,T;dt)}. We use HsH^{s} (resp. H˙s\dot{H}^{s}) to denote inhomogeneous (resp. homogeneous) L2L^{2} based Sobolev spaces.

2. Preliminary

2.1. Poincaré-type inequality

Lemma 2.1.

For any p[1,]p\in[1,\infty] and fLpf\in L^{p}, the operator {\mathcal{M}} defined in (1.7) satisfies

(2.1) (f)LpfLp,andf(f)Lp2πθfLp.\|{\mathcal{M}}(f)\|_{L^{p}}\leq\|f\|_{L^{p}},\quad\hbox{and}\quad\|f-{\mathcal{M}}(f)\|_{L^{p}}\leq 2\pi\|\partial_{\theta}f\|_{L^{p}}.
Proof.

Let us first consider the case when p[1,)p\in[1,\infty). By applying Hölder’s inequality, we get

(f)Lpp\displaystyle\|{\mathcal{M}}(f)\|_{L^{p}}^{p} =2π+×|12π02πf(r,θ,z)dθ|prdrdz\displaystyle=2\pi\int_{\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{+}\times\mathop{\mathbb{R}\kern 0.0pt}\nolimits}\Bigl|\frac{1}{2\pi}\int_{0}^{2\pi}f(r,\theta,z)\,d\theta\Bigr|^{p}\,rdrdz
+×(02π|f(r,θ,z)|pdθ)rdrdz=fLpp.\displaystyle\leq\int_{\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{+}\times\mathop{\mathbb{R}\kern 0.0pt}\nolimits}\bigl(\int_{0}^{2\pi}|f(r,\theta,z)|^{p}\,d\theta\bigr)\,rdrdz=\|f\|_{L^{p}}^{p}.

To prove the second inequality of (2.1), we first write

|f(r,θ,z)(f)(r,z)|p\displaystyle|f(r,\theta,z)-{\mathcal{M}}(f)(r,z)|^{p} =|12π02π(f(r,θ,z)f(r,θ,z))dθ|p\displaystyle=\Bigl|\frac{1}{2\pi}\int_{0}^{2\pi}\bigl(f(r,\theta,z)-f(r,\theta^{\prime},z)\bigr)\,d\theta^{\prime}\Bigr|^{p}
=|12π02π(θθ(θf)(r,θ′′,z)dθ′′)dθ|p\displaystyle=\Bigl|\frac{1}{2\pi}\int_{0}^{2\pi}\bigl(\int_{\theta^{\prime}}^{\theta}(\partial_{\theta}f)(r,\theta^{\prime\prime},z)\,d\theta^{\prime\prime}\bigr)\,d\theta^{\prime}\Bigr|^{p}
12π02π|θθ|(θf)(r,θ′′,z)|pdθ′′||θθ|p1dθ\displaystyle\leq\frac{1}{2\pi}\int_{0}^{2\pi}\Bigl|\int_{\theta^{\prime}}^{\theta}\bigl|(\partial_{\theta}f)(r,\theta^{\prime\prime},z)\bigr|^{p}\,d\theta^{\prime\prime}\Bigr||\theta-\theta^{\prime}|^{p-1}\,d\theta^{\prime}
12π02π|(θf)(r,θ′′,z)|pdθ′′02π|θθ|p1dθ.\displaystyle\leq\frac{1}{2\pi}\int_{0}^{2\pi}\bigl|(\partial_{\theta}f)(r,\theta^{\prime\prime},z)\bigr|^{p}\,d\theta^{\prime\prime}\int_{0}^{2\pi}|\theta-\theta^{\prime}|^{p-1}\,d\theta^{\prime}.

As a result, we can obtain

f(r,θ,z)(f)(r,z)Lpp\displaystyle\|f(r,\theta,z)-{\mathcal{M}}(f)(r,z)\|_{L^{p}}^{p} =12π+×(02π|(θf)(r,θ′′,z)|pdθ′′)rdrdz\displaystyle=\frac{1}{2\pi}\int_{\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{+}\times\mathop{\mathbb{R}\kern 0.0pt}\nolimits}\Bigl(\int_{0}^{2\pi}\bigl|(\partial_{\theta}f)(r,\theta^{\prime\prime},z)\bigr|^{p}\,d\theta^{\prime\prime}\Bigr)\,rdrdz
×02π02π|θθ|p1dθ𝑑θ\displaystyle\qquad\qquad\qquad\qquad\times\int_{0}^{2\pi}\int_{0}^{2\pi}|\theta-\theta^{\prime}|^{p-1}\,d\theta^{\prime}d\theta
=2p+1(2π)pθfLpp(2π)pθfLpp.\displaystyle=\frac{2}{p+1}(2\pi)^{p}\|\partial_{\theta}f\|_{L^{p}}^{p}\leq(2\pi)^{p}\|\partial_{\theta}f\|_{L^{p}}^{p}.

Clearly this gives the second inequality of (2.1) for p[1,)p\in[1,\infty).

As for the case when p=p=\infty, we have the following formulas:

|(f)(x)|=|12π02πf(r,θ,z)𝑑θ|fL,|{\mathcal{M}}(f)(x)|=\Bigl|\frac{1}{2\pi}\int_{0}^{2\pi}f(r,\theta,z)\,d\theta\Bigr|\leq\|f\|_{L^{\infty}},

and

|f(x)(f)(x)|=|12π02π(θθ(θf)(r,θ′′,z)dθ′′)dθ|2πθfL,|f(x)-{\mathcal{M}}(f)(x)|=\Bigl|\frac{1}{2\pi}\int_{0}^{2\pi}\bigl(\int_{\theta^{\prime}}^{\theta}(\partial_{\theta}f)(r,\theta^{\prime\prime},z)\,d\theta^{\prime\prime}\bigr)\,d\theta^{\prime}\Bigr|\leq 2\pi\|\partial_{\theta}f\|_{L^{\infty}},

which hold for any x3x\in\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{3}. This completes the proof of this lemma. ∎

2.2. Properties for axisymmetric functions.

Let us first recall the well-known Biot-Savart law, which asserts that any divergence-free velocity field 𝒖\boldsymbol{u} can be uniquely determined by its vorticity curl𝒖\mathop{\rm curl}\nolimits\boldsymbol{u}. Moreover, for any s>0s>0 and any 1<p<1<p<\infty, there holds

(2.2) 𝒖H˙scurl𝒖H˙s,𝒖Lpcurl𝒖Lp.\|\nabla\boldsymbol{u}\|_{\dot{H}^{s}}\sim\|\mathop{\rm curl}\nolimits\boldsymbol{u}\|_{\dot{H}^{s}},\quad\|\nabla\boldsymbol{u}\|_{L^{p}}\sim\|\mathop{\rm curl}\nolimits\boldsymbol{u}\|_{L^{p}}.

For the special case when the velocity field is axisymmetric without swirl, namely

𝒖~(x)=u~r(r,z)𝒆r+u~z(r,z)𝒆z,\widetilde{\boldsymbol{u}}(x)=\widetilde{u}^{r}(r,z)\boldsymbol{e}_{r}+\widetilde{u}^{z}(r,z)\boldsymbol{e}_{z},

then we can use ω~θ=zu~rru~z\widetilde{\omega}^{\theta}=\partial_{z}\widetilde{u}^{r}-\partial_{r}\widetilde{u}^{z} to represent 𝒖~\widetilde{\boldsymbol{u}}. Moreover, there holds:

Lemma 2.2.

If in addition 𝒖~H2\widetilde{\boldsymbol{u}}\in H^{2}, then we have the following estimates:

(2.3) 𝒖~L2~u~rL2+~u~zL2+u~rrL2ω~θL2,\|\nabla\widetilde{\boldsymbol{u}}\|_{L^{2}}\sim\|\widetilde{\nabla}\widetilde{u}^{r}\|_{L^{2}}+\|\widetilde{\nabla}\widetilde{u}^{z}\|_{L^{2}}+\bigl\|\frac{\widetilde{u}^{r}}{r}\bigr\|_{L^{2}}\sim\|{\widetilde{\omega}}^{\theta}\|_{L^{2}},
(2.4) 2𝒖~L22~ω~θL22+ω~θrL22.\|\nabla^{2}\widetilde{\boldsymbol{u}}\|_{L^{2}}^{2}\sim\|\widetilde{\nabla}\widetilde{\omega}^{\theta}\|_{L^{2}}^{2}+\bigl\|\frac{\widetilde{\omega}^{\theta}}{r}\bigr\|_{L^{2}}^{2}.
Proof.

Notice that u~r,u~z\widetilde{u}^{r},\,\widetilde{u}^{z} and 𝒆z\boldsymbol{e}_{z} are independent of θ\theta, we have the point-wise estimate

|r1u~r(x)|=|r1θ(u~r(r,z)𝒆r+u~z(r,z)𝒆z)||𝒖~(x)|,x3.\bigl|r^{-1}\widetilde{u}^{r}(x)\bigr|=\bigl|r^{-1}{\partial_{\theta}}\bigl(\widetilde{u}^{r}(r,z)\boldsymbol{e}_{r}+\widetilde{u}^{z}(r,z)\boldsymbol{e}_{z}\bigr)\bigr|\leq|\nabla\widetilde{\boldsymbol{u}}(x)|,\quad\forall\ x\in\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{3}.

which along with (2.2) implies the first desired estimate (2.3).

On the other hand, since div𝒖~=0\mathop{\rm div}\nolimits\widetilde{\boldsymbol{u}}=0, θ𝒆r=𝒆θ\partial_{\theta}\boldsymbol{e}_{r}=\boldsymbol{e}_{\theta} and θ𝒆θ=𝒆r\partial_{\theta}\boldsymbol{e}_{\theta}=-\boldsymbol{e}_{r}, one has

Δ𝒖~=curlcurlu~=curl(ω~θ𝒆θ)=zω~θ𝒆r+(rω~θ+ω~θr)𝒆z,\displaystyle\begin{aligned} &-\Delta\widetilde{\boldsymbol{u}}=\mathop{\rm curl}\nolimits\mathop{\rm curl}\nolimits\widetilde{u}=\mathop{\rm curl}\nolimits(\widetilde{\omega}^{\theta}\boldsymbol{e}_{\theta})=-\partial_{z}\widetilde{\omega}^{\theta}\boldsymbol{e}_{r}+(\partial_{r}\widetilde{\omega}^{\theta}+\frac{\widetilde{\omega}^{\theta}}{r})\boldsymbol{e}_{z},\end{aligned}

which implies

(2.5) 2𝒖~L22\displaystyle\|\nabla^{2}\widetilde{\boldsymbol{u}}\|_{L^{2}}^{2} rω~θ+ω~θrL22+zω~θL22\displaystyle\sim\bigl\|\partial_{r}\widetilde{\omega}^{\theta}+\frac{\widetilde{\omega}^{\theta}}{r}\bigr\|_{L^{2}}^{2}+\|\partial_{z}\widetilde{\omega}^{\theta}\|_{L^{2}}^{2}
=~ω~θL22+ω~θrL22+23rω~θω~θrdx.\displaystyle=\|\widetilde{\nabla}\widetilde{\omega}^{\theta}\|_{L^{2}}^{2}+\bigl\|\frac{\widetilde{\omega}^{\theta}}{r}\bigr\|_{L^{2}}^{2}+2\int_{\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{3}}\partial_{r}\widetilde{\omega}^{\theta}\cdot\frac{\widetilde{\omega}^{\theta}}{r}\,dx.

While the condition 𝒖~H2\widetilde{\boldsymbol{u}}\in H^{2} implies ω~θL2\widetilde{\omega}^{\theta}\in L^{2} and r1ω~θL2r^{-1}\widetilde{\omega}^{\theta}\in L^{2}, and thus limr0ω~θ=limrω~θ=0.\lim_{r\rightarrow 0}\widetilde{\omega}^{\theta}=\lim_{r\rightarrow\infty}\widetilde{\omega}^{\theta}=0. As a result, there holds

23rω~θω~θrdx=2π+×r|ω~θ|2drdz=2π|ω~θ|2|r=0dz=0,\displaystyle 2\int_{\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{3}}\partial_{r}\widetilde{\omega}^{\theta}\cdot\frac{\widetilde{\omega}^{\theta}}{r}\,dx=2\pi\int_{\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{+}\times\mathop{\mathbb{R}\kern 0.0pt}\nolimits}\partial_{r}|\widetilde{\omega}^{\theta}|^{2}\,drdz=2\pi\int_{\mathop{\mathbb{R}\kern 0.0pt}\nolimits}|\widetilde{\omega}^{\theta}|^{2}\big|_{r=0}^{\infty}\,dz=0,

which along with (2.5) gives the second desired estimate (2.4). It completes the proof of the lemma. ∎

Lemma 2.3.

Let 𝒖¯(x)=u¯r(r,z)𝒆r+u¯θ(r,z)𝒆θ+u¯z(r,z)𝒆zH1\bar{\boldsymbol{u}}(x)=\bar{u}^{r}(r,z)\boldsymbol{e}_{r}+\bar{u}^{\theta}(r,z)\boldsymbol{e}_{\theta}+\bar{u}^{z}(r,z)\boldsymbol{e}_{z}\in H^{1} be divergence-free, and the corresponding vorticity ω¯θ=zu¯rru¯z\bar{\omega}^{\theta}=\partial_{z}\bar{u}^{r}-\partial_{r}\bar{u}^{z}. Then we have

(2.6) 𝒖¯L22\displaystyle\|\nabla\bar{\boldsymbol{u}}\|_{L^{2}}^{2} ω¯θL22+~u¯θL22+u¯θrL22\displaystyle\sim\|\bar{\omega}^{\theta}\|_{L^{2}}^{2}+\|\widetilde{\nabla}\bar{u}^{\theta}\|_{L^{2}}^{2}+\bigl\|\frac{\bar{u}^{\theta}}{r}\bigr\|_{L^{2}}^{2}
~u¯rL22+~u¯zL22+~u¯θL22+u¯rrL22+u¯θrL22,\displaystyle\sim\|\widetilde{\nabla}\bar{u}^{r}\|_{L^{2}}^{2}+\|\widetilde{\nabla}\bar{u}^{z}\|_{L^{2}}^{2}+\|\widetilde{\nabla}\bar{u}^{\theta}\|_{L^{2}}^{2}+\bigl\|\frac{\bar{u}^{r}}{r}\bigr\|_{L^{2}}^{2}+\bigl\|\frac{\bar{u}^{\theta}}{r}\bigr\|_{L^{2}}^{2},
Proof.

Notice that curl𝒖¯=(zu¯θ)𝒆r+(zu¯rru¯z)𝒆θ+(ru¯θ+u¯θr)𝒆z\mathop{\rm curl}\nolimits\bar{\boldsymbol{u}}=(-\partial_{z}\bar{u}^{\theta})\boldsymbol{e}_{r}+(\partial_{z}\bar{u}^{r}-\partial_{r}\bar{u}^{z})\boldsymbol{e}_{\theta}+(\partial_{r}\bar{u}^{\theta}+\frac{\bar{u}^{\theta}}{r})\boldsymbol{e}_{z}, we have

(2.7) 𝒖¯L22curl𝒖¯L22\displaystyle\|\nabla\bar{\boldsymbol{u}}\|_{L^{2}}^{2}\thicksim\|\mathop{\rm curl}\nolimits\bar{\boldsymbol{u}}\|_{L^{2}}^{2} =ω¯θL22+ru¯θ+u¯θrL22+zu¯θL22\displaystyle=\|\bar{\omega}^{\theta}\|_{L^{2}}^{2}+\bigl\|\partial_{r}\bar{u}^{\theta}+\frac{\bar{u}^{\theta}}{r}\bigr\|_{L^{2}}^{2}+\|\partial_{z}\bar{u}^{\theta}\|_{L^{2}}^{2}
~u¯rL22+~u¯zL22+u¯rrL22+ru¯θ+u¯θrL22+zu¯θL22,\displaystyle\sim\|\widetilde{\nabla}\bar{u}^{r}\|_{L^{2}}^{2}+\|\widetilde{\nabla}\bar{u}^{z}\|_{L^{2}}^{2}+\bigl\|\frac{\bar{u}^{r}}{r}\bigr\|_{L^{2}}^{2}+\bigl\|\partial_{r}\bar{u}^{\theta}+\frac{\bar{u}^{\theta}}{r}\bigr\|_{L^{2}}^{2}+\|\partial_{z}\bar{u}^{\theta}\|_{L^{2}}^{2},

where we have used Lemma 2.2 in the last step. On the other hand, since 𝒖¯H1\bar{\boldsymbol{u}}\in H^{1}, we have u¯θL2\bar{u}^{\theta}\in L^{2} and r1u¯θL2r^{-1}\bar{u}^{\theta}\in L^{2}, and thus limr0u¯θ=limru¯θ=0\lim_{r\rightarrow 0}\bar{u}^{\theta}=\lim_{r\rightarrow\infty}\bar{u}^{\theta}=0, which implies

23ru¯θu¯θrdx=2π+×0r|u¯θ|2drdz=2π|u¯θ|2|r=0dz=0.\displaystyle 2\int_{\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{3}}\partial_{r}\bar{u}^{\theta}\cdot\frac{\bar{u}^{\theta}}{r}\,dx=2\pi\int_{\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{+}\times\mathop{\mathbb{R}\kern 0.0pt}\nolimits}\int_{0}^{\infty}\partial_{r}|\bar{u}^{\theta}|^{2}\,drdz=2\pi\int_{\mathop{\mathbb{R}\kern 0.0pt}\nolimits}|\bar{u}^{\theta}|^{2}\big|_{r=0}^{\infty}\,dz=0.

As a result, there holds

ru¯θ+u¯θrL22=ru¯θL22+u¯θrL22+23ru¯θu¯θrdx=ru¯θL22+u¯θrL22.\displaystyle\begin{aligned} &\bigl\|\partial_{r}\bar{u}^{\theta}+\frac{\bar{u}^{\theta}}{r}\bigr\|_{L^{2}}^{2}=\|\partial_{r}\bar{u}^{\theta}\|_{L^{2}}^{2}+\bigl\|\frac{\bar{u}^{\theta}}{r}\bigr\|_{L^{2}}^{2}+2\int_{\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{3}}\partial_{r}\bar{u}^{\theta}\cdot\frac{\bar{u}^{\theta}}{r}\,dx=\|\partial_{r}\bar{u}^{\theta}\|_{L^{2}}^{2}+\bigl\|\frac{\bar{u}^{\theta}}{r}\bigr\|_{L^{2}}^{2}.\end{aligned}

Substituting this into (2.7) gives the desired estimate (2.6). The lemma is proved. ∎

2.3. A stability result for N-S

In this subsection, we shall give a stability result for N-S. There are numerous works concerning this problem, here we only list two classical results [5, 10].

Proposition 2.1.

Let 𝒗\boldsymbol{v} be a global strong solution to N-S with initial data 𝒗0H1\boldsymbol{v}_{0}\in H^{1}, and there exists some positive constants AA and BB such that

(2.8) 𝒗L(+;L2)+𝒗L2(+;L2)A,and𝒗L(+;H˙1)+𝒗L2(+;H˙1)B.\|\boldsymbol{v}\|_{L^{\infty}(\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{+};L^{2})}+\|\nabla\boldsymbol{v}\|_{L^{2}(\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{+};L^{2})}\leq A,\quad\hbox{and}\quad\|\boldsymbol{v}\|_{L^{\infty}(\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{+};\dot{H}^{1})}+\|\nabla\boldsymbol{v}\|_{L^{2}(\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{+};\dot{H}^{1})}\leq B.

Then there exists some small positive constant c0c_{0} such that whenever 𝒖0H1\boldsymbol{u}_{0}\in H^{1} satisfies

(2.9) 𝒖0𝒗0L2𝒖0𝒗0H˙1exp(CA2B2)<c0,\|\boldsymbol{u}_{0}-\boldsymbol{v}_{0}\|_{L^{2}}\|\boldsymbol{u}_{0}-\boldsymbol{v}_{0}\|_{\dot{H}^{1}}\exp\bigl(CA^{2}B^{2}\bigr)<c_{0},

then N-S with 𝒖0\boldsymbol{u}_{0} as initial data also has a global strong solution 𝒖\boldsymbol{u}. Moreover, this solution satisfies for s=0,1s=0,1 that

(2.10) 𝒖𝒗L(+;H˙s)2+(𝒖𝒗)L2(+;H˙s)2C𝒖0𝒗0H˙s2exp(CA2B2),\|\boldsymbol{u}-\boldsymbol{v}\|_{L^{\infty}(\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{+};\dot{H}^{s})}^{2}+\|\nabla(\boldsymbol{u}-\boldsymbol{v})\|_{L^{2}(\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{+};\dot{H}^{s})}^{2}\leq C\|\boldsymbol{u}_{0}-\boldsymbol{v}_{0}\|_{\dot{H}^{s}}^{2}\exp\bigl(CA^{2}B^{2}\bigr),

and

(2.11) 𝒖𝒗L(+;L)𝒖0𝒗0H2exp(CA2B2+CB4).\|\boldsymbol{u}-\boldsymbol{v}\|_{L^{\infty}(\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{+};L^{\infty})}\leq\|\boldsymbol{u}_{0}-\boldsymbol{v}_{0}\|_{H^{2}}\exp\bigl(CA^{2}B^{2}+CB^{4}\bigr).
Proof.

Step 1. The proof of (2.10). Let us denote 𝒉=def𝒖𝒗\boldsymbol{h}\mathrel{\mathop{\kern 0.0pt=}\limits^{\hbox{\footnotesize def}}}\boldsymbol{u}-\boldsymbol{v}, then we can find

(2.12) {t𝒉+𝒖𝒉+𝒉𝒗Δ𝒉+Π=0,div𝒉=0,𝒉|t=0=𝒖0𝒗0,\left\{\begin{aligned} &\partial_{t}\boldsymbol{h}+\boldsymbol{u}\cdot\nabla\boldsymbol{h}+\boldsymbol{h}\cdot\nabla\boldsymbol{v}-\Delta\boldsymbol{h}+\nabla\Pi=0,\quad\mathop{\rm div}\nolimits\boldsymbol{h}=0,\\ &\boldsymbol{h}|_{t=0}=\boldsymbol{u}_{0}-\boldsymbol{v}_{0},\end{aligned}\right.

for some properly chosen Π\Pi. By taking L2L^{2} inner product of (2.12) with 𝒉\boldsymbol{h}, we obtain

12ddt𝒉L22+𝒉L22\displaystyle\frac{1}{2}\frac{d}{dt}\|\boldsymbol{h}\|_{L^{2}}^{2}+\|\nabla\boldsymbol{h}\|_{L^{2}}^{2} =3(𝒉𝒗)𝒉dx\displaystyle=-\int_{\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{3}}(\boldsymbol{h}\cdot\nabla\boldsymbol{v})\cdot\boldsymbol{h}\,dx
𝒉L42𝒗L2\displaystyle\leq\|\boldsymbol{h}\|_{L^{4}}^{2}\|\nabla\boldsymbol{v}\|_{L^{2}}
12𝒉L22+C𝒉L22𝒗L24.\displaystyle\leq\frac{1}{2}\|\nabla\boldsymbol{h}\|_{L^{2}}^{2}+C\|\boldsymbol{h}\|_{L^{2}}^{2}\|\nabla\boldsymbol{v}\|_{L^{2}}^{4}.

After subtracting 12𝒉L22\frac{1}{2}\|\nabla\boldsymbol{h}\|_{L^{2}}^{2} on both sides, then applying Gronwall’s inequality leads to

(2.13) 𝒉Lt(L2)2+𝒉Lt2(L2)2𝒖0𝒗0L22exp(C𝒗Lt2(L2)2𝒗Lt(H˙1)2)𝒖0𝒗0L22exp(CA2B2).\begin{split}\|\boldsymbol{h}\|_{L^{\infty}_{t}(L^{2})}^{2}+\|\nabla\boldsymbol{h}\|_{L^{2}_{t}(L^{2})}^{2}&\leq\|\boldsymbol{u}_{0}-\boldsymbol{v}_{0}\|_{L^{2}}^{2}\exp\bigl(C\|\nabla\boldsymbol{v}\|_{L^{2}_{t}(L^{2})}^{2}\|\boldsymbol{v}\|_{L^{\infty}_{t}(\dot{H}^{1})}^{2}\bigr)\\ &\leq\|\boldsymbol{u}_{0}-\boldsymbol{v}_{0}\|_{L^{2}}^{2}\exp\bigl(CA^{2}B^{2}\bigr).\end{split}

While by taking L2L^{2} inner product of (2.12) with Δ𝒉-\Delta\boldsymbol{h}, we have

12ddt𝒉L22+Δ𝒉L22=(𝒖𝒉|Δ𝒉)+(𝒉𝒗|Δ𝒉)=j=13(j(𝒗+𝒉)𝒉|j𝒉)+(𝒉𝒗|Δ𝒉)𝒉L232𝒉L632+𝒗L2(𝒉L42+𝒉LΔ𝒉L2)𝒉L212𝒉L212Δ𝒉L22+𝒗L2𝒉L212Δ𝒉L232.\displaystyle\begin{aligned} \frac{1}{2}\frac{d}{dt}\|\nabla\boldsymbol{h}\|_{L^{2}}^{2}+\|\Delta\boldsymbol{h}\|_{L^{2}}^{2}&=(\boldsymbol{u}\cdot\nabla\boldsymbol{h}\,|\,\Delta\boldsymbol{h})+(\boldsymbol{h}\cdot\nabla\boldsymbol{v}\,|\,\Delta\boldsymbol{h})\\ &=-\sum_{j=1}^{3}(\partial_{j}(\boldsymbol{v}+\boldsymbol{h})\cdot\nabla\boldsymbol{h}\,|\,\partial_{j}\boldsymbol{h})+(\boldsymbol{h}\cdot\nabla\boldsymbol{v}\,|\,\Delta\boldsymbol{h})\\ &\lesssim\|\nabla\boldsymbol{h}\|_{L^{2}}^{\frac{3}{2}}\|\nabla\boldsymbol{h}\|_{L^{6}}^{\frac{3}{2}}+\|\nabla\boldsymbol{v}\|_{L^{2}}\bigl(\|\nabla\boldsymbol{h}\|_{L^{4}}^{2}+\|\boldsymbol{h}\|_{L^{\infty}}\|\Delta\boldsymbol{h}\|_{L^{2}}\bigr)\\ &\lesssim\|\boldsymbol{h}\|_{L^{2}}^{\frac{1}{2}}\|\nabla\boldsymbol{h}\|_{L^{2}}^{\frac{1}{2}}\|\Delta\boldsymbol{h}\|_{L^{2}}^{2}+\|\nabla\boldsymbol{v}\|_{L^{2}}\|\nabla\boldsymbol{h}\|_{L^{2}}^{\frac{1}{2}}\|\Delta\boldsymbol{h}\|_{L^{2}}^{\frac{3}{2}}.\end{aligned}

Then by using Young’s inequality to the last term, we get

(2.14) ddt𝒉L22+32Δ𝒉L22C𝒉L212𝒉L212Δ𝒉L22+C𝒗L24𝒉L22.\begin{split}\frac{d}{dt}\|\nabla\boldsymbol{h}\|_{L^{2}}^{2}+\frac{3}{2}\|\Delta\boldsymbol{h}\|_{L^{2}}^{2}\leq C\|\boldsymbol{h}\|_{L^{2}}^{\frac{1}{2}}\|\nabla\boldsymbol{h}\|_{L^{2}}^{\frac{1}{2}}\|\Delta\boldsymbol{h}\|_{L^{2}}^{2}+C\|\nabla\boldsymbol{v}\|_{L^{2}}^{4}\|\nabla\boldsymbol{h}\|_{L^{2}}^{2}.\end{split}

On the other hand, by the local well-posedness result, the following set is not empty:

𝒟=def{T+: there holds 𝒉LT(L2)2+Δ𝒉LT2(L2)22(𝒖0𝒗0)L22exp(CA2B2)}.{\mathcal{D}}\mathrel{\mathop{\kern 0.0pt=}\limits^{\hbox{\footnotesize def}}}\bigl\{\,T\in\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{+}:\mbox{ there holds }\|\nabla\boldsymbol{h}\|_{L^{\infty}_{T}(L^{2})}^{2}+\|\Delta\boldsymbol{h}\|_{L^{2}_{T}(L^{2})}^{2}\leq 2\|\nabla(\boldsymbol{u}_{0}-\boldsymbol{v}_{0})\|_{L^{2}}^{2}\exp\bigl(CA^{2}B^{2}\bigr)\,\bigr\}.

Let us take T=sup{T:T𝒟}T^{*}=\sup\{T:T\in{\mathcal{D}}\}. If T<T^{*}<\infty, then for any tTt\leq T^{*}, we can use the estimate (2.13) and the smallness condition (2.9) with c0c_{0} sufficiently small to deduce

C𝒉Lt(L2)12𝒉Lt(L2)12C𝒖0𝒗0L212(𝒖0𝒗0)L212exp(CA2B2)Cc012<12.\displaystyle C\|\boldsymbol{h}\|_{L^{\infty}_{t}(L^{2})}^{\frac{1}{2}}\|\nabla\boldsymbol{h}\|_{L^{\infty}_{t}(L^{2})}^{\frac{1}{2}}\leq C\|\boldsymbol{u}_{0}-\boldsymbol{v}_{0}\|_{L^{2}}^{\frac{1}{2}}\|\nabla(\boldsymbol{u}_{0}-\boldsymbol{v}_{0})\|_{L^{2}}^{\frac{1}{2}}\exp\bigl(CA^{2}B^{2}\bigr)\leq Cc_{0}^{\frac{1}{2}}<\frac{1}{2}.

By substituting this into (2.14), and then using Gronwall’s inequality, we achieve

𝒉(t)L22+Δ𝒉Lt2(L2)2\displaystyle\|\nabla\boldsymbol{h}(t)\|_{L^{2}}^{2}+\|\Delta\boldsymbol{h}\|_{L^{2}_{t}(L^{2})}^{2} (𝒖0𝒗0)L22exp(C𝒗Lt(L2)2𝒗Lt2(L2)2)\displaystyle\leq\|\nabla(\boldsymbol{u}_{0}-\boldsymbol{v}_{0})\|_{L^{2}}^{2}\exp\bigl(C\|\nabla\boldsymbol{v}\|_{L^{\infty}_{t}(L^{2})}^{2}\|\nabla\boldsymbol{v}\|_{L^{2}_{t}(L^{2})}^{2}\bigr)
(𝒖0𝒗0)L22exp(CA2B2),\displaystyle\leq\|\nabla(\boldsymbol{u}_{0}-\boldsymbol{v}_{0})\|_{L^{2}}^{2}\exp\bigl(CA^{2}B^{2}\bigr),

which contradicts to the definition of TT^{*}. Thus there must be T=T^{*}=\infty, and we have

(2.15) 𝒉L(+;L2)2+Δ𝒉L2(+;L2)22(𝒖0𝒗0)L22exp(CA2B2).\|\nabla\boldsymbol{h}\|_{L^{\infty}(\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{+};L^{2})}^{2}+\|\Delta\boldsymbol{h}\|_{L^{2}(\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{+};L^{2})}^{2}\leq 2\|\nabla(\boldsymbol{u}_{0}-\boldsymbol{v}_{0})\|_{L^{2}}^{2}\exp\bigl(CA^{2}B^{2}\bigr).

Step 2. The proof of (2.11). Let us denote 𝜹=defcurl𝒉\boldsymbol{\delta}\mathrel{\mathop{\kern 0.0pt=}\limits^{\hbox{\footnotesize def}}}\mathop{\rm curl}\nolimits\boldsymbol{h} and 𝝎=defcurl𝒗\boldsymbol{\omega}\mathrel{\mathop{\kern 0.0pt=}\limits^{\hbox{\footnotesize def}}}\mathop{\rm curl}\nolimits\boldsymbol{v}, which satisfy

(2.16) {t𝜹+𝒖𝜹+𝒉𝝎Δ𝜹=𝜹𝒖+𝝎𝒉,𝜹|t=0=curl(𝒖0𝒗0).\left\{\begin{split}&\partial_{t}\boldsymbol{\delta}+\boldsymbol{u}\cdot\nabla\boldsymbol{\delta}+\boldsymbol{h}\cdot\nabla\boldsymbol{\omega}-\Delta\boldsymbol{\delta}=\boldsymbol{\delta}\cdot\nabla\boldsymbol{u}+\boldsymbol{\omega}\cdot\nabla\boldsymbol{h},\\ &\boldsymbol{\delta}|_{t=0}=\mathop{\rm curl}\nolimits(\boldsymbol{u}_{0}-\boldsymbol{v}_{0}).\end{split}\right.

By taking L2L^{2} inner product of (2.16) wit |𝜹|2𝜹|\boldsymbol{\delta}|^{2}\boldsymbol{\delta}, we get

(2.17) 14ddt𝜹L44+|𝜹|𝜹L22+12|𝜹|2L22|3(𝜹𝒖+𝝎𝒉𝒉𝝎)|𝜹|2𝜹dx|.\frac{1}{4}\frac{d}{dt}\|\boldsymbol{\delta}\|_{L^{4}}^{4}+\bigl\||\boldsymbol{\delta}|\nabla\boldsymbol{\delta}\bigr\|_{L^{2}}^{2}+\frac{1}{2}\bigl\|\nabla|\boldsymbol{\delta}|^{2}\bigr\|_{L^{2}}^{2}\leq\Bigl|\int_{\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{3}}(\boldsymbol{\delta}\cdot\nabla\boldsymbol{u}+\boldsymbol{\omega}\cdot\nabla\boldsymbol{h}-\boldsymbol{h}\cdot\nabla\boldsymbol{\omega})\cdot|\boldsymbol{\delta}|^{2}\boldsymbol{\delta}\,dx\Bigr|.

The terms on the right-hand side can be handled as follows:

|3(𝜹𝒖)|𝜹|2𝜹𝑑x|\displaystyle\Bigl|\int_{\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{3}}(\boldsymbol{\delta}\cdot\nabla\boldsymbol{u})\cdot|\boldsymbol{\delta}|^{2}\boldsymbol{\delta}\,dx\Bigr| |𝜹|2L3|𝜹|2L6(𝒗+𝒉)L2\displaystyle\leq\bigl\||\boldsymbol{\delta}|^{2}\bigr\|_{L^{3}}\bigl\||\boldsymbol{\delta}|^{2}\bigr\|_{L^{6}}\|\nabla(\boldsymbol{v}+\boldsymbol{h})\|_{L^{2}}
18|𝜹|2L22+C|𝜹|2L22(𝝎L24+𝒉L24),\displaystyle\leq\frac{1}{8}\bigl\|\nabla|\boldsymbol{\delta}|^{2}\bigr\|_{L^{2}}^{2}+C\bigl\||\boldsymbol{\delta}|^{2}\bigr\|_{L^{2}}^{2}\bigl(\|\boldsymbol{\omega}\|_{L^{2}}^{4}+\|\nabla\boldsymbol{h}\|_{L^{2}}^{4}\bigr),

and by using the Biot-Savart law that

|3(𝝎𝒉)|𝜹|2𝜹𝑑x|\displaystyle\Bigl|\int_{\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{3}}(\boldsymbol{\omega}\cdot\nabla\boldsymbol{h})\cdot|\boldsymbol{\delta}|^{2}\boldsymbol{\delta}\,dx\Bigr| 𝝎L2𝒉L6|𝜹|2L6𝜹L6\displaystyle\leq\|\boldsymbol{\omega}\|_{L^{2}}\|\nabla\boldsymbol{h}\|_{L^{6}}\bigl\||\boldsymbol{\delta}|^{2}\bigr\|_{L^{6}}\|\boldsymbol{\delta}\|_{L^{6}}
C𝝎L2|𝜹|2L3|𝜹|2L6\displaystyle\leq C\|\boldsymbol{\omega}\|_{L^{2}}\bigl\||\boldsymbol{\delta}|^{2}\bigr\|_{L^{3}}\bigl\||\boldsymbol{\delta}|^{2}\bigr\|_{L^{6}}
18|𝜹|2L22+C|𝜹|2L22𝝎L24,\displaystyle\leq\frac{1}{8}\bigl\|\nabla|\boldsymbol{\delta}|^{2}\bigr\|_{L^{2}}^{2}+C\bigl\||\boldsymbol{\delta}|^{2}\bigr\|_{L^{2}}^{2}\|\boldsymbol{\omega}\|_{L^{2}}^{4},

and by using integration by parts together with the divergence-free condition that

|3(\displaystyle\Bigl|\int_{\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{3}}( 𝒉𝝎)|𝜹|2𝜹dx|=|3(𝝎𝒉):(|𝜹|2𝜹)dx|\displaystyle\boldsymbol{h}\cdot\nabla\boldsymbol{\omega})\cdot|\boldsymbol{\delta}|^{2}\boldsymbol{\delta}\,dx\Bigr|=\Bigl|\int_{\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{3}}(\boldsymbol{\omega}\otimes\boldsymbol{h}):\nabla\bigl(|\boldsymbol{\delta}|^{2}\boldsymbol{\delta}\bigr)\,dx\Bigr|
C(|𝜹|2L2+|𝜹|𝜹L2)𝜹L12𝒉L12𝝎L3\displaystyle\leq C\bigl(\bigl\|\nabla|\boldsymbol{\delta}|^{2}\bigr\|_{L^{2}}+\bigl\||\boldsymbol{\delta}|\nabla\boldsymbol{\delta}\bigr\|_{L^{2}}\bigr)\|\boldsymbol{\delta}\|_{L^{12}}\|\boldsymbol{h}\|_{L^{12}}\|\boldsymbol{\omega}\|_{L^{3}}
C(|𝜹|2L2+|𝜹|𝜹L2)|𝜹|2L212𝒉L412𝒉L412𝝎L212𝝎L212\displaystyle\leq C\bigl(\bigl\|\nabla|\boldsymbol{\delta}|^{2}\bigr\|_{L^{2}}+\bigl\||\boldsymbol{\delta}|\nabla\boldsymbol{\delta}\bigr\|_{L^{2}}\bigr)\bigl\|\nabla|\boldsymbol{\delta}|^{2}\bigr\|_{L^{2}}^{\frac{1}{2}}\|\boldsymbol{h}\|_{L^{4}}^{\frac{1}{2}}\|\nabla\boldsymbol{h}\|_{L^{4}}^{\frac{1}{2}}\|\boldsymbol{\omega}\|_{L^{2}}^{\frac{1}{2}}\|\nabla\boldsymbol{\omega}\|_{L^{2}}^{\frac{1}{2}}
18(|𝜹|2L22+|𝜹|𝜹L22)+C(𝒉L44+𝒉L44)𝝎L22𝝎L22.\displaystyle\leq\frac{1}{8}\bigl(\bigl\|\nabla|\boldsymbol{\delta}|^{2}\bigr\|_{L^{2}}^{2}+\bigl\||\boldsymbol{\delta}|\nabla\boldsymbol{\delta}\bigr\|_{L^{2}}^{2}\bigr)+C\bigl(\|\boldsymbol{h}\|_{L^{4}}^{4}+\|\nabla\boldsymbol{h}\|_{L^{4}}^{4}\bigr)\|\boldsymbol{\omega}\|_{L^{2}}^{2}\|\nabla\boldsymbol{\omega}\|_{L^{2}}^{2}.

Now by substituting the above three estimates into (2.18), and using the relation that

𝒉L4curl𝒉L4=𝜹L4,\|\nabla\boldsymbol{h}\|_{L^{4}}\lesssim\|\mathop{\rm curl}\nolimits\boldsymbol{h}\|_{L^{4}}=\|\boldsymbol{\delta}\|_{L^{4}},

we get

ddt𝜹L44+|𝜹|𝜹L22+|𝜹|2L22𝜹L44(𝝎L22𝝎H12+𝒉L24)+𝒉L44𝝎L22𝝎L22.\displaystyle\frac{d}{dt}\|\boldsymbol{\delta}\|_{L^{4}}^{4}+\bigl\||\boldsymbol{\delta}|\nabla\boldsymbol{\delta}\bigr\|_{L^{2}}^{2}+\bigl\|\nabla|\boldsymbol{\delta}|^{2}\bigr\|_{L^{2}}^{2}\lesssim\|\boldsymbol{\delta}\|_{L^{4}}^{4}\bigl(\|\boldsymbol{\omega}\|_{L^{2}}^{2}\|\boldsymbol{\omega}\|_{H^{1}}^{2}+\|\nabla\boldsymbol{h}\|_{L^{2}}^{4}\bigr)+\|\boldsymbol{h}\|_{L^{4}}^{4}\|\boldsymbol{\omega}\|_{L^{2}}^{2}\|\nabla\boldsymbol{\omega}\|_{L^{2}}^{2}.

Then Gronwall’s inequality together with the bounds (2.8) and (2.10) leads to

(2.18) 𝜹Lt(L4)4((𝒖0𝒗0)L44+𝒉Lt(L4)4𝝎Lt(L2)2𝝎Lt2(L2)2)×exp(C𝝎Lt(L2)2𝝎Lt2(H1)2+C𝒉Lt(L2)2𝒉Lt2(L2)2)(𝒖0𝒗0H˙744+B4𝒖0𝒗0L2𝒖0𝒗0H˙13)exp(CA2B2+CB4+Cc02)𝒖0𝒗0H24exp(CA2B2+CB4).\begin{split}\|\boldsymbol{\delta}\|_{L^{\infty}_{t}(L^{4})}^{4}\lesssim&\bigl(\|\nabla(\boldsymbol{u}_{0}-\boldsymbol{v}_{0})\|_{L^{4}}^{4}+\|\boldsymbol{h}\|_{L^{\infty}_{t}(L^{4})}^{4}\|\boldsymbol{\omega}\|_{L^{\infty}_{t}(L^{2})}^{2}\|\nabla\boldsymbol{\omega}\|_{L^{2}_{t}(L^{2})}^{2}\bigr)\\ &\times\exp\bigl(C\|\boldsymbol{\omega}\|_{L^{\infty}_{t}(L^{2})}^{2}\|\boldsymbol{\omega}\|_{L^{2}_{t}(H^{1})}^{2}+C\|\nabla\boldsymbol{h}\|_{L^{\infty}_{t}(L^{2})}^{2}\|\nabla\boldsymbol{h}\|_{L^{2}_{t}(L^{2})}^{2}\bigr)\\ \lesssim&\bigl(\|\boldsymbol{u}_{0}-\boldsymbol{v}_{0}\|_{\dot{H}^{\frac{7}{4}}}^{4}+B^{4}\|\boldsymbol{u}_{0}-\boldsymbol{v}_{0}\|_{L^{2}}\|\boldsymbol{u}_{0}-\boldsymbol{v}_{0}\|_{\dot{H}^{1}}^{3}\bigr)\exp\bigl(CA^{2}B^{2}+CB^{4}+Cc_{0}^{2}\bigr)\\ \lesssim&\|\boldsymbol{u}_{0}-\boldsymbol{v}_{0}\|_{H^{2}}^{4}\exp\bigl(CA^{2}B^{2}+CB^{4}\bigr).\end{split}

Now interpolating between (2.15) and (2.18) gives

𝒉Lt(L)\displaystyle\|\boldsymbol{h}\|_{L^{\infty}_{t}(L^{\infty})} 𝒉Lt(L2)13𝒉Lt(L4)23\displaystyle\lesssim\|\nabla\boldsymbol{h}\|_{L^{\infty}_{t}(L^{2})}^{\frac{1}{3}}\|\nabla\boldsymbol{h}\|_{L^{\infty}_{t}(L^{4})}^{\frac{2}{3}}
𝜹Lt(L2)13𝜹Lt(L4)23𝒖0𝒗0H2exp(CA2B2+CB4),\displaystyle\lesssim\|\boldsymbol{\delta}\|_{L^{\infty}_{t}(L^{2})}^{\frac{1}{3}}\|\boldsymbol{\delta}\|_{L^{\infty}_{t}(L^{4})}^{\frac{2}{3}}\lesssim\|\boldsymbol{u}_{0}-\boldsymbol{v}_{0}\|_{H^{2}}\exp\bigl(CA^{2}B^{2}+CB^{4}\bigr),

which is exactly the desired estimate (2.11). This completes the proof of this proposition. ∎

3. The proof of Theorem 1.1

The purpose of this section is to prove Theorem 1.1 by using perturbation method.

3.1. Global solvability of (1.6)

Let us first introduce the velocity field 𝒖~(x)=u~r(r,z)𝒆r+u~z(r,z)𝒆z\widetilde{\boldsymbol{u}}(x)=\widetilde{u}^{r}(r,z)\boldsymbol{e}_{r}+\widetilde{u}^{z}(r,z)\boldsymbol{e}_{z} satisfying the following axisymmetric without swirl N-S:

(3.1) {tu~r+(u~rr+u~zz)u~r(r2+z2+1rr1r2)u~r+rP~=0,tu~z+(u~rr+u~zz)u~z(r2+z2+1rr)u~z+zP~=0,ru~r+1ru~r+zu~z=0,u~r|t=0=u~r0=(u0r),u~z|t=0=u~z0=(u0z).\left\{\begin{split}&\partial_{t}\widetilde{u}^{r}+(\widetilde{u}^{r}\partial_{r}+\widetilde{u}^{z}\partial_{z})\widetilde{u}^{r}-(\partial_{r}^{2}+\partial_{z}^{2}+\frac{1}{r}\partial_{r}-\frac{1}{r^{2}})\widetilde{u}^{r}+\partial_{r}\widetilde{P}=0,\\ &\partial_{t}\widetilde{u}^{z}+(\widetilde{u}^{r}\partial_{r}+\widetilde{u}^{z}\partial_{z})\widetilde{u}^{z}-(\partial_{r}^{2}+\partial_{z}^{2}+\frac{1}{r}\partial_{r})\widetilde{u}^{z}+\partial_{z}\widetilde{P}=0,\\ &\partial_{r}\widetilde{u}^{r}+\frac{1}{r}\widetilde{u}^{r}+\partial_{z}\widetilde{u}^{z}=0,\\ &\widetilde{u}^{r}|_{t=0}=\widetilde{u}^{r}_{0}={\mathcal{M}}(u_{0}^{r}),\ \widetilde{u}^{z}|_{t=0}=\widetilde{u}^{z}_{0}={\mathcal{M}}(u_{0}^{z}).\end{split}\right.
Proposition 3.1.

Under the assumption of Theorem 1.1, (3.1) has a unique global solution 𝒖~\widetilde{\boldsymbol{u}} such that for any time t>0t>0, there hold

(3.2) 𝒖~Lt(L2)2+2𝒖~Lt2(L2)2𝒖0L22,\|\widetilde{\boldsymbol{u}}\|_{L^{\infty}_{t}(L^{2})}^{2}+2\|\nabla\widetilde{\boldsymbol{u}}\|_{L^{2}_{t}(L^{2})}^{2}\leq\|{\boldsymbol{u}}_{0}\|_{L^{2}}^{2},
(3.3) 𝒖~Lt(H˙1)2+𝒖~Lt2(H˙1)2𝒖0H˙12+𝒖0L24𝒖0H˙22.\|\widetilde{\boldsymbol{u}}\|_{L^{\infty}_{t}(\dot{H}^{1})}^{2}+\|\nabla\widetilde{\boldsymbol{u}}\|_{L^{2}_{t}(\dot{H}^{1})}^{2}\lesssim\|{\boldsymbol{u}}_{0}\|_{\dot{H}^{1}}^{2}+\|{\boldsymbol{u}}_{0}\|_{L^{2}}^{4}\|{\boldsymbol{u}}_{0}\|_{\dot{H}^{2}}^{2}.
Proof.

The first estimate (3.2) is nothing but the energy equality and the fact that

𝒖~0L22=(u0r)L22+(u0z)L22𝒖0L22.\|\widetilde{\boldsymbol{u}}_{0}\|_{L^{2}}^{2}=\|{\mathcal{M}}(u_{0}^{r})\|_{L^{2}}^{2}+\|{\mathcal{M}}(u_{0}^{z})\|_{L^{2}}^{2}\leq\|{\boldsymbol{u}}_{0}\|_{L^{2}}^{2}.

Next, the Biot-Savart law tells us that we can use curl𝒖~=ω~θ𝒆θ=(zu~rru~z)𝒆θ\mathop{\rm curl}\nolimits\widetilde{\boldsymbol{u}}=\widetilde{\omega}^{\theta}\boldsymbol{e}_{\theta}=(\partial_{z}\widetilde{u}^{r}-\partial_{r}\widetilde{u}^{z})\boldsymbol{e}_{\theta} to represent 𝒖~\widetilde{\boldsymbol{u}}. Hence we can reformulate the System (3.1) as

(3.4) {tω~θ+(u~rr+u~zz)ω~θ(r2+z2+1rr1r2)ω~θu~rω~θr=0,ω~θ|t=0=ω~0θ=(zu0rru0z).\left\{\begin{split}&\partial_{t}\widetilde{\omega}^{\theta}+(\widetilde{u}^{r}\partial_{r}+\widetilde{u}^{z}\partial_{z})\widetilde{\omega}^{\theta}-(\partial_{r}^{2}+\partial_{z}^{2}+\frac{1}{r}\partial_{r}-\frac{1}{r^{2}})\widetilde{\omega}^{\theta}-\frac{\widetilde{u}^{r}\widetilde{\omega}^{\theta}}{r}=0,\\ &\widetilde{\omega}^{\theta}|_{t=0}=\widetilde{\omega}^{\theta}_{0}={\mathcal{M}}(\partial_{z}u^{r}_{0}-\partial_{r}u^{z}_{0}).\end{split}\right.

Then it is not difficult to verify that ω~θ/r\widetilde{\omega}^{\theta}/r satisfies

(3.5) tω~θr+(u~rr+u~zz)ω~θr(Δ+2rr)ω~θr=0.\partial_{t}\frac{\widetilde{\omega}^{\theta}}{r}+(\widetilde{u}^{r}\partial_{r}+\widetilde{u}^{z}\partial_{z})\frac{\widetilde{\omega}^{\theta}}{r}-(\Delta+\frac{2}{r}\partial_{r})\frac{\widetilde{\omega}^{\theta}}{r}=0.

For a strong solution of N-S, the decay property at infinity implies ω~θ|r==0\widetilde{\omega}^{\theta}|_{r=\infty}=0, while the smoothness implies ω~θ|r=0=0\widetilde{\omega}^{\theta}|_{r=0}=0. As a result, we have

32rrω~θrω~θrdx=2π+×r|ω~θr|2drdz=2πlimr0|ω~θr|2dz0.-\int_{\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{3}}\frac{2}{r}\partial_{r}\frac{\widetilde{\omega}^{\theta}}{r}\cdot\frac{\widetilde{\omega}^{\theta}}{r}\,dx=-2\pi\int_{\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{+}\times\mathop{\mathbb{R}\kern 0.0pt}\nolimits}\partial_{r}\bigl|\frac{\widetilde{\omega}^{\theta}}{r}\bigr|^{2}\,drdz=2\pi\int_{\mathop{\mathbb{R}\kern 0.0pt}\nolimits}\lim_{r\rightarrow 0}\bigl|\frac{\widetilde{\omega}^{\theta}}{r}\bigr|^{2}\,dz\geq 0.

In view of this, the L2L^{2} energy estimate of ω~θ/r\widetilde{\omega}^{\theta}/r in (3.5) gives

(3.6) ω~θrLt(L2)+ω~θrLt2(L2)ω~0θrL2.\bigl\|\frac{\widetilde{\omega}^{\theta}}{r}\bigr\|_{L^{\infty}_{t}(L^{2})}+\bigl\|\nabla\frac{\widetilde{\omega}^{\theta}}{r}\bigr\|_{L^{2}_{t}(L^{2})}\leq\bigl\|\frac{\widetilde{\omega}^{\theta}_{0}}{r}\bigr\|_{L^{2}}.

By using (2.2) and Lemma 2.1, we have

2𝒖0L2𝝎0L2\displaystyle\|\nabla^{2}\boldsymbol{u}_{0}\|_{L^{2}}\sim\|\nabla\boldsymbol{\omega}_{0}\|_{L^{2}} θr(𝝎0)𝒆rL2=ω0θr+θω0rrL2\displaystyle\geq\bigl\|\frac{\partial_{\theta}}{r}(\boldsymbol{\omega}_{0})\cdot\boldsymbol{e}_{r}\bigr\|_{L^{2}}=\bigl\|-\frac{\omega^{\theta}_{0}}{r}+\frac{\partial_{\theta}\omega^{r}_{0}}{r}\bigr\|_{L^{2}}
(ω0θr+θω0rr)L2=(ω0θr)L2=ω~0θrL2,\displaystyle\geq\bigl\|{\mathcal{M}}\bigl(-\frac{\omega^{\theta}_{0}}{r}+\frac{\partial_{\theta}\omega^{r}_{0}}{r}\bigr)\bigr\|_{L^{2}}=\bigl\|{\mathcal{M}}\bigl(-\frac{\omega^{\theta}_{0}}{r}\bigr)\bigr\|_{L^{2}}=\bigl\|\frac{\widetilde{\omega}^{\theta}_{0}}{r}\bigr\|_{L^{2}},

where 𝝎0=defcurl𝒖0\boldsymbol{\omega}_{0}\mathrel{\mathop{\kern 0.0pt=}\limits^{\hbox{\footnotesize def}}}\mathop{\rm curl}\nolimits\boldsymbol{u}_{0}. Substituting this into (3.6) gives

(3.7) ω~θrLt(L2)+ω~θrLt2(L2)𝒖0H˙2.\bigl\|\frac{\widetilde{\omega}^{\theta}}{r}\bigr\|_{L^{\infty}_{t}(L^{2})}+\bigl\|\nabla\frac{\widetilde{\omega}^{\theta}}{r}\bigr\|_{L^{2}_{t}(L^{2})}\leq\|\boldsymbol{u}_{0}\|_{\dot{H}^{2}}.

Next, by taking L2L^{2} inner product of (3.4) with ω~θ\widetilde{\omega}^{\theta}, we obtain

(3.8) 12ddtω~θL22+ω~θL22+ω~θrL223u~rr|ω~θ|2𝑑x.\frac{1}{2}\frac{d}{dt}\|\widetilde{\omega}^{\theta}\|_{L^{2}}^{2}+\|\nabla\widetilde{\omega}^{\theta}\|_{L^{2}}^{2}+\bigl\|\frac{\widetilde{\omega}^{\theta}}{r}\|_{L^{2}}^{2}\leq\int_{\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{3}}\frac{\widetilde{u}^{r}}{r}|\widetilde{\omega}^{\theta}|^{2}\,dx.

For the right-hand side term, we have

|3u~rr|ω~θ|2𝑑x|\displaystyle\bigl|\int_{\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{3}}\frac{\widetilde{u}^{r}}{r}|\widetilde{\omega}^{\theta}|^{2}\,dx\bigr| u~rL2ω~θL6ω~θrL212ω~θrL612\displaystyle\leq\|\widetilde{u}^{r}\|_{L^{2}}\|\widetilde{\omega}^{\theta}\|_{L^{6}}\bigl\|\frac{\widetilde{\omega}^{\theta}}{r}\bigr\|_{L^{2}}^{\frac{1}{2}}\bigl\|\frac{\widetilde{\omega}^{\theta}}{r}\bigr\|_{L^{6}}^{\frac{1}{2}}
12(ω~θL22+ω~θrL22)+Cu~rL24(ω~θr)L22.\displaystyle\leq\frac{1}{2}\bigl(\|\nabla\widetilde{\omega}^{\theta}\|_{L^{2}}^{2}+\bigl\|\frac{\widetilde{\omega}^{\theta}}{r}\bigr\|_{L^{2}}^{2}\bigr)+C\|\widetilde{u}^{r}\|_{L^{2}}^{4}\|\nabla\bigl(\frac{\widetilde{\omega}^{\theta}}{r}\bigr)\|_{L^{2}}^{2}.

Substituting this into (3.8) and then integrating in time, we deduce

(3.9) ω~θLt(L2)2+ω~θLt2(L2)2+ω~θrLt2(L2)2ω~0θL22+Cu~rLt(L2)4(ω~θr)Lt2(L2)2.\|\widetilde{\omega}^{\theta}\|_{L^{\infty}_{t}(L^{2})}^{2}+\|\nabla\widetilde{\omega}^{\theta}\|_{L^{2}_{t}(L^{2})}^{2}+\|\frac{\widetilde{\omega}^{\theta}}{r}\|_{L^{2}_{t}(L^{2})}^{2}\leq\|\widetilde{\omega}^{\theta}_{0}\|_{L^{2}}^{2}+C\|\widetilde{u}^{r}\|_{L^{\infty}_{t}(L^{2})}^{4}\|\nabla\bigl(\frac{\widetilde{\omega}^{\theta}}{r}\bigr)\|_{L^{2}_{t}(L^{2})}^{2}.

Thanks to the estimates (3.7) and (3.2) , we finally dedecue from (3.9) that

ω~θLt(L2)2+ω~θLt2(L2)2+ω~θ/rLt2(L2)2𝒖0H˙12+𝒖0L24𝒖0H˙22,\displaystyle\|\widetilde{\omega}^{\theta}\|_{L^{\infty}_{t}(L^{2})}^{2}+\|\nabla\widetilde{\omega}^{\theta}\|_{L^{2}_{t}(L^{2})}^{2}+\|\widetilde{\omega}^{\theta}/r\|_{L^{2}_{t}(L^{2})}^{2}\lesssim\|{\boldsymbol{u}}_{0}\|_{\dot{H}^{1}}^{2}+\|{\boldsymbol{u}}_{0}\|_{L^{2}}^{4}\|{\boldsymbol{u}}_{0}\|_{\dot{H}^{2}}^{2},

which together with Lemma 2.2 leads to the second desired estimate (3.3). ∎

Next, we shall use Proposition 2.1 to derive the global existence of the solution to (1.6).

Proposition 3.2.

Under the assumption of Theorem 1.1, (1.6) has a unique global solution 𝒖¯\bar{\boldsymbol{u}} such that for any time t>0t>0, there hold

(3.10) 𝒖¯Lt(L2)2+2𝒖¯Lt2(L2)2𝒖0L22,\|\bar{\boldsymbol{u}}\|_{L^{\infty}_{t}(L^{2})}^{2}+2\|\nabla\bar{\boldsymbol{u}}\|_{L^{2}_{t}(L^{2})}^{2}\leq\|{\boldsymbol{u}}_{0}\|_{L^{2}}^{2},
(3.11) 𝒖¯Lt(H˙1)2+𝒖¯Lt2(H˙1)2𝒖0L22exp(C𝒖0L26𝒖0H˙22).\|\bar{\boldsymbol{u}}\|_{L^{\infty}_{t}(\dot{H}^{1})}^{2}+\|\nabla\bar{\boldsymbol{u}}\|_{L^{2}_{t}(\dot{H}^{1})}^{2}\lesssim\|\nabla\boldsymbol{u}_{0}\|_{L^{2}}^{2}\exp\bigl(C\|{\boldsymbol{u}}_{0}\|_{L^{2}}^{6}\|{\boldsymbol{u}}_{0}\|_{\dot{H}^{2}}^{2}\bigr).
Proof.

By using Lemma 2.1 and the fact that 𝒖¯0𝒖~0=u¯0θ(r,z)𝒆θ=(u0θ)𝒆θ\bar{\boldsymbol{u}}_{0}-\widetilde{\boldsymbol{u}}_{0}=\bar{u}^{\theta}_{0}(r,z)\boldsymbol{e}_{\theta}={\mathcal{M}}(u^{\theta}_{0})\boldsymbol{e}_{\theta}, we have

𝒖¯0𝒖~0L2=(u0θ)L2u0θL2,\displaystyle\|\bar{\boldsymbol{u}}_{0}-\widetilde{\boldsymbol{u}}_{0}\|_{L^{2}}=\|{\mathcal{M}}(u^{\theta}_{0})\|_{L^{2}}\leq\|u^{\theta}_{0}\|_{L^{2}},

and

(𝒖¯0𝒖~0)L22\displaystyle\|\nabla(\bar{\boldsymbol{u}}_{0}-\widetilde{\boldsymbol{u}}_{0})\|_{L^{2}}^{2} =((u0θ)𝒆θ)L22=~(u0θ)L22+(u0θ)rL22\displaystyle=\bigl\|\nabla\bigl({\mathcal{M}}(u^{\theta}_{0})\boldsymbol{e}_{\theta}\bigr)\bigr\|_{L^{2}}^{2}=\|\widetilde{\nabla}{\mathcal{M}}(u^{\theta}_{0})\|_{L^{2}}^{2}+\bigl\|\frac{{\mathcal{M}}(u^{\theta}_{0})}{r}\bigr\|_{L^{2}}^{2}
=(~u0θ)L22+min{(u0θr)L22,(u0θθu0rr)L22}\displaystyle=\|{\mathcal{M}}(\widetilde{\nabla}u^{\theta}_{0})\|_{L^{2}}^{2}+\min\Bigl\{\bigl\|{\mathcal{M}}\bigl(\frac{u^{\theta}_{0}}{r}\bigr)\bigr\|_{L^{2}}^{2},\bigl\|{\mathcal{M}}\bigl(\frac{u^{\theta}_{0}-\partial_{\theta}u^{r}_{0}}{r}\bigr)\bigr\|_{L^{2}}^{2}\Bigr\}
~u0θL22+min{u0θrL22,u0θθu0rrL22}\displaystyle\leq\|\widetilde{\nabla}u^{\theta}_{0}\|_{L^{2}}^{2}+\min\Bigl\{\bigl\|\frac{u^{\theta}_{0}}{r}\bigr\|_{L^{2}}^{2},\bigl\|\frac{u^{\theta}_{0}-\partial_{\theta}u^{r}_{0}}{r}\bigr\|_{L^{2}}^{2}\Bigr\}
min{u0θH˙axi12,𝒖0H˙12}.\displaystyle\leq\min\bigl\{\|u^{\theta}_{0}\|_{\dot{H}^{1}_{\rm axi}}^{2},\|{\boldsymbol{u}}_{0}\|_{\dot{H}^{1}}^{2}\bigr\}.

These together with the bounds (3.2), (3.3) and the smallness condition (1.9), we get that

𝒖¯0𝒖~0L2𝒖¯0𝒖~0H˙1exp(C𝒖0L22(𝒖0H˙12+𝒖0L24𝒖0H˙22))Cu0θL2u0θH˙axi1exp(C𝒖0L26𝒖0H˙22)<c0,\displaystyle\begin{aligned} &\|\bar{\boldsymbol{u}}_{0}-\widetilde{\boldsymbol{u}}_{0}\|_{L^{2}}\|\bar{\boldsymbol{u}}_{0}-\widetilde{\boldsymbol{u}}_{0}\|_{\dot{H}^{1}}\exp\bigl(C\|{\boldsymbol{u}}_{0}\|_{L^{2}}^{2}(\|{\boldsymbol{u}}_{0}\|_{\dot{H}^{1}}^{2}+\|{\boldsymbol{u}}_{0}\|_{L^{2}}^{4}\|{\boldsymbol{u}}_{0}\|_{\dot{H}^{2}}^{2})\bigr)\\ &\qquad\leq C\|u^{\theta}_{0}\|_{L^{2}}\|u^{\theta}_{0}\|_{\dot{H}^{1}_{\rm axi}}\exp\bigl(C\|{\boldsymbol{u}}_{0}\|_{L^{2}}^{6}\|{\boldsymbol{u}}_{0}\|_{\dot{H}^{2}}^{2}\bigr)<c_{0},\end{aligned}

where we used the fact that

𝒖0L22𝒖0H˙12𝒖0L23𝒖0H˙21+𝒖0L26𝒖0H˙22.\displaystyle\|{\boldsymbol{u}}_{0}\|_{L^{2}}^{2}\|{\boldsymbol{u}}_{0}\|_{\dot{H}^{1}}^{2}\lesssim\|{\boldsymbol{u}}_{0}\|_{L^{2}}^{3}\|{\boldsymbol{u}}_{0}\|_{\dot{H}^{2}}\lesssim 1+\|{\boldsymbol{u}}_{0}\|_{L^{2}}^{6}\|{\boldsymbol{u}}_{0}\|_{\dot{H}^{2}}^{2}.

So that the condition (2.9) in Proposition 2.1 is fulfilled. Thus (1.6) has a unique global strong solution 𝒖¯\bar{\boldsymbol{u}} such that

𝒖¯𝒖~L(+;H˙1)2+𝒖¯𝒖~L2(+;H˙2)2min{u0θH˙axi12,𝒖0H˙12}exp(C𝒖0L26𝒖0H˙22),\|\bar{\boldsymbol{u}}-\widetilde{\boldsymbol{u}}\|_{L^{\infty}(\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{+};\dot{H}^{1})}^{2}+\|\bar{\boldsymbol{u}}-\widetilde{\boldsymbol{u}}\|_{L^{2}(\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{+};\dot{H}^{2})}^{2}\lesssim\min\bigl\{\|u^{\theta}_{0}\|_{\dot{H}^{1}_{\rm axi}}^{2},\|{\boldsymbol{u}}_{0}\|_{\dot{H}^{1}}^{2}\bigr\}\exp\bigl(C\|{\boldsymbol{u}}_{0}\|_{L^{2}}^{6}\|{\boldsymbol{u}}_{0}\|_{\dot{H}^{2}}^{2}\bigr),

which together with (3.3) leads to the desired estimate (3.11).

The estimate (3.10) follows from the Basic energy equality of Navier-Stokes equations. Thus, we complete the proof of the proposition. ∎

3.2. The proof of Theorem 1.1

The goal of this subsection is to prove Theorem 1.1.

The proof of Theorem 1.1.

We divide the proof into two steps.

Step 1. Global solvability of (1.4). The strategy is still to use Proposition 2.1. To do this, we need to analyse the difference between 𝒖0\boldsymbol{u}_{0} and 𝒖¯0\bar{\boldsymbol{u}}_{0}, which reads as follows:

𝒖0𝒖¯0=(u0r(u0r))er+(u0θ(u0θ))eθ+(u0z(u0z))ez,\boldsymbol{u}_{0}-\bar{\boldsymbol{u}}_{0}=\bigl(u_{0}^{r}-{\mathcal{M}}(u_{0}^{r})\bigr)e_{r}+\bigl(u_{0}^{\theta}-{\mathcal{M}}(u_{0}^{\theta})\bigr)e_{\theta}+\bigl(u_{0}^{z}-{\mathcal{M}}(u_{0}^{z})\bigr)e_{z},
~(𝒖0𝒖¯0)=(~u0r(~u0r))er+(~u0θ(~u0θ))eθ+(~u0z(~u0z))ez,\widetilde{\nabla}(\boldsymbol{u}_{0}-\bar{\boldsymbol{u}}_{0})=\bigl(\widetilde{\nabla}u_{0}^{r}-{\mathcal{M}}(\widetilde{\nabla}u_{0}^{r})\bigr)e_{r}+\bigl(\widetilde{\nabla}u_{0}^{\theta}-{\mathcal{M}}(\widetilde{\nabla}u_{0}^{\theta})\bigr)e_{\theta}+\bigl(\widetilde{\nabla}u_{0}^{z}-{\mathcal{M}}(\widetilde{\nabla}u_{0}^{z})\bigr)e_{z},

and

θr(𝒖0𝒖¯0)=(θu0rru0θr+(u0θr))er+(θu0θr+u0rr(u0rr))eθ+(θu0zr)ez.\frac{\partial_{\theta}}{r}(\boldsymbol{u}_{0}-\bar{\boldsymbol{u}}_{0})=\Bigl(\frac{\partial_{\theta}u_{0}^{r}}{r}-\frac{u_{0}^{\theta}}{r}+{\mathcal{M}}\bigl(\frac{u_{0}^{\theta}}{r}\bigr)\Bigr)e_{r}+\Bigl(\frac{\partial_{\theta}u_{0}^{\theta}}{r}+\frac{u_{0}^{r}}{r}-{\mathcal{M}}\bigl(\frac{u_{0}^{r}}{r}\bigr)\Bigr)e_{\theta}+\bigl(\frac{\partial_{\theta}u_{0}^{z}}{r}\bigr)e_{z}.

Then by using Lemma 2.1 and the notation 𝖀0=(θu0r,θu0θ,θu0z),\boldsymbol{\mathfrak{U}}_{0}=(\partial_{\theta}u^{r}_{0},\partial_{\theta}u^{\theta}_{0},\partial_{\theta}u^{z}_{0}), we can obtain

(3.12) 𝒖0𝒖¯0L2𝖀0L2,\|\boldsymbol{u}_{0}-\bar{\boldsymbol{u}}_{0}\|_{L^{2}}\lesssim\|\boldsymbol{\mathfrak{U}}_{0}\|_{L^{2}},
(3.13) (𝒖0𝒖¯0)L2~𝖀0L2+r1𝖀0L2=𝖀0H˙axi1.\|\nabla(\boldsymbol{u}_{0}-\bar{\boldsymbol{u}}_{0})\|_{L^{2}}\lesssim\|\widetilde{\nabla}\boldsymbol{\mathfrak{U}}_{0}\|_{L^{2}}+\|r^{-1}\boldsymbol{\mathfrak{U}}_{0}\|_{L^{2}}=\|\boldsymbol{\mathfrak{U}}_{0}\|_{\dot{H}^{1}_{\rm axi}}.

In view of the estimates (3.10)-(3.13) and the smallness condition (1.10), the condition (2.9) of Propostion 2.1 holds for 𝒖0\boldsymbol{u}_{0} and 𝒗0=𝒖¯0\boldsymbol{v}_{0}=\bar{\boldsymbol{u}}_{0}. Then by using Proposition 2.1 again, (1.4) has a unique global strong solution 𝒖\boldsymbol{u} in C(+;H1)L2(+;H˙1H˙2)C(\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{+};H^{1})\cap L^{2}(\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{+};\dot{H}^{1}\cap\dot{H}^{2}), satisfying

(3.14) 𝒖𝒖¯Lt(L2)2+(𝒖𝒖¯)Lt2(L2)2𝖀0L22exp(exp(C𝒖0L26𝒖0H˙22)),\displaystyle\|\boldsymbol{u}-\bar{\boldsymbol{u}}\|_{L^{\infty}_{t}(L^{2})}^{2}+\|\nabla(\boldsymbol{u}-\bar{\boldsymbol{u}})\|_{L^{2}_{t}(L^{2})}^{2}\lesssim\|\boldsymbol{\mathfrak{U}}_{0}\|_{L^{2}}^{2}\exp\bigl(\exp(C\|{\boldsymbol{u}}_{0}\|_{L^{2}}^{6}\|{\boldsymbol{u}}_{0}\|_{\dot{H}^{2}}^{2})\bigr),
𝒖𝒖¯Lt(H˙1)2+(𝒖𝒖¯)Lt2(H˙1)2𝖀0H˙axi12exp(exp(C𝒖0L26𝒖0H˙22)).\displaystyle\|\boldsymbol{u}-\bar{\boldsymbol{u}}\|_{L^{\infty}_{t}(\dot{H}^{1})}^{2}+\|\nabla(\boldsymbol{u}-\bar{\boldsymbol{u}})\|_{L^{2}_{t}(\dot{H}^{1})}^{2}\lesssim\|\boldsymbol{\mathfrak{U}}_{0}\|_{\dot{H}^{1}_{\rm axi}}^{2}\exp\bigl(\exp(C\|{\boldsymbol{u}}_{0}\|_{L^{2}}^{6}\|{\boldsymbol{u}}_{0}\|_{\dot{H}^{2}}^{2})\bigr).

In particular, the above estimates together with interpolation inequality and the smallness condition (1.10) implies

𝒖𝒖¯Lt(H˙12)2+(𝒖𝒖¯)Lt2(H˙12)2𝖀0L2𝖀0H˙axi1exp(exp(C𝒖0L26𝒖0H˙22))<ϵ,\|\boldsymbol{u}-\bar{\boldsymbol{u}}\|_{L^{\infty}_{t}(\dot{H}^{\frac{1}{2}})}^{2}+\|\nabla(\boldsymbol{u}-\bar{\boldsymbol{u}})\|_{L^{2}_{t}(\dot{H}^{\frac{1}{2}})}^{2}\lesssim\|\boldsymbol{\mathfrak{U}}_{0}\|_{L^{2}}\|\boldsymbol{\mathfrak{U}}_{0}\|_{\dot{H}^{1}_{\rm axi}}\exp\bigl(\exp(C\|{\boldsymbol{u}}_{0}\|_{L^{2}}^{6}\|{\boldsymbol{u}}_{0}\|_{\dot{H}^{2}}^{2})\bigr)<\epsilon,

which means that 𝒖\boldsymbol{u} is indeed close to an axisymmetric solution.

Step 2. Error estimates of uu¯{\mathcal{M}}\boldsymbol{u}-\bar{\boldsymbol{u}}

Step 2.1. Equations for 𝒖𝒖¯{\mathcal{M}}\boldsymbol{u}-\bar{\boldsymbol{u}}. We first get, by applying {\mathcal{M}} to (1.4) that

(3.15) {tur+((urr+uθθr+uzz)ur)(Δ1r2)ur(|uθ|2r)+rP=0,tuθ+((urr+uθθr+uzz)uθ)(Δ1r2)uθ+(uruθr)=0,tuz+((urr+uθθr+uzz)uz)Δuz+zP=0,rur+urr+zuz=0,𝒖|t=0=𝒖0,\left\{\begin{aligned} &\partial_{t}{\mathcal{M}}u^{r}+{\mathcal{M}}\Bigl((u^{r}\partial_{r}+u^{\theta}\frac{\partial_{\theta}}{r}+u^{z}\partial_{z})u^{r}\Bigr)\\ &\qquad\qquad\qquad\qquad-\bigl(\Delta-\frac{1}{r^{2}}\bigr){\mathcal{M}}u^{r}-{\mathcal{M}}\Bigl(\frac{|u^{\theta}|^{2}}{r}\Bigr)+\partial_{r}{\mathcal{M}}P=0,\\ &\partial_{t}{\mathcal{M}}u^{\theta}+{\mathcal{M}}\Bigl((u^{r}\partial_{r}+u^{\theta}\frac{\partial_{\theta}}{r}+u^{z}\partial_{z})u^{\theta}\Bigr)-\bigl(\Delta-\frac{1}{r^{2}}\bigr){\mathcal{M}}u^{\theta}+{\mathcal{M}}\Bigl(\frac{u^{r}u^{\theta}}{r}\Bigr)=0,\\ &\partial_{t}{\mathcal{M}}u^{z}+{\mathcal{M}}\Bigl((u^{r}\partial_{r}+u^{\theta}\frac{\partial_{\theta}}{r}+u^{z}\partial_{z})u^{z}\Bigr)-\Delta{\mathcal{M}}u^{z}+\partial_{z}{\mathcal{M}}P=0,\\ &\partial_{r}{\mathcal{M}}u^{r}+\frac{{\mathcal{M}}u^{r}}{r}+\partial_{z}{\mathcal{M}}u^{z}=0,\\ &{\mathcal{M}}{\boldsymbol{u}}|_{t=0}={\mathcal{M}}{\boldsymbol{u}_{0}},\end{aligned}\right.

where we have used the fact that for any regular enough function ff, there holds

02πθf(r,θ,z)𝑑θ=0.\int_{0}^{2\pi}\partial_{\theta}f(r,\theta,z)\,d\theta=0.

Then by denoting 𝒗=def𝒖𝒖¯,Q=defPP¯\boldsymbol{v}\mathrel{\mathop{\kern 0.0pt=}\limits^{\hbox{\footnotesize def}}}{\mathcal{M}}\boldsymbol{u}-\bar{\boldsymbol{u}},\,Q\mathrel{\mathop{\kern 0.0pt=}\limits^{\hbox{\footnotesize def}}}{\mathcal{M}}P-\bar{P}, and in view of (1.6) and (3.15), we deduce

(3.16) {t𝒗Δ𝒗+Q=𝑭+𝑮,div𝒗=0,𝒗|t=0=0,\left\{\begin{aligned} &\partial_{t}\boldsymbol{v}-\Delta\boldsymbol{v}+\nabla Q=\boldsymbol{F}+\boldsymbol{G},\quad\mathop{\rm div}\nolimits\boldsymbol{v}=0,\\ &\boldsymbol{v}|_{t=0}=0,\end{aligned}\right.

where 𝑭=Fr𝒆r+Fθ𝒆θ+Fz𝒆z,𝑮=Gr𝒆r+Gθ𝒆θ+Gz𝒆z\boldsymbol{F}=F^{r}\boldsymbol{e}_{r}+F^{\theta}\boldsymbol{e}_{\theta}+F^{z}\boldsymbol{e}_{z},~\boldsymbol{G}=G^{r}\boldsymbol{e}_{r}+G^{\theta}\boldsymbol{e}_{\theta}+G^{z}\boldsymbol{e}_{z} with

Fr=(u¯rr+u¯zz)u¯r((urr+uzz)ur),Gr=u¯θ(θu¯rru¯θr)(uθ(θurruθr)),\displaystyle F^{r}=(\bar{u}^{r}\partial_{r}+\bar{u}^{z}\partial_{z})\bar{u}^{r}-{\mathcal{M}}\Bigl((u^{r}\partial_{r}+u^{z}\partial_{z})u^{r}\Bigr),~G^{r}=\bar{u}^{\theta}\bigl(\frac{\partial_{\theta}\bar{u}^{r}}{r}-\frac{\bar{u}^{\theta}}{r}\bigr)-{\mathcal{M}}\Bigl(u^{\theta}\bigl(\frac{\partial_{\theta}u^{r}}{r}-\frac{u^{\theta}}{r}\bigr)\Bigr),
Fθ=(u¯rr+u¯zz)u¯θ((urr+uzz)uθ),Gθ=u¯θ(θu¯θr+u¯rr)(uθ(θuθr+urr)),\displaystyle F^{\theta}=(\bar{u}^{r}\partial_{r}+\bar{u}^{z}\partial_{z})\bar{u}^{\theta}-{\mathcal{M}}\Bigl((u^{r}\partial_{r}+u^{z}\partial_{z})u^{\theta}\Bigr),~G^{\theta}=\bar{u}^{\theta}\bigl(\frac{\partial_{\theta}\bar{u}^{\theta}}{r}+\frac{\bar{u}^{r}}{r}\bigr)-{\mathcal{M}}\Bigl(u^{\theta}\bigl(\frac{\partial_{\theta}u^{\theta}}{r}+\frac{u^{r}}{r}\bigr)\Bigr),
Fz=(u¯rr+u¯zz)u¯z((urr+uzz)uz),Gz=(uθθuzr).\displaystyle F^{z}=(\bar{u}^{r}\partial_{r}+\bar{u}^{z}\partial_{z})\bar{u}^{z}-{\mathcal{M}}\Bigl((u^{r}\partial_{r}+u^{z}\partial_{z})u^{z}\Bigr),~G^{z}=-{\mathcal{M}}\Bigl(\frac{u^{\theta}\partial_{\theta}u^{z}}{r}\Bigr).

We mention that here θu¯r,θu¯θ\partial_{\theta}\bar{u}^{r},\,\partial_{\theta}\bar{u}^{\theta} indeed vanishes, but we still write them to derive a symmetric form. In this way, we can handle these terms by using the following key observation: for any functions f,gf,\,g and any axisymmetric functions f¯,g¯\bar{f},\,\bar{g}, there holds

(3.17) (fg)f¯g¯=(fgf¯g¯)=((ff¯)(gg¯)+(ff¯)g¯+f¯(gg¯))=((ff¯)(gg¯))+g¯(ff¯)+f¯(gg¯).\begin{split}{\mathcal{M}}(fg)-\bar{f}\bar{g}&={\mathcal{M}}(fg-\bar{f}\bar{g})\\ &={\mathcal{M}}\bigl((f-\bar{f})(g-\bar{g})+(f-\bar{f})\bar{g}+\bar{f}(g-\bar{g})\bigr)\\ &={\mathcal{M}}\bigl((f-\bar{f})(g-\bar{g})\bigr)+\bar{g}{\mathcal{M}}(f-\bar{f})+\bar{f}{\mathcal{M}}(g-\bar{g}).\end{split}

On the other hand, noting that f¯,g¯\bar{f},\,\bar{g} are axisymmetric, we have

θg=θ(gg¯),and(f¯θ(gg¯))=f¯(θ(gg¯))=0.\partial_{\theta}g=\partial_{\theta}(g-\bar{g}),\quad\hbox{and}\quad{\mathcal{M}}\bigl(\bar{f}\partial_{\theta}(g-\bar{g})\bigr)=\bar{f}{\mathcal{M}}\bigl(\partial_{\theta}(g-\bar{g})\bigr)=0.

As a result, there holds

(3.18) (fθg)=(fθ(gg¯))=((ff¯)θ(gg¯)).{\mathcal{M}}(f\partial_{\theta}g)={\mathcal{M}}\bigl(f\partial_{\theta}(g-\bar{g})\bigr)={\mathcal{M}}\bigl((f-\bar{f})\partial_{\theta}(g-\bar{g})\bigr).

For notation simplification, let us introduce 𝑽=𝒖𝒖¯\boldsymbol{V}=\boldsymbol{u}-\bar{\boldsymbol{u}}. Obviously there holds

𝑽=𝒖𝒖¯=𝒖𝒖¯=𝒗.{\mathcal{M}}\boldsymbol{V}={\mathcal{M}}\boldsymbol{u}-{\mathcal{M}}\bar{\boldsymbol{u}}={\mathcal{M}}\boldsymbol{u}-\bar{\boldsymbol{u}}=\boldsymbol{v}.

Then by using (3.17), we have

(urrur)u¯rru¯r=(VrrVr)+vrru¯r+u¯rrvr.\displaystyle{\mathcal{M}}(u^{r}\partial_{r}u^{r})-\bar{u}^{r}\partial_{r}\bar{u}^{r}={\mathcal{M}}(V^{r}\partial_{r}V^{r})+v^{r}\partial_{r}\bar{u}^{r}+\bar{u}^{r}\partial_{r}v^{r}.

Similar formulas hold for the other terms in Fr,Fθ,FzF^{r},\,F^{\theta},\,F^{z}. And we can write

(3.19) Fr=((Vrr+Vzz)Vr)(vrr+vzz)u¯r(u¯rr+u¯zz)vr,\displaystyle F^{r}=-{\mathcal{M}}\Bigl((V^{r}\partial_{r}+V^{z}\partial_{z})V^{r}\Bigr)-(v^{r}\partial_{r}+v^{z}\partial_{z})\bar{u}^{r}-(\bar{u}^{r}\partial_{r}+\bar{u}^{z}\partial_{z})v^{r},
Fθ=((Vrr+Vzz)Vθ)(vrr+vzz)u¯θ(u¯rr+u¯zz)vθ,\displaystyle F^{\theta}=-{\mathcal{M}}\Bigl((V^{r}\partial_{r}+V^{z}\partial_{z})V^{\theta}\Bigr)-(v^{r}\partial_{r}+v^{z}\partial_{z})\bar{u}^{\theta}-(\bar{u}^{r}\partial_{r}+\bar{u}^{z}\partial_{z})v^{\theta},
Fz=((Vrr+Vzz)Vz)(vrr+vzz)u¯z(u¯rr+u¯zz)vz.\displaystyle F^{z}=-{\mathcal{M}}\Bigl((V^{r}\partial_{r}+V^{z}\partial_{z})V^{z}\Bigr)-(v^{r}\partial_{r}+v^{z}\partial_{z})\bar{u}^{z}-(\bar{u}^{r}\partial_{r}+\bar{u}^{z}\partial_{z})v^{z}.

Exactly along the same line, by using (3.17), we have

Gr\displaystyle G^{r} =(Vθ(θVrrVθr))u¯θ(θVrrVθr)(θu¯rru¯θr)(Vθ)\displaystyle=-{\mathcal{M}}\Bigl(V^{\theta}\bigl(\frac{\partial_{\theta}V^{r}}{r}-\frac{V^{\theta}}{r}\bigr)\Bigr)-\bar{u}^{\theta}{\mathcal{M}}\Bigl(\frac{\partial_{\theta}V^{r}}{r}-\frac{V^{\theta}}{r}\Bigr)-\bigl(\frac{\partial_{\theta}\bar{u}^{r}}{r}-\frac{\bar{u}^{\theta}}{r}\bigr){\mathcal{M}}(V^{\theta})
=(Vθ(θVrrVθr))+2u¯θrvθ,\displaystyle=-{\mathcal{M}}\Bigl(V^{\theta}\bigl(\frac{\partial_{\theta}V^{r}}{r}-\frac{V^{\theta}}{r}\bigr)\Bigr)+2\frac{\bar{u}^{\theta}}{r}v^{\theta},

and

Gθ=(Vθ(θVθr+Vrr))u¯θrvru¯rrvθ.G^{\theta}=-{\mathcal{M}}\Bigl(V^{\theta}\bigl(\frac{\partial_{\theta}V^{\theta}}{r}+\frac{V^{r}}{r}\bigr)\Bigr)-\frac{\bar{u}^{\theta}}{r}v^{r}-\frac{\bar{u}^{r}}{r}v^{\theta}.

Notice that

θ𝑽r=(θVrrVθr)𝒆r+(θVθr+Vrr)𝒆θ+θVzr𝒆z,\frac{\partial_{\theta}\boldsymbol{V}}{r}=(\frac{\partial_{\theta}V^{r}}{r}-\frac{V^{\theta}}{r})\boldsymbol{e}_{r}+(\frac{\partial_{\theta}V^{\theta}}{r}+\frac{V^{r}}{r})\boldsymbol{e}_{\theta}+\frac{\partial_{\theta}V^{z}}{r}\boldsymbol{e}_{z},

thus we can write

(3.20) Gr=(Vθ(θ𝑽r𝒆r))+2u¯θrvθ,andGθ=(Vθ(θ𝑽r𝒆θ))u¯θrvru¯rrvθ.G^{r}=-{\mathcal{M}}\Bigl(V^{\theta}\bigl(\frac{\partial_{\theta}\boldsymbol{V}}{r}\cdot\boldsymbol{e}_{r}\bigr)\Bigr)+2\frac{\bar{u}^{\theta}}{r}v^{\theta},\quad\hbox{and}\quad G^{\theta}=-{\mathcal{M}}\Bigl(V^{\theta}\bigl(\frac{\partial_{\theta}\boldsymbol{V}}{r}\cdot\boldsymbol{e}_{\theta}\bigr)\Bigr)-\frac{\bar{u}^{\theta}}{r}v^{r}-\frac{\bar{u}^{r}}{r}v^{\theta}.

On the other hand, by using (3.18), we have

(3.21) Gz=(VθθVzr)=(Vθ(θ𝑽r𝒆z)).G^{z}=-{\mathcal{M}}\Bigl(V^{\theta}\frac{\partial_{\theta}V^{z}}{r}\Bigr)=-{\mathcal{M}}\Bigl(V^{\theta}\bigl(\frac{\partial_{\theta}\boldsymbol{V}}{r}\cdot\boldsymbol{e}_{z}\bigr)\Bigr).

Step 2.2. L2L^{2}-estimate for 𝒗\boldsymbol{v}. Taking L2L^{2} inner product of (3.16) with 𝒗\boldsymbol{v} gives rise to

(3.22) 12ddt𝒗L22+𝒗L22=(𝑭|𝒗)+(𝑮|𝒗).\frac{1}{2}\frac{d}{dt}\|\boldsymbol{v}\|_{L^{2}}^{2}+\|\nabla\boldsymbol{v}\|_{L^{2}}^{2}=(\boldsymbol{F}\,|\,\boldsymbol{v})+(\boldsymbol{G}\,|\,\boldsymbol{v}).

Thanks to the formula (3.19) and Lemma 2.1, we obtain

|(𝑭|𝒗)|𝑽L3𝑽L2𝒗L6+𝒗L3𝒖¯L2𝒗L6+𝒖¯L6𝒗L2𝒗L3𝑽L212𝑽L232𝒗L2+𝒖¯L2𝒗L212𝒗L232,\displaystyle\begin{aligned} |(\boldsymbol{F}\,|\,\boldsymbol{v})|&\lesssim\|\boldsymbol{V}\|_{L^{3}}\|{\nabla}\boldsymbol{V}\|_{L^{2}}\|\boldsymbol{v}\|_{L^{6}}+\|\boldsymbol{v}\|_{L^{3}}\|{\nabla}\bar{\boldsymbol{u}}\|_{L^{2}}\|\boldsymbol{v}\|_{L^{6}}+\|\bar{\boldsymbol{u}}\|_{L^{6}}\|{\nabla}\boldsymbol{v}\|_{L^{2}}\|\boldsymbol{v}\|_{L^{3}}\\ &\lesssim\|\boldsymbol{V}\|_{L^{2}}^{\frac{1}{2}}\|\nabla\boldsymbol{V}\|_{L^{2}}^{\frac{3}{2}}\|\nabla\boldsymbol{v}\|_{L^{2}}+\|\nabla\bar{\boldsymbol{u}}\|_{L^{2}}\|\boldsymbol{v}\|_{L^{2}}^{\frac{1}{2}}\|\nabla\boldsymbol{v}\|_{L^{2}}^{\frac{3}{2}},\end{aligned}

which along with Young’s inequality implies

(3.23) |(𝑭|𝒗)|14𝒗L22+C𝑽L2𝑽L23+𝒖¯L24𝒗L22.|(\boldsymbol{F}\,|\,\boldsymbol{v})|\leq\frac{1}{4}\|\nabla\boldsymbol{v}\|_{L^{2}}^{2}+C\|\boldsymbol{V}\|_{L^{2}}\|\nabla\boldsymbol{V}\|_{L^{2}}^{3}+\|\nabla\bar{\boldsymbol{u}}\|_{L^{2}}^{4}\|\boldsymbol{v}\|_{L^{2}}^{2}.

While by virtue of (3.20), (3.21), Lemma 2.1 and Lemma 2.3, we get

|(𝑮|𝒗)|\displaystyle|(\boldsymbol{G}\,|\,\boldsymbol{v})| VθL3θ𝑽rL2𝒗L6+𝒗L3(u¯rrL2+u¯θrL2)𝒗L6\displaystyle\lesssim\|V^{\theta}\|_{L^{3}}\bigl\|\frac{\partial_{\theta}\boldsymbol{V}}{r}\bigr\|_{L^{2}}\|\boldsymbol{v}\|_{L^{6}}+\|\boldsymbol{v}\|_{L^{3}}\bigl(\bigl\|\frac{\bar{u}^{r}}{r}\bigr\|_{L^{2}}+\bigl\|\frac{\bar{u}^{\theta}}{r}\bigr\|_{L^{2}}\bigr)\|\boldsymbol{v}\|_{L^{6}}
𝑽L212𝑽L232𝒗L2+𝒗L212𝒗L232𝒖¯L2.\displaystyle\lesssim\|\boldsymbol{V}\|_{L^{2}}^{\frac{1}{2}}\|\nabla\boldsymbol{V}\|_{L^{2}}^{\frac{3}{2}}\|\nabla\boldsymbol{v}\|_{L^{2}}+\|\boldsymbol{v}\|_{L^{2}}^{\frac{1}{2}}\|\nabla\boldsymbol{v}\|_{L^{2}}^{\frac{3}{2}}\|\nabla\bar{\boldsymbol{u}}\|_{L^{2}}.

Then by using Young’s inequality, we deduce

(3.24) |(𝑮|𝒗)|14𝒗L22+C𝑽L2𝑽L23+C𝒗L22𝒖¯L24.|(\boldsymbol{G}\,|\,\boldsymbol{v})|\leq\frac{1}{4}\|\nabla\boldsymbol{v}\|_{L^{2}}^{2}+C\|\boldsymbol{V}\|_{L^{2}}\|\nabla\boldsymbol{V}\|_{L^{2}}^{3}+C\|\boldsymbol{v}\|_{L^{2}}^{2}\|\nabla\bar{\boldsymbol{u}}\|_{L^{2}}^{4}.

Now by substituting (3.23) and (3.24) into (3.22), we obtain

ddt𝒗L22+𝒗L22C𝑽L2𝑽L23+C𝒗L22𝒖¯L24.\displaystyle\frac{d}{dt}\|\boldsymbol{v}\|_{L^{2}}^{2}+\|\nabla\boldsymbol{v}\|_{L^{2}}^{2}\leq C\|\boldsymbol{V}\|_{L^{2}}\|\nabla\boldsymbol{V}\|_{L^{2}}^{3}+C\|\boldsymbol{v}\|_{L^{2}}^{2}\|\nabla\bar{\boldsymbol{u}}\|_{L^{2}}^{4}.

Then by using Gronwall’s inequality and the fact that 𝒗|t=0=0\boldsymbol{v}|_{t=0}=0, we achieve

𝒗Lt(L2)2+𝒗Lt2(L2)2𝑽Lt(L2)𝑽Lt(L2)𝑽Lt2(L2)2exp(C𝒖¯Lt(L2)2𝒖¯Lt2(L2)2).\|\boldsymbol{v}\|_{L^{\infty}_{t}(L^{2})}^{2}+\|\nabla\boldsymbol{v}\|_{L^{2}_{t}(L^{2})}^{2}\lesssim\|\boldsymbol{V}\|_{L^{\infty}_{t}(L^{2})}\|\nabla\boldsymbol{V}\|_{L^{\infty}_{t}(L^{2})}\|\nabla\boldsymbol{V}\|_{L^{2}_{t}(L^{2})}^{2}\exp\bigl(C\|\nabla\bar{\boldsymbol{u}}\|_{L^{\infty}_{t}(L^{2})}^{2}\|\nabla\bar{\boldsymbol{u}}\|_{L^{2}_{t}(L^{2})}^{2}\bigr).

Recall that 𝑽=𝒖𝒖¯\boldsymbol{V}=\boldsymbol{u}-\bar{\boldsymbol{u}}, by using (3.10), (3.11) and (3.14), we obtain

(3.25) 𝒗Lt(L2)2+𝒗Lt2(L2)2𝖀0L23𝖀0H˙axi1exp(exp(C𝒖0L26𝒖0H˙22)).\|\boldsymbol{v}\|_{L^{\infty}_{t}(L^{2})}^{2}+\|\boldsymbol{v}\|_{L^{2}_{t}(L^{2})}^{2}\lesssim\|\boldsymbol{\mathfrak{U}}_{0}\|_{L^{2}}^{3}\|\boldsymbol{\mathfrak{U}}_{0}\|_{\dot{H}^{1}_{\rm axi}}\exp\bigl(\exp(C\|{\boldsymbol{u}}_{0}\|_{L^{2}}^{6}\|{\boldsymbol{u}}_{0}\|_{\dot{H}^{2}}^{2})\bigr).

This together with the smallness assumption (1.10) gives

𝒗Lt(L2)2+𝒗Lt2(L2)2ϵ𝖀0L22exp(exp(C𝒖0L26𝒖0H˙22)),\|\boldsymbol{v}\|_{L^{\infty}_{t}(L^{2})}^{2}+\|\boldsymbol{v}\|_{L^{2}_{t}(L^{2})}^{2}\lesssim\epsilon\|\boldsymbol{\mathfrak{U}}_{0}\|_{L^{2}}^{2}\exp\bigl(\exp(C\|{\boldsymbol{u}}_{0}\|_{L^{2}}^{6}\|{\boldsymbol{u}}_{0}\|_{\dot{H}^{2}}^{2})\bigr),

which is exactly the first inequality of (1.12).

Step 2.3. H˙1\dot{H}^{1}-estimate for 𝒗\boldsymbol{v}. Taking L2L^{2} inner product of (3.16) with Δ𝒗-\Delta\boldsymbol{v} gives rise to

(3.26) 12ddt𝒗L22+Δ𝒗L22=(𝑭|Δ𝒗)(𝑮|Δ𝒗)(𝑭L2+𝑮L2)Δ𝒗L2.\begin{split}\frac{1}{2}\frac{d}{dt}\|\nabla\boldsymbol{v}\|_{L^{2}}^{2}+\|\Delta\boldsymbol{v}\|_{L^{2}}^{2}&=-(\boldsymbol{F}\,|\,\Delta\boldsymbol{v})-(\boldsymbol{G}\,|\,\Delta\boldsymbol{v})\\ &\leq\bigl(\|\boldsymbol{F}\|_{L^{2}}+\|\boldsymbol{G}\|_{L^{2}}\bigr)\|\Delta\boldsymbol{v}\|_{L^{2}}.\end{split}

In view of the formulas (3.19)-(3.21), we can use Lemmas 2.1 and 2.3 to get

𝑭L2+𝑮L2\displaystyle\|\boldsymbol{F}\|_{L^{2}}+\|\boldsymbol{G}\|_{L^{2}}\lesssim 𝑽L(~𝑽L2+θ𝑽rL2)\displaystyle\|\boldsymbol{V}\|_{L^{\infty}}\bigl(\|\widetilde{\nabla}\boldsymbol{V}\|_{L^{2}}+\bigl\|\frac{\partial_{\theta}\boldsymbol{V}}{r}\bigr\|_{L^{2}}\bigr)
+𝒗L(~𝒖¯L2+u¯rrL2+u¯θrL2)+𝒖¯L~𝒗L2\displaystyle+\|\boldsymbol{v}\|_{L^{\infty}}\bigl(\|\widetilde{\nabla}\bar{\boldsymbol{u}}\|_{L^{2}}+\bigl\|\frac{\bar{u}^{r}}{r}\bigr\|_{L^{2}}+\bigl\|\frac{\bar{u}^{\theta}}{r}\bigr\|_{L^{2}}\bigr)+\|\bar{\boldsymbol{u}}\|_{L^{\infty}}\|\widetilde{\nabla}\boldsymbol{v}\|_{L^{2}}
\displaystyle\lesssim 𝑽L𝑽L2+𝒗L𝒖¯L2+𝒖¯L𝒗L2\displaystyle\|\boldsymbol{V}\|_{L^{\infty}}\|\nabla\boldsymbol{V}\|_{L^{2}}+\|\boldsymbol{v}\|_{L^{\infty}}\|\nabla\bar{\boldsymbol{u}}\|_{L^{2}}+\|\bar{\boldsymbol{u}}\|_{L^{\infty}}\|\nabla\boldsymbol{v}\|_{L^{2}}
\displaystyle\lesssim 𝑽L232Δ𝑽L212+𝒗L212Δ𝒗L212𝒖¯L2+𝒖¯L212Δ𝒖¯L212𝒗L2,\displaystyle\|\nabla\boldsymbol{V}\|_{L^{2}}^{\frac{3}{2}}\|\Delta\boldsymbol{V}\|_{L^{2}}^{\frac{1}{2}}+\|\nabla\boldsymbol{v}\|_{L^{2}}^{\frac{1}{2}}\|\Delta\boldsymbol{v}\|_{L^{2}}^{\frac{1}{2}}\|\nabla\bar{\boldsymbol{u}}\|_{L^{2}}+\|\nabla\bar{\boldsymbol{u}}\|_{L^{2}}^{\frac{1}{2}}\|\Delta\bar{\boldsymbol{u}}\|_{L^{2}}^{\frac{1}{2}}\|\nabla\boldsymbol{v}\|_{L^{2}},

which together with Young’s inequality leads to

(𝑭L2+CLOSE\displaystyle\bigl(\|\boldsymbol{F}\|_{L^{2}}+ OPEN𝑮L2)Δ𝒗L2\displaystyle\|\boldsymbol{G}\|_{L^{2}}\bigr)\|\Delta\boldsymbol{v}\|_{L^{2}}
12Δ𝒗L22+C𝑽L23Δ𝑽L2+C(𝒖¯L24+𝒖¯L2Δ𝒖¯L2)𝒗L22.\displaystyle\leq\frac{1}{2}\|\Delta\boldsymbol{v}\|_{L^{2}}^{2}+C\|\nabla\boldsymbol{V}\|_{L^{2}}^{3}\|\Delta\boldsymbol{V}\|_{L^{2}}+C\bigl(\|\nabla\bar{\boldsymbol{u}}\|_{L^{2}}^{4}+\|\nabla\bar{\boldsymbol{u}}\|_{L^{2}}\|\Delta\bar{\boldsymbol{u}}\|_{L^{2}}\bigr)\|\nabla\boldsymbol{v}\|_{L^{2}}^{2}.

By substituting this into (3.26), we infer

ddt𝒗L22+Δ𝒗L22𝑽L23Δ𝑽L2+(𝒖¯L24+𝒖¯L2Δ𝒖¯L2)𝒗L22,\displaystyle\frac{d}{dt}\|\nabla\boldsymbol{v}\|_{L^{2}}^{2}+\|\Delta\boldsymbol{v}\|_{L^{2}}^{2}\lesssim\|\nabla\boldsymbol{V}\|_{L^{2}}^{3}\|\Delta\boldsymbol{V}\|_{L^{2}}+\bigl(\|\nabla\bar{\boldsymbol{u}}\|_{L^{2}}^{4}+\|\nabla\bar{\boldsymbol{u}}\|_{L^{2}}\|\Delta\bar{\boldsymbol{u}}\|_{L^{2}}\bigr)\|\nabla\boldsymbol{v}\|_{L^{2}}^{2},

Then by applying Gronwall’s inequality and using the fact that 𝒗|t=0=0\boldsymbol{v}|_{t=0}=0, we deduce

𝒗Lt(L2)2+Δ𝒗Lt2(L2)2\displaystyle\|\nabla\boldsymbol{v}\|_{L^{\infty}_{t}(L^{2})}^{2}+\|\Delta\boldsymbol{v}\|_{L^{2}_{t}(L^{2})}^{2}\leq C𝑽Lt(L2)2𝑽Lt2(L2)Δ𝑽Lt2(L2)\displaystyle C\|\nabla\boldsymbol{V}\|_{L^{\infty}_{t}(L^{2})}^{2}\|\nabla\boldsymbol{V}\|_{L^{2}_{t}(L^{2})}\|\Delta\boldsymbol{V}\|_{L^{2}_{t}(L^{2})}
×exp(C𝒖¯Lt(L2)2𝒖¯Lt2(L2)2+C𝒖¯Lt2(L2)Δ𝒖¯Lt2(L2)).\displaystyle\times\exp\bigl(C\|\nabla\bar{\boldsymbol{u}}\|_{L^{\infty}_{t}(L^{2})}^{2}\|\nabla\bar{\boldsymbol{u}}\|_{L^{2}_{t}(L^{2})}^{2}+C\|\nabla\bar{\boldsymbol{u}}\|_{L^{2}_{t}(L^{2})}\|\Delta\bar{\boldsymbol{u}}\|_{L^{2}_{t}(L^{2})}\bigr).

Notice that 𝑽=𝒖𝒖¯\boldsymbol{V}=\boldsymbol{u}-\bar{\boldsymbol{u}}, then we can use (3.10), (3.11) and (3.14) to obtain

(3.27) 𝒗Lt(L2)2+Δ𝒗Lt2(L2)2𝖀0L2𝖀0H˙axi13exp(exp(C𝒖0L26𝒖0H˙22)).\|\nabla\boldsymbol{v}\|_{L^{\infty}_{t}(L^{2})}^{2}+\|\Delta\boldsymbol{v}\|_{L^{2}_{t}(L^{2})}^{2}\lesssim\|\boldsymbol{\mathfrak{U}}_{0}\|_{L^{2}}\|\boldsymbol{\mathfrak{U}}_{0}\|_{\dot{H}^{1}_{\rm axi}}^{3}\exp\bigl(\exp(C\|{\boldsymbol{u}}_{0}\|_{L^{2}}^{6}\|{\boldsymbol{u}}_{0}\|_{\dot{H}^{2}}^{2})\bigr).

This together with the smallness assumption (1.10) gives

𝒗Lt(L2)2+Δ𝒗Lt2(L2)2ϵ𝖀0H˙axi12exp(exp(C𝒖0L26𝒖0H˙22)),\|\nabla\boldsymbol{v}\|_{L^{\infty}_{t}(L^{2})}^{2}+\|\Delta\boldsymbol{v}\|_{L^{2}_{t}(L^{2})}^{2}\lesssim\epsilon\|\boldsymbol{\mathfrak{U}}_{0}\|_{\dot{H}^{1}_{\rm axi}}^{2}\exp\bigl(\exp(C\|{\boldsymbol{u}}_{0}\|_{L^{2}}^{6}\|{\boldsymbol{u}}_{0}\|_{\dot{H}^{2}}^{2})\bigr),

which is exactly the second inequality of (1.12).

Till now, we have completed the proof of Theorem 1.1. ∎

4. The proof of Theorem 1.2

As we have mentioned in Subsection 1.2, for any initial data given by (1.13), Theorem 1.1 guarantees the existence of some positive constant ε0\varepsilon_{0} such that for any ε(0,ε0)\varepsilon\in(0,\varepsilon_{0}), (1.1) has a unique global solution 𝒖C(+;H1)L2(+;H˙1H˙2)\boldsymbol{u}\in C(\mathop{\mathbb{R}\kern 0.0pt}\nolimits_{+};H^{1})\cap L^{2}(\mathop{\mathbb{R}\kern 0.0pt}\nolimits_{+};\dot{H}^{1}\cap\dot{H}^{2}).

By virtue of the classical result that any strong solution to N-S will become analytic at positive time, hence we can expand this solution into Fourier series in θ\theta variable as

(4.1) {ur(t,x)=(u(0),0r+εu(1),0r)(t,r,z)+k=1(u(0),kr+εu(1),kr)(t,r,z)coskθ+k=1(vr(0),k+εvr(1),k)(t,r,z)sinkθ+𝒪(ε2),uθ(t,x)=(u(0),0θ+εu(1),0θ)(t,r,z)+k=1(u(0),kθ+εu(1),kθ)(t,r,z)coskθ+k=1(vθ(0),k+εvθ(1),k)(t,r,z)sinkθ+𝒪(ε2),uz(t,x)=(u(0),0z+εu(1),0z)(t,r,z)+k=1(u(0),kz+εu(1),kz)(t,r,z)coskθ+k=1(vz(0),k+εvz(1),k)(t,r,z)sinkθ+𝒪(ε2).\left\{\begin{split}u^{r}(t,x)=&\bigl(u^{r}_{(0),0}+\varepsilon u^{r}_{(1),0}\bigr)(t,r,z)+\sum_{k=1}^{\infty}\bigl(u^{r}_{(0),k}+\varepsilon u^{r}_{(1),k}\bigr)(t,r,z)\cos k\theta\\ &+\sum_{k=1}^{\infty}\bigl(v^{r}_{(0),k}+\varepsilon v^{r}_{(1),k}\bigr)(t,r,z)\sin k\theta+{\mathcal{O}}(\varepsilon^{2}),\\ u^{\theta}(t,x)=&\bigl(u^{\theta}_{(0),0}+\varepsilon u^{\theta}_{(1),0}\bigr)(t,r,z)+\sum_{k=1}^{\infty}\bigl(u^{\theta}_{(0),k}+\varepsilon u^{\theta}_{(1),k}\bigr)(t,r,z)\cos k\theta\\ &+\sum_{k=1}^{\infty}\bigl(v^{\theta}_{(0),k}+\varepsilon v^{\theta}_{(1),k}\bigr)(t,r,z)\sin k\theta+{\mathcal{O}}(\varepsilon^{2}),\\ u^{z}(t,x)=&\bigl(u^{z}_{(0),0}+\varepsilon u^{z}_{(1),0}\bigr)(t,r,z)+\sum_{k=1}^{\infty}\bigl(u^{z}_{(0),k}+\varepsilon u^{z}_{(1),k}\bigr)(t,r,z)\cos k\theta\\ &+\sum_{k=1}^{\infty}\bigl(v^{z}_{(0),k}+\varepsilon v^{z}_{(1),k}\bigr)(t,r,z)\sin k\theta+{\mathcal{O}}(\varepsilon^{2}).\end{split}\right.

Correspondingly, we can expand the pressure P=(Δ)1divdiv(𝒖𝒖)P=(-\Delta)^{-1}\mathop{\rm div}\nolimits\mathop{\rm div}\nolimits(\boldsymbol{u}\otimes\boldsymbol{u}) into

(4.2) P(t,x)=(P(0),0+εP(1),0)(t,r,z)+k=1(P(0),k+εP(1),k)(t,r,z)coskθ+k=1(Q(0),k+εQ(1),k)(t,r,z)sinkθ+𝒪(ε2).\begin{split}P(t,x)=&\bigl(P_{(0),0}+\varepsilon P_{(1),0}\bigr)(t,r,z)+\sum_{k=1}^{\infty}\bigl(P_{(0),k}+\varepsilon P_{(1),k}\bigr)(t,r,z)\cos k\theta\\ &+\sum_{k=1}^{\infty}\bigl(Q_{(0),k}+\varepsilon Q_{(1),k}\bigr)(t,r,z)\sin k\theta+{\mathcal{O}}(\varepsilon^{2}).\end{split}

In the following, we shall give the explicit formulas for the profiles in the expansion (4.1), and verify the validity of this expansion in L(+;L2L)L^{\infty}(\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{+};L^{2}\cap L^{\infty}) sense. For notation simplification, we shall use 𝒖(i)\boldsymbol{u}_{(i)} to denote the εi\varepsilon^{i} order term in the expansion of 𝒖\boldsymbol{u}, i.e.

(4.3) 𝒖=𝒖(0)+ε𝒖(1)+𝒪(ε2),𝒖(i)=𝒖(i),0+k=1(𝒖(i),kcoskθ+𝒗(i),ksinkθ),\boldsymbol{u}=\boldsymbol{u}_{(0)}+\varepsilon\boldsymbol{u}_{(1)}+{\mathcal{O}}(\varepsilon^{2}),\quad\boldsymbol{u}_{(i)}=\boldsymbol{u}_{(i),0}+\sum_{k=1}^{\infty}\Bigl(\boldsymbol{u}_{(i),k}\cos k\theta+\boldsymbol{v}_{(i),k}\sin k\theta\Bigr),

and 𝒖(i)\boldsymbol{u}_{(i)} does not rely on ε\varepsilon.

4.1. The ε0\varepsilon^{0} order terms

We make the following Ansatz 11: 𝒖(0)=u(0),0r𝒆r+u(0),0z𝒆z\boldsymbol{u}_{(0)}=u^{r}_{(0),0}\boldsymbol{e}_{r}+u^{z}_{(0),0}\boldsymbol{e}_{z}, where u(0),0ru^{r}_{(0),0} and u(0),0zu^{z}_{(0),0} satisfy the following axisymmetric without swirl N-S:

(4.4) {tur(0),0+(ur(0),0r+uz(0),0z)ur(0),0(r2+z2+1rr1r2)ur(0),0+rP(0),0=0,tuz(0),0+(ur(0),0r+uz(0),0z)uz(0),0(r2+z2+1rr)uz(0),0+zP(0),0=0,ru(0),0r+1ru(0),0r+zu(0),0z=0,ur(0),0|t=0=ar0,uz(0),0|t=0=az0.\left\{\begin{split}&\partial_{t}u^{r}_{(0),0}+(u^{r}_{(0),0}\partial_{r}+u^{z}_{(0),0}\partial_{z})u^{r}_{(0),0}-(\partial_{r}^{2}+\partial_{z}^{2}+\frac{1}{r}\partial_{r}-\frac{1}{r^{2}})u^{r}_{(0),0}+\partial_{r}P_{(0),0}=0,\\ &\partial_{t}u^{z}_{(0),0}+(u^{r}_{(0),0}\partial_{r}+u^{z}_{(0),0}\partial_{z})u^{z}_{(0),0}-(\partial_{r}^{2}+\partial_{z}^{2}+\frac{1}{r}\partial_{r})u^{z}_{(0),0}+\partial_{z}P_{(0),0}=0,\\ &\partial_{r}u^{r}_{(0),0}+\frac{1}{r}u^{r}_{(0),0}+\partial_{z}u^{z}_{(0),0}=0,\\ &u^{r}_{(0),0}|_{t=0}=a^{r}_{0},\quad u^{z}_{(0),0}|_{t=0}=a^{z}_{0}.\end{split}\right.

To verify this ansatz, we first deduce from Proposition 3.1 that

(4.5) 𝒖(0)L(+;H1)2+𝒖(0)L2(+;H1)2C0.\|\boldsymbol{u}_{(0)}\|_{L^{\infty}(\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{+};H^{1})}^{2}+\|\nabla\boldsymbol{u}_{(0)}\|_{L^{2}(\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{+};H^{1})}^{2}\leq C_{0}.

Here and in all that follows, C0C_{0} denotes some positive constant depending only on the norms of the profiles of 𝒖(0,x)\boldsymbol{u}(0,x) appearing in (1.14), and may be different in each appearance.

On the other hand, in view of the expression (1.13) for initial data, we have

𝒖|t=0𝒖(0)|t=0=εa0θ(r,z)𝒆θ+εk=1(𝒂k(r,z)cos(kθ)+𝒃k(r,z)sin(kθ)).\displaystyle\boldsymbol{u}|_{t=0}-\boldsymbol{u}_{(0)}|_{t=0}=\varepsilon a^{\theta}_{0}(r,z)\boldsymbol{e}_{\theta}+\varepsilon\sum_{k=1}^{\infty}\Bigl(\boldsymbol{a}_{k}(r,z)\cos(k\theta)+\boldsymbol{b}_{k}(r,z)\sin(k\theta)\Bigr).

By using Parseval’s identities, there holds

(4.6) 𝒖|t=0𝒖(0)|t=0H1C0ε.\bigl\|\boldsymbol{u}|_{t=0}-\boldsymbol{u}_{(0)}|_{t=0}\bigr\|_{H^{1}}\leq C_{0}\varepsilon.

Then for sufficiently small ε>0\varepsilon>0, by virtue of (4.5), (4.6) and Proposition 2.1, we obtain

(4.7) 𝒖𝒖(0)L(+;H1L)+(𝒖𝒖(0))L2(+;H1)C0ε.\|\boldsymbol{u}-\boldsymbol{u}_{(0)}\|_{L^{\infty}(\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{+};H^{1}\cap L^{\infty})}+\|\nabla(\boldsymbol{u}-\boldsymbol{u}_{(0)})\|_{L^{2}(\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{+};H^{1})}\leq C_{0}\varepsilon.

Notice that the system (4.4) does not rely on ε\varepsilon, and thus its solution (u(0),0r,u(0),0z)(u^{r}_{(0),0},u^{z}_{(0),0}) also does not rely on ε\varepsilon. This together with the estimate (4.7) guarantees the validity of our Ansatz 11, namely u(0),0r𝒆r+u(0),0z𝒆zu^{r}_{(0),0}\boldsymbol{e}_{r}+u^{z}_{(0),0}\boldsymbol{e}_{z} is indeed the ε0\varepsilon^{0} order term in the expansion of 𝒖\boldsymbol{u}.

In particular, we have shown that u(0),0θu^{\theta}_{(0),0} vanishes, and for every kk\in\mathop{\mathbb{N}\kern 0.0pt}\nolimits, the kk-th Fourier coefficient does not contain ε0\varepsilon^{0} order terms, just the same as the initial data (1.13).

4.2. Derivation of the ε1\varepsilon^{1} order terms in the Euclidean coordinates

Let us temporarily go back to the Euclidean coordinates, and consider 𝒖(1)\boldsymbol{u}_{(1)} as a whole part.

We make the following Ansatz 22: 𝒖(1)\boldsymbol{u}_{(1)} is a solution to the linearization of the perturbed Navier-Stokes system around 𝒖(0)\boldsymbol{u}_{(0)}, precisely

(4.8) {t𝒖(1)+𝒖(0)𝒖(1)+𝒖(1)𝒖(0)Δ𝒖(1)=P(1),div𝒖(1)=0,𝒖(1)|t=0=a0θ𝒆θ+k=1(𝒂kcoskθ+𝒃ksinkθ).\left\{\begin{split}&\partial_{t}\boldsymbol{u}_{(1)}+\boldsymbol{u}_{(0)}\cdot\nabla\boldsymbol{u}_{(1)}+\boldsymbol{u}_{(1)}\cdot\nabla\boldsymbol{u}_{(0)}-\Delta\boldsymbol{u}_{(1)}=-\nabla P_{(1)},\\ &\mathop{\rm div}\nolimits\boldsymbol{u}_{(1)}=0,\\ &\boldsymbol{u}_{(1)}|_{t=0}=a^{\theta}_{0}\boldsymbol{e}_{\theta}+\sum_{k=1}^{\infty}\Bigl(\boldsymbol{a}_{k}\cos k\theta+\boldsymbol{b}_{k}\sin k\theta\Bigr).\end{split}\right.

To verify this ansatz, we first get, by taking L2L^{2} inner product of (4.8) with 𝒖(1)Δ𝒖(1)\boldsymbol{u}_{(1)}-\Delta\boldsymbol{u}_{(1)} that

12ddt\displaystyle\frac{1}{2}\frac{d}{dt} 𝒖(1)H12+𝒖(1)H12|(𝒖(0)𝒖(1)+𝒖(1)𝒖(0))|𝒖(1)Δ𝒖(1))|\displaystyle\|\boldsymbol{u}_{(1)}\|_{H^{1}}^{2}+\|\nabla\boldsymbol{u}_{(1)}\|_{H^{1}}^{2}\leq\bigl|\bigl(\boldsymbol{u}_{(0)}\cdot\nabla\boldsymbol{u}_{(1)}+\boldsymbol{u}_{(1)}\cdot\nabla\boldsymbol{u}_{(0)})\,\big|\,\boldsymbol{u}_{(1)}-\Delta\boldsymbol{u}_{(1)}\bigr)\bigr|
𝒖(1)L3𝒖(0)L2𝒖(1)L6+(𝒖(0)L6𝒖(1)L3+𝒖(1)L𝒖(0)L2)Δ𝒖(1)L2\displaystyle\leq\|\boldsymbol{u}_{(1)}\|_{L^{3}}\|\nabla\boldsymbol{u}_{(0)}\|_{L^{2}}\|\boldsymbol{u}_{(1)}\|_{L^{6}}+\bigl(\|\boldsymbol{u}_{(0)}\|_{L^{6}}\|\nabla\boldsymbol{u}_{(1)}\|_{L^{3}}+\|\boldsymbol{u}_{(1)}\|_{L^{\infty}}\|\nabla\boldsymbol{u}_{(0)}\|_{L^{2}}\bigr)\|\Delta\boldsymbol{u}_{(1)}\|_{L^{2}}
12Δ𝒖(1)L22+C𝒖(1)H12𝒖(0)L24.\displaystyle\leq\frac{1}{2}\|\Delta\boldsymbol{u}_{(1)}\|_{L^{2}}^{2}+C\|\boldsymbol{u}_{(1)}\|_{H^{1}}^{2}\|\nabla\boldsymbol{u}_{(0)}\|_{L^{2}}^{4}.

Subtracting 12Δ𝒖(1)L22\frac{1}{2}\|\Delta\boldsymbol{u}_{(1)}\|_{L^{2}}^{2} on both sides, and then applying Gronwall’s inequality gives

(4.9) 𝒖(1)Lt(H1)2+𝒖(1)Lt2(H1)2𝒖(1)|t=0H12exp(C𝒖(0)Lt(L2)2𝒖(0)Lt2(L2)2)C0.\|\boldsymbol{u}_{(1)}\|_{L^{\infty}_{t}(H^{1})}^{2}+\|\nabla\boldsymbol{u}_{(1)}\|_{L^{2}_{t}(H^{1})}^{2}\leq\|\boldsymbol{u}_{(1)}|_{t=0}\|_{H^{1}}^{2}\exp\bigl(C\|\nabla\boldsymbol{u}_{(0)}\|_{L^{\infty}_{t}(L^{2})}^{2}\|\nabla\boldsymbol{u}_{(0)}\|_{L^{2}_{t}(L^{2})}^{2}\bigr)\leq C_{0}.

While following similar derivation as (2.18), we deduce

(4.10) 𝒖(1)Lt(L4)curl𝒖(1)Lt(L4)C0.\|\nabla\boldsymbol{u}_{(1)}\|_{L^{\infty}_{t}(L^{4})}\lesssim\|\mathop{\rm curl}\nolimits\boldsymbol{u}_{(1)}\|_{L^{\infty}_{t}(L^{4})}\leq C_{0}.

On the other hand, let us consider 𝑹(1)=def𝒖𝒖(0)ε𝒖(1)\boldsymbol{R}_{(1)}\mathrel{\mathop{\kern 0.0pt=}\limits^{\hbox{\footnotesize def}}}\boldsymbol{u}-\boldsymbol{u}_{(0)}-\varepsilon\boldsymbol{u}_{(1)}, which satisfies

(4.11) {t𝑹(1)+𝒖𝑹(1)+𝑹(1)(𝒖(0)+ε𝒖(1))+ε2𝒖(1)𝒖(1)Δ𝑹(1)=Π(1),div𝑹(1)=0,𝑹(1)|t=0=0,\left\{\begin{split}&\partial_{t}\boldsymbol{R}_{(1)}+\boldsymbol{u}\cdot\nabla\boldsymbol{R}_{(1)}+\boldsymbol{R}_{(1)}\cdot\nabla(\boldsymbol{u}_{(0)}+\varepsilon\boldsymbol{u}_{(1)})+\varepsilon^{2}\boldsymbol{u}_{(1)}\cdot\nabla\boldsymbol{u}_{(1)}-\Delta\boldsymbol{R}_{(1)}=-\nabla\Pi_{(1)},\\ &\mathop{\rm div}\nolimits\boldsymbol{R}_{(1)}=0,\\ &\boldsymbol{R}_{(1)}|_{t=0}=0,\end{split}\right.

where Π(1)\Pi_{(1)} can be obtained by taking divergence operator to the first equation in (4.11).

In the following, we shall derive L2,H˙1L^{2},~\dot{H}^{1} and W˙1,4\dot{W}^{1,4} estimate for 𝑹(1)\boldsymbol{R}_{(1)}. Notice that if there is no external force term ε2𝒖(1)𝒖(1)\varepsilon^{2}\boldsymbol{u}_{(1)}\cdot\nabla\boldsymbol{u}_{(1)} in (4.11), then this type of system has already been studied in Proposition 2.1. So here we only focus on the estimate for this external force term.

Firstly, we have

|3ε2(𝒖(1)𝒖(1))𝑹(1)𝑑x|\displaystyle\Bigl|\int_{\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{3}}\varepsilon^{2}\bigl(\boldsymbol{u}_{(1)}\cdot\nabla\boldsymbol{u}_{(1)}\bigr)\boldsymbol{R}_{(1)}\,dx\Bigr| Cε2𝒖(1)L3𝒖(1)L2𝑹(1)L6\displaystyle\leq C\varepsilon^{2}\|\boldsymbol{u}_{(1)}\|_{L^{3}}\|\nabla\boldsymbol{u}_{(1)}\|_{L^{2}}\|\boldsymbol{R}_{(1)}\|_{L^{6}}
12𝑹(1)L22+Cε4𝒖(1)L23𝒖(1)L2,\displaystyle\leq\frac{1}{2}\|\nabla\boldsymbol{R}_{(1)}\|_{L^{2}}^{2}+C\varepsilon^{4}\|\nabla\boldsymbol{u}_{(1)}\|_{L^{2}}^{3}\|\boldsymbol{u}_{(1)}\|_{L^{2}},

and in view of the bound (4.9), there holds

ε40t𝒖(1)L23𝒖(1)L2dtε4𝒖(1)Lt2(L2)2𝒖(1)Lt(L2)𝒖(1)Lt(L2)C0ε4.\varepsilon^{4}\int_{0}^{t}\|\nabla\boldsymbol{u}_{(1)}\|_{L^{2}}^{3}\|\boldsymbol{u}_{(1)}\|_{L^{2}}\,dt^{\prime}\leq\varepsilon^{4}\|\nabla\boldsymbol{u}_{(1)}\|_{L^{2}_{t}(L^{2})}^{2}\|\nabla\boldsymbol{u}_{(1)}\|_{L^{\infty}_{t}(L^{2})}\|\boldsymbol{u}_{(1)}\|_{L^{\infty}_{t}(L^{2})}\leq C_{0}\varepsilon^{4}.

Then a similar procedure as the proof of Proposition 2.1 leads to

(4.12) 𝑹(1)Lt(L2)2+𝑹(1)Lt2(L2)2C0ε4.\|\boldsymbol{R}_{(1)}\|_{L^{\infty}_{t}(L^{2})}^{2}+\|\nabla\boldsymbol{R}_{(1)}\|_{L^{2}_{t}(L^{2})}^{2}\leq C_{0}\varepsilon^{4}.

Similarly, we have

|3ε2(𝒖(1)𝒖(1))Δ𝑹(1)𝑑x|\displaystyle\Bigl|\int_{\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{3}}\varepsilon^{2}\bigl(\boldsymbol{u}_{(1)}\cdot\nabla\boldsymbol{u}_{(1)}\bigr)\cdot\Delta\boldsymbol{R}_{(1)}\,dx\Bigr| ε2𝒖(1)L𝒖(1)L2Δ𝑹(1)L2\displaystyle\leq\varepsilon^{2}\|\boldsymbol{u}_{(1)}\|_{L^{\infty}}\|\nabla\boldsymbol{u}_{(1)}\|_{L^{2}}\|\Delta\boldsymbol{R}_{(1)}\|_{L^{2}}
12Δ𝑹(1)L22+ε4𝒖(1)L23𝒖(1)H˙1,\displaystyle\leq\frac{1}{2}\|\Delta\boldsymbol{R}_{(1)}\|_{L^{2}}^{2}+\varepsilon^{4}\|\nabla\boldsymbol{u}_{(1)}\|_{L^{2}}^{3}\|\nabla\boldsymbol{u}_{(1)}\|_{\dot{H}^{1}},

and

|3ε2curl(𝒖(1)𝒖(1))|curl𝑹(1)|2curl𝑹(1)dx|\displaystyle\Bigl|\int_{\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{3}}\varepsilon^{2}\mathop{\rm curl}\nolimits\bigl(\boldsymbol{u}_{(1)}\cdot\nabla\boldsymbol{u}_{(1)}\bigr)\cdot|\mathop{\rm curl}\nolimits\boldsymbol{R}_{(1)}|^{2}\mathop{\rm curl}\nolimits\boldsymbol{R}_{(1)}\,dx\Bigr|
ε2𝒖(1)L6𝒖(1)L4curl𝑹(1)L12(|curl𝑹(1)|2L2+|curl𝑹(1)|curl𝑹(1)L2)\displaystyle\leq\varepsilon^{2}\|\boldsymbol{u}_{(1)}\|_{L^{6}}\|\nabla\boldsymbol{u}_{(1)}\|_{L^{4}}\|\mathop{\rm curl}\nolimits\boldsymbol{R}_{(1)}\|_{L^{12}}\bigl(\bigl\|\nabla|\mathop{\rm curl}\nolimits\boldsymbol{R}_{(1)}|^{2}\bigr\|_{L^{2}}+\bigl\||\mathop{\rm curl}\nolimits\boldsymbol{R}_{(1)}|\cdot\nabla\mathop{\rm curl}\nolimits\boldsymbol{R}_{(1)}\bigr\|_{L^{2}}\bigr)
14(|curl𝑹(1)|2L22+|curl𝑹(1)|curl𝑹(1)L22)+ε8𝒖(1)L24𝒖(1)L44.\displaystyle\leq\frac{1}{4}\bigl(\bigl\|\nabla|\mathop{\rm curl}\nolimits\boldsymbol{R}_{(1)}|^{2}\bigr\|_{L^{2}}^{2}+\bigl\||\mathop{\rm curl}\nolimits\boldsymbol{R}_{(1)}|\cdot\nabla\mathop{\rm curl}\nolimits\boldsymbol{R}_{(1)}\bigr\|_{L^{2}}^{2}\bigr)+\varepsilon^{8}\|\nabla\boldsymbol{u}_{(1)}\|_{L^{2}}^{4}\|\nabla\boldsymbol{u}_{(1)}\|_{L^{4}}^{4}.

In view of the bounds (4.9) and (4.10), there holds

ε40t𝒖(1)L23𝒖(1)H˙1dtC0ε4,andε80t𝒖(1)L24𝒖(1)L44dtC0ε8.\varepsilon^{4}\int_{0}^{t}\|\nabla\boldsymbol{u}_{(1)}\|_{L^{2}}^{3}\|\nabla\boldsymbol{u}_{(1)}\|_{\dot{H}^{1}}\,dt^{\prime}\leq C_{0}\varepsilon^{4},\quad\hbox{and}\quad\varepsilon^{8}\int_{0}^{t}\|\nabla\boldsymbol{u}_{(1)}\|_{L^{2}}^{4}\|\nabla\boldsymbol{u}_{(1)}\|_{L^{4}}^{4}\,dt^{\prime}\leq C_{0}\varepsilon^{8}.

Then a similar procedure as the proof of Proposition 2.1 leads to

(4.13) 𝑹(1)Lt(H˙1)2+𝑹(1)Lt2(H˙1)2C0ε4,and𝑹(1)Lt(L4)4C0ε8.\|\boldsymbol{R}_{(1)}\|_{L^{\infty}_{t}(\dot{H}^{1})}^{2}+\|\nabla\boldsymbol{R}_{(1)}\|_{L^{2}_{t}(\dot{H}^{1})}^{2}\leq C_{0}\varepsilon^{4},\quad\hbox{and}\quad\|\nabla\boldsymbol{R}_{(1)}\|_{L^{\infty}_{t}(L^{4})}^{4}\leq C_{0}\varepsilon^{8}.

Now in view of the estimates (4.12) and (4.13), together with the interpolation inequality fLfL213fL423\|f\|_{L^{\infty}}\lesssim\|\nabla f\|_{L^{2}}^{\frac{1}{3}}\|\nabla f\|_{L^{4}}^{\frac{2}{3}}, we achieve

(4.14) 𝑹(1)Lt(H1L)2+𝑹(1)Lt2(H1)2C0ε4.\|\boldsymbol{R}_{(1)}\|_{L^{\infty}_{t}(H^{1}\cap L^{\infty})}^{2}+\|\nabla\boldsymbol{R}_{(1)}\|_{L^{2}_{t}(H^{1})}^{2}\leq C_{0}\varepsilon^{4}.

In view of the estimate (4.14) for the remainder 𝑹(1)\boldsymbol{R}_{(1)}, and the fact that 𝒖(1)\boldsymbol{u}_{(1)} determined by (4.8) does not rely on ε\varepsilon, we have verified our Ansatz 22.

Remark 4.1.

Exactly along the same line, we can prove by induction that for any n2n\geq 2, 𝐮(n)\boldsymbol{u}_{(n)} is a solution to the following linearized system:

{t𝒖(n)+𝒖(0)𝒖(n)+𝒖(n)𝒖(0)Δ𝒖(n)+P(n)=i=1n1𝒖(i)𝒖(ni),div𝒖(n)=0,𝒖(n)|t=0=0.\left\{\begin{split}&\partial_{t}\boldsymbol{u}_{(n)}+\boldsymbol{u}_{(0)}\cdot\nabla\boldsymbol{u}_{(n)}+\boldsymbol{u}_{(n)}\cdot\nabla\boldsymbol{u}_{(0)}-\Delta\boldsymbol{u}_{(n)}+\nabla P_{(n)}=-\sum_{i=1}^{n-1}\boldsymbol{u}_{(i)}\cdot\nabla\boldsymbol{u}_{(n-i)},\\ &\mathop{\rm div}\nolimits\boldsymbol{u}_{(n)}=0,\\ &\boldsymbol{u}_{(n)}|_{t=0}=0.\end{split}\right.

And the remainder term 𝐑(n)=def𝐮𝐮(0)ε𝐮(1)εn𝐮(n)\boldsymbol{R}_{(n)}\mathrel{\mathop{\kern 0.0pt=}\limits^{\hbox{\footnotesize def}}}\boldsymbol{u}-\boldsymbol{u}_{(0)}-\varepsilon\boldsymbol{u}_{(1)}-\cdots-\varepsilon^{n}\boldsymbol{u}_{(n)} satisfies

𝑹(n)Lt(H1L)C0εn+1.\|\boldsymbol{R}_{(n)}\|_{L^{\infty}_{t}(H^{1}\cap L^{\infty})}\leq C_{0}\varepsilon^{n+1}.

4.3. Verification of u(1),0r=u(1),0z=0u^{r}_{(1),0}=u^{z}_{(1),0}=0

Noticing that 𝒖(0)=u(0),0r𝒆r+u(0),0z𝒆z\boldsymbol{u}_{(0)}=u^{r}_{(0),0}\boldsymbol{e}_{r}+u^{z}_{(0),0}\boldsymbol{e}_{z} is axisymmetric without swirl, it is not difficult to deduce from (4.8) that (u(1),0r,u(1),0z)\bigl(u^{r}_{(1),0},u^{z}_{(1),0}\bigr) satisfies

(4.15) {tu(1),0r+𝒖(0)u(1),0r+𝒖~(1),0~u(0),0r(Δ1r2)u(1),0r+rP(1),0=0,tu(1),0z+𝒖(0)u(1),0z+𝒖~(1),0~u(0),0zΔu(1),0z+zP(1),0=0,ru(1),0r+1ru(1),0r+zu(1),0z=0,u(1),0r|t=0=u(1),0z|t=0=0,\left\{\begin{aligned} &\partial_{t}u^{r}_{(1),0}+\boldsymbol{u}_{(0)}\cdot\nabla u^{r}_{(1),0}+\widetilde{\boldsymbol{u}}_{(1),0}\cdot\widetilde{\nabla}u^{r}_{(0),0}-(\Delta-\frac{1}{r^{2}})u^{r}_{(1),0}+\partial_{r}P_{(1),0}=0,\\ &\partial_{t}u^{z}_{(1),0}+\boldsymbol{u}_{(0)}\cdot\nabla u^{z}_{(1),0}+\widetilde{\boldsymbol{u}}_{(1),0}\cdot\widetilde{\nabla}u^{z}_{(0),0}-\Delta u^{z}_{(1),0}+\partial_{z}P_{(1),0}=0,\\ &\partial_{r}u^{r}_{(1),0}+\frac{1}{r}u^{r}_{(1),0}+\partial_{z}u^{z}_{(1),0}=0,\\ &u^{r}_{(1),0}|_{t=0}=u^{z}_{(1),0}|_{t=0}=0,\end{aligned}\right.

where 𝒖~(1),0=defu(1),0r𝒆r+u(1),0z𝒆z\widetilde{\boldsymbol{u}}_{(1),0}\mathrel{\mathop{\kern 0.0pt=}\limits^{\hbox{\footnotesize def}}}u^{r}_{(1),0}\boldsymbol{e}_{r}+u^{z}_{(1),0}\boldsymbol{e}_{z}, and the divergence-free condition here follows from

div𝒖(1),0=ru(1),0r+u(1),0rr+zu(1),0z=(ru(1)r+u(1)rr+θu(1)θr+zu(1)z)=(div𝒖(1))=0.\displaystyle\begin{aligned} \mathop{\rm div}\nolimits\boldsymbol{u}_{(1),0}=&\partial_{r}u^{r}_{(1),0}+\frac{u^{r}_{(1),0}}{r}+\partial_{z}u^{z}_{(1),0}\\ =&{\mathcal{M}}\Bigl(\partial_{r}u^{r}_{(1)}+\frac{u^{r}_{(1)}}{r}+\frac{\partial_{\theta}u^{\theta}_{(1)}}{r}+\partial_{z}u^{z}_{(1)}\Bigr)={\mathcal{M}}(\mathop{\rm div}\nolimits\boldsymbol{u}_{(1)})=0.\end{aligned}

By taking L2L^{2} inner product of (4.15) with (u(1),0r,u(1),0z)\bigl(u^{r}_{(1),0},u^{z}_{(1),0}\bigr), we get

(4.16) 12ddt𝒖~(1),0L22+𝒖~(1),0L22=(𝒖~(1),0~u(0),0r|u(1),0r)(𝒖~(1),0~u(0),0z|u(1),0z),\frac{1}{2}\frac{d}{dt}\|\widetilde{\boldsymbol{u}}_{(1),0}\|_{L^{2}}^{2}+\|\nabla\widetilde{\boldsymbol{u}}_{(1),0}\|_{L^{2}}^{2}=-\bigl(\widetilde{\boldsymbol{u}}_{(1),0}\cdot\widetilde{\nabla}u^{r}_{(0),0}\,|\,u^{r}_{(1),0}\bigr)-\bigl(\widetilde{\boldsymbol{u}}_{(1),0}\cdot\widetilde{\nabla}u^{z}_{(0),0}\,|\,u^{z}_{(1),0}\bigr),

where we used the fact that θrP(1),0(t,r,z)=0\frac{\partial_{\theta}}{r}P_{(1),0}(t,r,z)=0 and then the following equality

(~P(1),0|𝒖~(1),0)=(P(1),0|𝒖(1),0)=(P(1),0|div𝒖(1),0)=0.\displaystyle-\bigl(\widetilde{\nabla}P_{(1),0}\,|\,\widetilde{\boldsymbol{u}}_{(1),0}\bigr)=-\bigl(\nabla P_{(1),0}\,|\,\boldsymbol{u}_{(1),0}\bigr)=\bigl(P_{(1),0}\,|\,\mathop{\rm div}\nolimits\boldsymbol{u}_{(1),0}\bigr)=0.

For the terms on the right-hand side of (4.16), we have

|(𝒖~(1),0ur(0),0|ur(1),0)|+|(𝒖~(1),0OPENu(0),0z|u(1),0z)|C𝒖(0)L2𝒖~(1),0L42C𝒖(0)L2𝒖~(1),0L212𝒖~(1),0L23212𝒖~(1),0L22+C𝒖~(1),0L22𝒖(0)L24.\displaystyle\begin{aligned} \bigl|\bigl(\widetilde{\boldsymbol{u}}_{(1),0}\cdot\nabla u^{r}_{(0),0}\,|\,u^{r}_{(1),0}\bigr)\bigr|+\bigl|\bigl(\widetilde{\boldsymbol{u}}_{(1),0}\cdot&\nabla u^{z}_{(0),0}\,|\,u^{z}_{(1),0}\bigr)\bigr|\leq C\|\nabla\boldsymbol{u}_{(0)}\|_{L^{2}}\|\widetilde{\boldsymbol{u}}_{(1),0}\|_{L^{4}}^{2}\\ &\leq C\|\nabla\boldsymbol{u}_{(0)}\|_{L^{2}}\|\widetilde{\boldsymbol{u}}_{(1),0}\|_{L^{2}}^{\frac{1}{2}}\|\nabla\widetilde{\boldsymbol{u}}_{(1),0}\|_{L^{2}}^{\frac{3}{2}}\\ &\leq\frac{1}{2}\|\nabla\widetilde{\boldsymbol{u}}_{(1),0}\|_{L^{2}}^{2}+C\|\widetilde{\boldsymbol{u}}_{(1),0}\|_{L^{2}}^{2}\|\nabla\boldsymbol{u}_{(0)}\|_{L^{2}}^{4}.\end{aligned}

As a result, we deduce

ddt𝒖~(1),0L22+𝒖~(1),0L22C𝒖~(1),0L22𝒖(0)L24.\frac{d}{dt}\|\widetilde{\boldsymbol{u}}_{(1),0}\|_{L^{2}}^{2}+\|\nabla\widetilde{\boldsymbol{u}}_{(1),0}\|_{L^{2}}^{2}\leq C\|\widetilde{\boldsymbol{u}}_{(1),0}\|_{L^{2}}^{2}\|\nabla\boldsymbol{u}_{(0)}\|_{L^{2}}^{4}.

Then by applying Gronwall’s inequality, together with the fact that initially 𝒖~(1),0|t=0=0\widetilde{\boldsymbol{u}}_{(1),0}|_{t=0}=0, we deduce that 𝒖~(1),0\widetilde{\boldsymbol{u}}_{(1),0} actually vanishes for all time. This completes the proof of Theorem 1.2.

5. The proof of Theorem 1.3

As the initial data (1.19) considered here is a special case of (1.13), Theorem 1.1 guarantees the existence of a unique global solution 𝒖C(+;H1)L2(+;H˙1H˙2)\boldsymbol{u}\in C(\mathop{\mathbb{R}\kern 0.0pt}\nolimits_{+};H^{1})\cap L^{2}(\mathop{\mathbb{R}\kern 0.0pt}\nolimits_{+};\dot{H}^{1}\cap\dot{H}^{2}) for sufficiently small ε\varepsilon. And this solution can be expanded as (1.18). Hence the aim in the following is to show that uru^{r} and uzu^{z} remain even in θ\theta, while uθu^{\theta} keeps odd in θ\theta for all time, namely

𝒖(1),0=0,uθ(j),0=0,vr(j),k=uθ(j),k=vz(j),k=0,j,k.\boldsymbol{u}_{(1),0}=0,\quad u^{\theta}_{(j),0}=0,\quad v^{r}_{(j),k}=u^{\theta}_{(j),k}=v^{z}_{(j),k}=0,\quad\forall\ j\in\mathop{\mathbb{N}\kern 0.0pt}\nolimits,~k\in\mathop{\mathbb{N}\kern 0.0pt}\nolimits.

5.1. Verification of 𝒖(1),0=𝟎\boldsymbol{u}_{(1),0}=\boldsymbol{0}

For the initial data 𝒖(0,x)\boldsymbol{u}(0,x) given by (1.19), we have

(𝒖|t=0)=a0r(r,z)𝒆r+a0z(r,z)𝒆z.\displaystyle{\mathcal{M}}(\boldsymbol{u}|_{t=0})=a^{r}_{0}(r,z)\boldsymbol{e}_{r}+a^{z}_{0}(r,z)\boldsymbol{e}_{z}.

Thus the quantity 𝒖¯\bar{\boldsymbol{u}} defined by (1.6), is exactly u(0),0r𝒆r+u(0),0z𝒆zu^{r}_{(0),0}\boldsymbol{e}_{r}+u^{z}_{(0),0}\boldsymbol{e}_{z}, which sloves the axisymmetric without swirl N-S (4.4) for the case here.

On the other hand, noticing that uθ|t=0εu^{\theta}|_{t=0}\thicksim\varepsilon and

θur|t=0=εk=1karksinkθ,θuθ|t=0=εk=1kbθkcoskθ,θuz|t=0=εk=1kazksinkθ,\partial_{\theta}u^{r}|_{t=0}=-\varepsilon\sum_{k=1}^{\infty}ka^{r}_{k}\sin k\theta,\quad\partial_{\theta}u^{\theta}|_{t=0}=\varepsilon\sum_{k=1}^{\infty}kb^{\theta}_{k}\cos k\theta,\quad\partial_{\theta}u^{z}|_{t=0}=-\varepsilon\sum_{k=1}^{\infty}ka^{z}_{k}\sin k\theta,

we can get by using the refined estimate (1.12) in Theorem 1.1 that

(𝒖)u(0),0r𝒆ru(0),0z𝒆zL(+;L2)C0ε2.\|{\mathcal{M}}(\boldsymbol{u})-u^{r}_{(0),0}\boldsymbol{e}_{r}-u^{z}_{(0),0}\boldsymbol{e}_{z}\|_{L^{\infty}(\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{+};L^{2})}\leq C_{0}\varepsilon^{2}.

This together with the fact that (𝒖)=𝒖(0),0+ε𝒖(1),0+ε2𝒖(2),0+{\mathcal{M}}(\boldsymbol{u})=\boldsymbol{u}_{(0),0}+\varepsilon\boldsymbol{u}_{(1),0}+\varepsilon^{2}\boldsymbol{u}_{(2),0}+\cdots implies

(5.1) 𝒖(0),0=u(0),0r𝒆r+u(0),0z𝒆z,and𝒖(1),0=0.\boldsymbol{u}_{(0),0}=u^{r}_{(0),0}\boldsymbol{e}_{r}+u^{z}_{(0),0}\boldsymbol{e}_{z},\quad\hbox{and}\quad\boldsymbol{u}_{(1),0}=0.

5.2. Verification of v(1),kr=u(1),kθ=v(1),kz=0v^{r}_{(1),k}=u^{\theta}_{(1),k}=v^{z}_{(1),k}=0

In view of (5.1), we can write

(5.2) 𝒖(1)=k=1(𝒖(1),kcoskθ+𝒗(1),ksinkθ),\boldsymbol{u}_{(1)}=\sum_{k=1}^{\infty}\Bigl(\boldsymbol{u}_{(1),k}\cos k\theta+\boldsymbol{v}_{(1),k}\sin k\theta\Bigr),

and the corresponding pressure

P(1)=k=1(P(1),kcoskθ+Q(1),ksinkθ).P_{(1)}=\sum_{k=1}^{\infty}\Bigl(P_{(1),k}\cos k\theta+Q_{(1),k}\sin k\theta\Bigr).

And from the proof of Subsection 4.2, we know that (𝒖(1),P(1))(\boldsymbol{u}_{(1)},P_{(1)}) satisfies (4.8).

Then it is crucial to notice that 𝒖(0)\boldsymbol{u}_{(0)} is axisymmetric without swirl, which makes the couplings between each component of 𝒖(1)\boldsymbol{u}_{(1)} in (4.8)(4.8) not so strong. In fact, by rewriting (4.8) according to the basis {coskθ,sinkθ:k}\{\cos k\theta,\sin k\theta:k\in\mathop{\mathbb{N}\kern 0.0pt}\nolimits\}, it is not difficult to find that we can decompose 𝒖(1)\boldsymbol{u}_{(1)} and P(1)P_{(1)} into two parts: 𝒖(1)+𝒖(1)′′\boldsymbol{u}_{(1)}^{\prime}+\boldsymbol{u}_{(1)}^{\prime\prime} and P(1)+P(1)′′P_{(1)}^{\prime}+P_{(1)}^{\prime\prime} respectively, where

𝒖(1)=defk=1(u(1),krcoskθ𝒆r+v(1),kθsinkθ𝒆θ+u(1),kzcoskθ𝒆z),P(1)=defk=1P(1),kcoskθ,\boldsymbol{u}_{(1)}^{\prime}\mathrel{\mathop{\kern 0.0pt=}\limits^{\hbox{\footnotesize def}}}\sum_{k=1}^{\infty}\Bigl(u^{r}_{(1),k}\cos k\theta\boldsymbol{e}_{r}+v^{\theta}_{(1),k}\sin k\theta\boldsymbol{e}_{\theta}+u^{z}_{(1),k}\cos k\theta\boldsymbol{e}_{z}\Bigr),\quad P_{(1)}^{\prime}\mathrel{\mathop{\kern 0.0pt=}\limits^{\hbox{\footnotesize def}}}\sum_{k=1}^{\infty}P_{(1),k}\cos k\theta,

and

𝒖(1)′′=defk=1(v(1),krsinkθ𝒆r+u(1),kθcoskθ𝒆θ+v(1),kzsinkθ𝒆z),P(1)′′=defk=1Q(1),ksinkθ,\boldsymbol{u}_{(1)}^{\prime\prime}\mathrel{\mathop{\kern 0.0pt=}\limits^{\hbox{\footnotesize def}}}\sum_{k=1}^{\infty}\Bigl(v^{r}_{(1),k}\sin k\theta\boldsymbol{e}_{r}+u^{\theta}_{(1),k}\cos k\theta\boldsymbol{e}_{\theta}+v^{z}_{(1),k}\sin k\theta\boldsymbol{e}_{z}\Bigr),\quad P_{(1)}^{\prime\prime}\mathrel{\mathop{\kern 0.0pt=}\limits^{\hbox{\footnotesize def}}}\sum_{k=1}^{\infty}Q_{(1),k}\sin k\theta,

such that 𝒖(1)\boldsymbol{u}_{(1)}^{\prime} and P(1)P_{(1)}^{\prime} satisfy the following self-contained system:

(5.3) {tur(1),k+(ur(0),0r+uz(0),0z)ur(1),k+(ur(1),kr+uz(1),kz)ur(0),0(r2+z2+1rr1+k2r2)ur(1),k+2kv(1),kθr2+rP(1),k=0,tvθ(1),k+(ur(0),0r+uz(0),0z)vθ(1),k+u(0),0rv(1),kθr(r2+z2+1rr1+k2r2)vθ(1),k+2ku(1),krr2krP(1),k=0,tuz(1),k+(ur(0),0r+uz(0),0z)uz(1),k+(ur(1),kr+uz(1),kz)uz(0),0(r2+z2+1rrk2r2)uz(1),k+zP(1),k=0,ru(1),kr+1ru(1),kr+zu(1),kz+krv(1),kθ=0,ur(1),k|t=0=ark,vθ(1),k|t=0=bθk,uz(1),k|t=0=azk,\left\{\begin{aligned} &\partial_{t}u^{r}_{(1),k}+(u^{r}_{(0),0}\partial_{r}+u^{z}_{(0),0}\partial_{z})u^{r}_{(1),k}+(u^{r}_{(1),k}\partial_{r}+u^{z}_{(1),k}\partial_{z})u^{r}_{(0),0}\\ &\qquad\qquad\qquad-(\partial_{r}^{2}+\partial_{z}^{2}+\frac{1}{r}\partial_{r}-\frac{1+k^{2}}{r^{2}})u^{r}_{(1),k}+2k\frac{v^{\theta}_{(1),k}}{r^{2}}+\partial_{r}P_{(1),k}=0,\\ &\partial_{t}v^{\theta}_{(1),k}+(u^{r}_{(0),0}\partial_{r}+u^{z}_{(0),0}\partial_{z})v^{\theta}_{(1),k}+\frac{u^{r}_{(0),0}v^{\theta}_{(1),k}}{r}\\ &\qquad\qquad\qquad-(\partial_{r}^{2}+\partial_{z}^{2}+\frac{1}{r}\partial_{r}-\frac{1+k^{2}}{r^{2}})v^{\theta}_{(1),k}+2k\frac{u^{r}_{(1),k}}{r^{2}}-\frac{k}{r}P_{(1),k}=0,\\ &\partial_{t}u^{z}_{(1),k}+(u^{r}_{(0),0}\partial_{r}+u^{z}_{(0),0}\partial_{z})u^{z}_{(1),k}+(u^{r}_{(1),k}\partial_{r}+u^{z}_{(1),k}\partial_{z})u^{z}_{(0),0}\\ &\qquad\qquad\qquad-(\partial_{r}^{2}+\partial_{z}^{2}+\frac{1}{r}\partial_{r}-\frac{k^{2}}{r^{2}})u^{z}_{(1),k}+\partial_{z}P_{(1),k}=0,\\ &\partial_{r}u^{r}_{(1),k}+\frac{1}{r}u^{r}_{(1),k}+\partial_{z}u^{z}_{(1),k}+\frac{k}{r}v^{\theta}_{(1),k}=0,\\ &u^{r}_{(1),k}|_{t=0}=a^{r}_{k},\quad v^{\theta}_{(1),k}|_{t=0}=b^{\theta}_{k},\quad u^{z}_{(1),k}|_{t=0}=a^{z}_{k},\end{aligned}\right.

while 𝒖(1)′′\boldsymbol{u}_{(1)}^{\prime\prime} and P(1)′′P_{(1)}^{\prime\prime} satisfy the following self-contained system:

(5.4) {tvr(1),k+(ur(0),0r+uz(0),0z)vr(1),k+(vr(1),kr+vz(1),kz)ur(0),0(r2+z2+1rr1+k2r2)vr(1),k2ku(1),kθr2+rQ(1),k=0,tuθ(1),k+(ur(0),0r+uz(0),0z)uθ(1),k+u(0),0ru(1),kθr(r2+z2+1rr1+k2r2)uθ(1),k2kv(1),krr2+krQ(1),k=0,tvz(1),k+(ur(0),0r+uz(0),0z)vz(1),k+(vr(1),kr+vz(1),kz)uz(0),0(r2+z2+1rrk2r2)vz(1),k+zQ(1),k=0,rv(1),kr+1rv(1),kr+zv(1),kzkru(1),kθ=0,vr(1),k|t=0=0,uθ(1),k|t=0=0,vz(1),k|t=0=0.\left\{\begin{aligned} &\partial_{t}v^{r}_{(1),k}+(u^{r}_{(0),0}\partial_{r}+u^{z}_{(0),0}\partial_{z})v^{r}_{(1),k}+(v^{r}_{(1),k}\partial_{r}+v^{z}_{(1),k}\partial_{z})u^{r}_{(0),0}\\ &\qquad\qquad\qquad-(\partial_{r}^{2}+\partial_{z}^{2}+\frac{1}{r}\partial_{r}-\frac{1+k^{2}}{r^{2}})v^{r}_{(1),k}-2k\frac{u^{\theta}_{(1),k}}{r^{2}}+\partial_{r}Q_{(1),k}=0,\\ &\partial_{t}u^{\theta}_{(1),k}+(u^{r}_{(0),0}\partial_{r}+u^{z}_{(0),0}\partial_{z})u^{\theta}_{(1),k}+\frac{u^{r}_{(0),0}u^{\theta}_{(1),k}}{r}\\ &\qquad\qquad\qquad-(\partial_{r}^{2}+\partial_{z}^{2}+\frac{1}{r}\partial_{r}-\frac{1+k^{2}}{r^{2}})u^{\theta}_{(1),k}-2k\frac{v^{r}_{(1),k}}{r^{2}}+\frac{k}{r}Q_{(1),k}=0,\\ &\partial_{t}v^{z}_{(1),k}+(u^{r}_{(0),0}\partial_{r}+u^{z}_{(0),0}\partial_{z})v^{z}_{(1),k}+(v^{r}_{(1),k}\partial_{r}+v^{z}_{(1),k}\partial_{z})u^{z}_{(0),0}\\ &\qquad\qquad\qquad-(\partial_{r}^{2}+\partial_{z}^{2}+\frac{1}{r}\partial_{r}-\frac{k^{2}}{r^{2}})v^{z}_{(1),k}+\partial_{z}Q_{(1),k}=0,\\ &\partial_{r}v^{r}_{(1),k}+\frac{1}{r}v^{r}_{(1),k}+\partial_{z}v^{z}_{(1),k}-\frac{k}{r}u^{\theta}_{(1),k}=0,\\ &v^{r}_{(1),k}|_{t=0}=0,\quad u^{\theta}_{(1),k}|_{t=0}=0,\quad v^{z}_{(1),k}|_{t=0}=0.\end{aligned}\right.

Then by taking L2L^{2} inner product of (5.4) with (v(1),kr,u(1),kθ,v(1),kz)(v^{r}_{(1),k},u^{\theta}_{(1),k},v^{z}_{(1),k}), we obtain

(5.5) \displaystyle 12ddt(v(1),kr,u(1),kθ,v(1),kz)L22+(v(1),kr,u(1),kθ,v(1),kz)L22+k2v(1),kzrL22\displaystyle\frac{1}{2}\frac{d}{dt}\|(v^{r}_{(1),k},u^{\theta}_{(1),k},v^{z}_{(1),k})\|_{L^{2}}^{2}+\|\nabla(v^{r}_{(1),k},u^{\theta}_{(1),k},v^{z}_{(1),k})\|_{L^{2}}^{2}+k^{2}\bigl\|\frac{v^{z}_{(1),k}}{r}\bigr\|_{L^{2}}^{2}
+(1+k2)(v(1),krrL22+u(1),kθrL22)=3(4ku(1),kθv(1),krr2u(0),0r|u(1),kθ|2rCLOSE\displaystyle+(1+k^{2})\bigl(\bigl\|\frac{v^{r}_{(1),k}}{r}\bigr\|_{L^{2}}^{2}+\bigl\|\frac{u^{\theta}_{(1),k}}{r}\bigr\|_{L^{2}}^{2}\bigr)=\int_{\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{3}}\Bigl(4k\frac{u^{\theta}_{(1),k}v^{r}_{(1),k}}{r^{2}}-\frac{u^{r}_{(0),0}|u^{\theta}_{(1),k}|^{2}}{r}
(vr(1),kr+vz(1),kz)ur(0),0vr(1),k(vr(1),kr+vz(1),kz)uz(0),0vz(1),k)dx.\displaystyle-(v^{r}_{(1),k}\partial_{r}+v^{z}_{(1),k}\partial_{z})u^{r}_{(0),0}\cdot v^{r}_{(1),k}-(v^{r}_{(1),k}\partial_{r}+v^{z}_{(1),k}\partial_{z})u^{z}_{(0),0}\cdot v^{z}_{(1),k}\Bigr)\,dx.

It is worth mentioning that, not the same as the most cases in doing estimates in PDE, the constant in this inequality is very important. Precisely, we have

4k|3u(1),kθv(1),krr2𝑑x|\displaystyle 4k\Bigl|\int_{\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{3}}\frac{u^{\theta}_{(1),k}v^{r}_{(1),k}}{r^{2}}\,dx\Bigr| 4kv(1),krrL2u(1),kθrL2\displaystyle\leq 4k\bigl\|\frac{v^{r}_{(1),k}}{r}\bigr\|_{L^{2}}\bigl\|\frac{u^{\theta}_{(1),k}}{r}\bigr\|_{L^{2}}
2k(v(1),krrL22+u(1),kθrL22)(1+k2)(v(1),krrL22+u(1),kθrL22).\displaystyle\leq 2k\bigl(\bigl\|\frac{v^{r}_{(1),k}}{r}\bigr\|_{L^{2}}^{2}+\bigl\|\frac{u^{\theta}_{(1),k}}{r}\bigr\|_{L^{2}}^{2}\bigr)\leq(1+k^{2})\bigl(\bigl\|\frac{v^{r}_{(1),k}}{r}\bigr\|_{L^{2}}^{2}+\bigl\|\frac{u^{\theta}_{(1),k}}{r}\bigr\|_{L^{2}}^{2}\bigr).

On the other hand, by using Sobolev’s embedding theorem and Young’s inequality, we get

|3((v(1),krr+v(1),kzz)u(0),0rv(1),kr+u(0),0r|u(1),kθ|2r+(v(1),krr+v(1),kzz)u(0),0zv(1),kz)dx|\displaystyle\Bigl|\int_{\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{3}}\Bigl((v^{r}_{(1),k}\partial_{r}+v^{z}_{(1),k}\partial_{z})u^{r}_{(0),0}\cdot v^{r}_{(1),k}+\frac{u^{r}_{(0),0}|u^{\theta}_{(1),k}|^{2}}{r}+(v^{r}_{(1),k}\partial_{r}+v^{z}_{(1),k}\partial_{z})u^{z}_{(0),0}\cdot v^{z}_{(1),k}\Bigr)\,dx\Bigr|
(v(1),krL42+v(1),kzL42)(~u(0),0rL2+~u(0),0zL2)+u(1),kθL42u(0),0rrL2\displaystyle\leq\bigl(\|v^{r}_{(1),k}\|_{L^{4}}^{2}+\|v^{z}_{(1),k}\|_{L^{4}}^{2}\bigr)\bigl(\|\widetilde{\nabla}u^{r}_{(0),0}\|_{L^{2}}+\|\widetilde{\nabla}u^{z}_{(0),0}\|_{L^{2}}\bigr)+\|u^{\theta}_{(1),k}\|_{L^{4}}^{2}\bigl\|\frac{u^{r}_{(0),0}}{r}\bigr\|_{L^{2}}
12(v(1),kr,u(1),kθ,v(1),kz)L22+C(v(1),kr,u(1),kθ,v(1),kz)L22𝒖(0)L24,\displaystyle\leq\frac{1}{2}\|\nabla(v^{r}_{(1),k},u^{\theta}_{(1),k},v^{z}_{(1),k})\|_{L^{2}}^{2}+C\|(v^{r}_{(1),k},u^{\theta}_{(1),k},v^{z}_{(1),k})\|_{L^{2}}^{2}\|\nabla\boldsymbol{u}_{(0)}\|_{L^{2}}^{4},

where in the last step we have used the fact that 𝒖(0)=u(0),0r𝒆r+u(0),0z𝒆z\boldsymbol{u}_{(0)}=u^{r}_{(0),0}\boldsymbol{e}_{r}+u^{z}_{(0),0}\boldsymbol{e}_{z}, so that

𝒖(0)L2~u(0),0rL2+~u(0),0zL2+u(0),0rrL2.\|\nabla\boldsymbol{u}_{(0)}\|_{L^{2}}\sim\|\widetilde{\nabla}u^{r}_{(0),0}\|_{L^{2}}+\|\widetilde{\nabla}u^{z}_{(0),0}\|_{L^{2}}+\bigl\|\frac{u^{r}_{(0),0}}{r}\bigr\|_{L^{2}}.

By substituting the above estimates into (5.5), we deduce

ddt(v(1),kr,u(1),kθ,v(1),kz)L22+(v(1),kr,u(1),kθ,v(1),kz)L22C(v(1),kr,u(1),kθ,v(1),kz)L22𝒖(0)L24.\frac{d}{dt}\|(v^{r}_{(1),k},u^{\theta}_{(1),k},v^{z}_{(1),k})\|_{L^{2}}^{2}+\|\nabla(v^{r}_{(1),k},u^{\theta}_{(1),k},v^{z}_{(1),k})\|_{L^{2}}^{2}\leq C\|(v^{r}_{(1),k},u^{\theta}_{(1),k},v^{z}_{(1),k})\|_{L^{2}}^{2}\|\nabla\boldsymbol{u}_{(0)}\|_{L^{2}}^{4}.

Then by applying Gronwall’s inequality, and using the fact that

0𝒖(0)(t)L24dt𝒖(0)L(+;L2)2𝒖(0)L2(+;L2)2<,\int_{0}^{\infty}\|\nabla\boldsymbol{u}_{(0)}(t^{\prime})\|_{L^{2}}^{4}\,dt^{\prime}\leq\|\nabla\boldsymbol{u}_{(0)}\|_{L^{\infty}(\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{+};L^{2})}^{2}\|\nabla\boldsymbol{u}_{(0)}\|_{L^{2}(\mathop{\mathbb{R}\kern 0.0pt}\nolimits^{+};L^{2})}^{2}<\infty,

which is guaranteed by (4.5), and initially v(1),kr|t=0=u(1),kθ|t=0=v(1),kz|t=0=0v^{r}_{(1),k}|_{t=0}=u^{\theta}_{(1),k}|_{t=0}=v^{z}_{(1),k}|_{t=0}=0, we obtain that

v(1),kr=u(1),kθ=v(1),kz=0,t>0.\displaystyle v^{r}_{(1),k}=u^{\theta}_{(1),k}=v^{z}_{(1),k}=0,\quad\forall\ t>0.

In another word, we can further reduce the expansion for 𝒖(1)\boldsymbol{u}_{(1)} in (5.2) to be

(5.6) 𝒖(1)=k=1(u(1),krcoskθ𝒆r+v(1),kθsinkθ𝒆θ+u(1),kzcoskθ𝒆z),\boldsymbol{u}_{(1)}=\sum_{k=1}^{\infty}\Bigl(u^{r}_{(1),k}\cos k\theta\boldsymbol{e}_{r}+v^{\theta}_{(1),k}\sin k\theta\boldsymbol{e}_{\theta}+u^{z}_{(1),k}\cos k\theta\boldsymbol{e}_{z}\Bigr),

where u(1),kr,v(1),kθu^{r}_{(1),k},~v^{\theta}_{(1),k} and u(1),kzu^{z}_{(1),k} are determined by (5.3).

5.3. Verification of u(j),0θ=v(j),kr=u(j),kθ=v(j),kz=0u^{\theta}_{(j),0}=v^{r}_{(j),k}=u^{\theta}_{(j),k}=v^{z}_{(j),k}=0, for any j,kj\in\mathop{\mathbb{N}\kern 0.0pt}\nolimits,~k\in\mathop{\mathbb{N}\kern 0.0pt}\nolimits

We shall prove this result by the induction method. Assume that for any n2n\geq 2 and any 1jn11\leq j\leq n-1,

uθ(j),0=vr(j),k=uθ(j),k=vz(j),k=0,k,\displaystyle u^{\theta}_{(j),0}=v^{r}_{(j),k}=u^{\theta}_{(j),k}=v^{z}_{(j),k}=0,\quad\forall\ k\in\mathop{\mathbb{N}\kern 0.0pt}\nolimits,

i.e., 𝒖(j)\boldsymbol{u}_{(j)} has the following form

(5.7) 𝒖(j)=u(j),0r𝒆r+u(j),0z𝒆z+k=1(u(j),krcoskθ𝒆r+v(j),kθsinkθ𝒆θ+u(j),kzcoskθ𝒆z),\boldsymbol{u}_{(j)}=u^{r}_{(j),0}\boldsymbol{e}_{r}+u^{z}_{(j),0}\boldsymbol{e}_{z}+\sum_{k=1}^{\infty}\Bigl(u^{r}_{(j),k}\cos k\theta\boldsymbol{e}_{r}+v^{\theta}_{(j),k}\sin k\theta\boldsymbol{e}_{\theta}+u^{z}_{(j),k}\cos k\theta\boldsymbol{e}_{z}\Bigr),

then our aim is to show that 𝒖(n)\boldsymbol{u}_{(n)} can also be written as this form, i.e.

uθ(n),0=vr(n),k=uθ(n),k=vz(n),k=0,k,\displaystyle u^{\theta}_{(n),0}=v^{r}_{(n),k}=u^{\theta}_{(n),k}=v^{z}_{(n),k}=0,\quad\forall\ k\in\mathop{\mathbb{N}\kern 0.0pt}\nolimits,

Indeed, due to Remark 4.1, we know that in the Euclidean coordinates, 𝒖(n)\boldsymbol{u}_{(n)} satisfies

(5.8) {t𝒖(n)+𝒖(0)𝒖(n)+𝒖(n)𝒖(0)Δ𝒖(n)+P(n)=j=1n1𝒖(j)𝒖(nj),div𝒖(n)=0,𝒖(n)|t=0=0.\left\{\begin{aligned} &\partial_{t}\boldsymbol{u}_{(n)}+\boldsymbol{u}_{(0)}\cdot\nabla\boldsymbol{u}_{(n)}+\boldsymbol{u}_{(n)}\cdot\nabla\boldsymbol{u}_{(0)}-\Delta\boldsymbol{u}_{(n)}+\nabla P_{(n)}=-\sum_{j=1}^{n-1}\boldsymbol{u}_{(j)}\cdot\nabla\boldsymbol{u}_{(n-j)},\\ &\mathop{\rm div}\nolimits\boldsymbol{u}_{(n)}=0,\\ &\boldsymbol{u}_{(n)}|_{t=0}=0.\end{aligned}\right.

This system has zero-valued initial data. However, due to the external force term j=1n1𝒖(j)𝒖(nj)-\sum_{j=1}^{n-1}\boldsymbol{u}_{(j)}\cdot\nabla\boldsymbol{u}_{(n-j)}, the solution 𝒖(n)\boldsymbol{u}_{(n)} in general does not vanish.

Noticing that 𝒖(j)\boldsymbol{u}_{(j)} has the form (5.7) for 1jn11\leq j\leq n-1, we can get

(5.9) 𝒖(j)𝒖(nj)=k1,k2=0{(ur(j),k1r+uz(j),k1z)(ur(nj),k2𝒆r+uz(nj),k2𝒆z)cosk1θcosk2θ+(ur(j),k1r+uz(j),kz)vθ(nj),k2𝒆θcosk1θsink2θ+v(j),k1θu(nj),k2rr(𝒆rk2sink1θsink2θ+𝒆θsink1θcosk2θ)+v(j),k1θv(nj),k2θr(𝒆θk2sink1θcosk2θ𝒆rsink1θsink2θ)}.\begin{split}\boldsymbol{u}_{(j)}\cdot\nabla\boldsymbol{u}_{(n-j)}=&\sum_{k_{1},k_{2}=0}^{\infty}\Bigl\{(u^{r}_{(j),k_{1}}\partial_{r}+u^{z}_{(j),k_{1}}\partial_{z})\bigl(u^{r}_{(n-j),k_{2}}\boldsymbol{e}_{r}+u^{z}_{(n-j),k_{2}}\boldsymbol{e}_{z}\bigr)\cdot\cos k_{1}\theta\cdot\cos k_{2}\theta\\ &\quad+(u^{r}_{(j),k_{1}}\partial_{r}+u^{z}_{(j),k}\partial_{z})v^{\theta}_{(n-j),k_{2}}\boldsymbol{e}_{\theta}\cdot\cos k_{1}\theta\cdot\sin k_{2}\theta\\ &\quad+\frac{v^{\theta}_{(j),k_{1}}u^{r}_{(n-j),k_{2}}}{r}\bigl(-\boldsymbol{e}_{r}k_{2}\sin k_{1}\theta\cdot\sin k_{2}\theta+\boldsymbol{e}_{\theta}\sin k_{1}\theta\cdot\cos k_{2}\theta\bigr)\\ &\quad+\frac{v^{\theta}_{(j),k_{1}}v^{\theta}_{(n-j),k_{2}}}{r}\bigl(\boldsymbol{e}_{\theta}k_{2}\sin k_{1}\theta\cdot\cos k_{2}\theta-\boldsymbol{e}_{r}\sin k_{1}\theta\cdot\sin k_{2}\theta\bigr)\Bigr\}.\end{split}

In particular, we can see that (𝒖(j)𝒖(nj))𝒆r(\boldsymbol{u}_{(j)}\cdot\nabla\boldsymbol{u}_{(n-j)})\cdot\boldsymbol{e}_{r} and (𝒖(j)𝒖(nj))𝒆z(\boldsymbol{u}_{(j)}\cdot\nabla\boldsymbol{u}_{(n-j)})\cdot\boldsymbol{e}_{z} is even in θ\theta, while (𝒖(j)𝒖(nj))𝒆θ(\boldsymbol{u}_{(j)}\cdot\nabla\boldsymbol{u}_{(n-j)})\cdot\boldsymbol{e}_{\theta} is odd in θ\theta. As a result, this external force j=1n1𝒖(j)𝒖(nj)-\sum_{j=1}^{n-1}\boldsymbol{u}_{(j)}\cdot\nabla\boldsymbol{u}_{(n-j)} does not appear in the equations for (v(n),kr,u(n),kθ,v(n),kz)(v^{r}_{(n),k},u^{\theta}_{(n),k},v^{z}_{(n),k}) for k1k\geq 1. Thus the equations for (v(n),kr,u(n),kθ,v(n),kz)(v^{r}_{(n),k},u^{\theta}_{(n),k},v^{z}_{(n),k}) are exactly the same as that for (v(1),kr,u(1),kθ,v(1),kz)(v^{r}_{(1),k},u^{\theta}_{(1),k},v^{z}_{(1),k}) (see (5.4)) stated as follows:

{tvr(n),k+(ur(0),0r+uz(0),0z)vr(n),k+(vr(n),kr+vz(n),kz)ur(0),0(r2+z2+1rr1+k2r2)vr(n),k2ku(n),kθr2+rQ(n),k=0,tuθ(n),k+(ur(0),0r+uz(0),0z)uθ(n),k+u(0),0ru(n),kθr(r2+z2+1rr1+k2r2)uθ(n),k2kv(n),krr2+krQ(n),k=0,tvz(n),k+(ur(0),0r+uz(0),0z)vz(n),k+(vr(n),kr+vz(n),kz)uz(0),0(r2+z2+1rrk2r2)vz(n),k+zQ(n),k=0,rv(n),kr+1rv(n),kr+zv(n),kzkru(n),kθ=0,vr(n),k|t=0=0,uθ(n),k|t=0=0,vz(n),k|t=0=0.\left\{\begin{aligned} &\partial_{t}v^{r}_{(n),k}+(u^{r}_{(0),0}\partial_{r}+u^{z}_{(0),0}\partial_{z})v^{r}_{(n),k}+(v^{r}_{(n),k}\partial_{r}+v^{z}_{(n),k}\partial_{z})u^{r}_{(0),0}\\ &\qquad\qquad\qquad-(\partial_{r}^{2}+\partial_{z}^{2}+\frac{1}{r}\partial_{r}-\frac{1+k^{2}}{r^{2}})v^{r}_{(n),k}-2k\frac{u^{\theta}_{(n),k}}{r^{2}}+\partial_{r}Q_{(n),k}=0,\\ &\partial_{t}u^{\theta}_{(n),k}+(u^{r}_{(0),0}\partial_{r}+u^{z}_{(0),0}\partial_{z})u^{\theta}_{(n),k}+\frac{u^{r}_{(0),0}u^{\theta}_{(n),k}}{r}\\ &\qquad\qquad\qquad-(\partial_{r}^{2}+\partial_{z}^{2}+\frac{1}{r}\partial_{r}-\frac{1+k^{2}}{r^{2}})u^{\theta}_{(n),k}-2k\frac{v^{r}_{(n),k}}{r^{2}}+\frac{k}{r}Q_{(n),k}=0,\\ &\partial_{t}v^{z}_{(n),k}+(u^{r}_{(0),0}\partial_{r}+u^{z}_{(0),0}\partial_{z})v^{z}_{(n),k}+(v^{r}_{(n),k}\partial_{r}+v^{z}_{(n),k}\partial_{z})u^{z}_{(0),0}\\ &\qquad\qquad\qquad-(\partial_{r}^{2}+\partial_{z}^{2}+\frac{1}{r}\partial_{r}-\frac{k^{2}}{r^{2}})v^{z}_{(n),k}+\partial_{z}Q_{(n),k}=0,\\ &\partial_{r}v^{r}_{(n),k}+\frac{1}{r}v^{r}_{(n),k}+\partial_{z}v^{z}_{(n),k}-\frac{k}{r}u^{\theta}_{(n),k}=0,\\ &v^{r}_{(n),k}|_{t=0}=0,\quad u^{\theta}_{(n),k}|_{t=0}=0,\quad v^{z}_{(n),k}|_{t=0}=0.\end{aligned}\right.

Then the same procedure as what we have done at the end of Subsection 5.2 shows that for k1k\geq 1, (v(n),kr,u(n),kθ,v(n),kz)(v^{r}_{(n),k},u^{\theta}_{(n),k},v^{z}_{(n),k}) indeed vanishes for all time, i.e.

v(n),kr=u(n),kθ=v(n),kz=0,t>0.\displaystyle v^{r}_{(n),k}=u^{\theta}_{(n),k}=v^{z}_{(n),k}=0,\quad\forall\ t>0.

Let us turn to study the 00-th Fourier coefficients u(n),0r𝒆r+u(n),0θ𝒆θ+u(n),0z𝒆zu^{r}_{(n),0}\boldsymbol{e}_{r}+u^{\theta}_{(n),0}\boldsymbol{e}_{\theta}+u^{z}_{(n),0}\boldsymbol{e}_{z}. In view of the expression (5.9), and the following identities

2cosk1θcosk2θ=cos(k1+k2)θ+cos(k1k2)θ,\displaystyle 2\cos k_{1}\theta\cdot\cos k_{2}\theta=\cos(k_{1}+k_{2})\theta+\cos(k_{1}-k_{2})\theta,
2sink1θsink2θ=cos(k1k2)θcos(k1+k2)θ,\displaystyle 2\sin k_{1}\theta\cdot\sin k_{2}\theta=\cos(k_{1}-k_{2})\theta-\cos(k_{1}+k_{2})\theta,
2sink1θcosk2θ=sin(k1+k2)θ+sin(k1k2)θ,\displaystyle 2\sin k_{1}\theta\cdot\cos k_{2}\theta=\sin(k_{1}+k_{2})\theta+\sin(k_{1}-k_{2})\theta,

and the fact that 𝒖(0)=u(0),0r𝒆r+u(0),0z𝒆z\boldsymbol{u}_{(0)}=u^{r}_{(0),0}\boldsymbol{e}_{r}+u^{z}_{(0),0}\boldsymbol{e}_{z} is axisymmetric without swirl, we can obtain

(5.10) tu(n),0θ+𝒖(0)u(n),0θ+u(0),0ru(n),0θr(Δ1r2)u(n),0θ=0,u(n),0θ|t=0=0,\partial_{t}u^{\theta}_{(n),0}+\boldsymbol{u}_{(0)}\cdot\nabla u^{\theta}_{(n),0}+\frac{u^{r}_{(0),0}u^{\theta}_{(n),0}}{r}-(\Delta-\frac{1}{r^{2}})u^{\theta}_{(n),0}=0,\quad u^{\theta}_{(n),0}|_{t=0}=0,

and

(5.11) {tur(n),0+𝒖(0)ur(n),0+(ur(n),0r+uz(n),0z)ur(0),0(Δ1r2)u(n),0r+rP(n),0=F(n),0r,tuz(n),0+𝒖(0)uz(n),0+(ur(n),0r+uz(n),0z)uz(0),0Δuz(n),0+zP(n),0=Fz(n),0,ru(n),0r+1ru(n),0r+zu(n),0z=0,ur(n),0|t=0=0,uz(n),0|t=0=0,\left\{\begin{aligned} &\partial_{t}u^{r}_{(n),0}+\boldsymbol{u}_{(0)}\cdot\nabla u^{r}_{(n),0}+(u^{r}_{(n),0}\partial_{r}+u^{z}_{(n),0}\partial_{z})u^{r}_{(0),0}\\ &\qquad\qquad\qquad\qquad\qquad\qquad-(\Delta-\frac{1}{r^{2}})u^{r}_{(n),0}+\partial_{r}P_{(n),0}=F^{r}_{(n),0},\\ &\partial_{t}u^{z}_{(n),0}+\boldsymbol{u}_{(0)}\cdot\nabla u^{z}_{(n),0}+(u^{r}_{(n),0}\partial_{r}+u^{z}_{(n),0}\partial_{z})u^{z}_{(0),0}-\Delta u^{z}_{(n),0}+\partial_{z}P_{(n),0}=F^{z}_{(n),0},\\ &\partial_{r}u^{r}_{(n),0}+\frac{1}{r}u^{r}_{(n),0}+\partial_{z}u^{z}_{(n),0}=0,\\ &u^{r}_{(n),0}|_{t=0}=0,\quad u^{z}_{(n),0}|_{t=0}=0,\end{aligned}\right.

where F(n),0r,F(n),0zF^{r}_{(n),0},~F^{z}_{(n),0} are the external force terms given by

F(n),0r=12\displaystyle F^{r}_{(n),0}=-\frac{1}{2} k=1j=1n1(u(j),krr+u(j),kzz)u(nj),kr+12k=1j=1n1v(j),kθv(nj),kθr,\displaystyle\sum_{k=1}^{\infty}\sum_{j=1}^{n-1}\bigl(u^{r}_{(j),k}\partial_{r}+u^{z}_{(j),k}\partial_{z}\bigr)u^{r}_{(n-j),k}+\frac{1}{2}\sum_{k=1}^{\infty}\sum_{j=1}^{n-1}\frac{v^{\theta}_{(j),k}v^{\theta}_{(n-j),k}}{r},
F(n),0z=12k=1j=1n1(u(j),krr+u(j),kzz)u(nj),kz.\displaystyle F^{z}_{(n),0}=-\frac{1}{2}\sum_{k=1}^{\infty}\sum_{j=1}^{n-1}\bigl(u^{r}_{(j),k}\partial_{r}+u^{z}_{(j),k}\partial_{z}\bigr)u^{z}_{(n-j),k}.

In particular, this reflects the fact that if two profiles have same frequency, then their product would contribute to the average of 𝒖\boldsymbol{u} in θ\theta variable.

Taking L2L^{2} inner product of (5.10) with u(n),0θu^{\theta}_{(n),0}, it is easy to get that

u(n),0θ=0,t>0.\displaystyle u^{\theta}_{(n),0}=0,\quad\forall\ t>0.

Therefore, 𝒖(n)\boldsymbol{u}_{(n)} can also be written in the following form:

𝒖(n)=u(n),0r𝒆r+u(n),0z𝒆z+k=1(u(n),krcoskθ𝒆r+v(n),kθsinkθ𝒆θ+u(n),kzcoskθ𝒆z).\boldsymbol{u}_{(n)}=u^{r}_{(n),0}\boldsymbol{e}_{r}+u^{z}_{(n),0}\boldsymbol{e}_{z}+\sum_{k=1}^{\infty}\Bigl(u^{r}_{(n),k}\cos k\theta\boldsymbol{e}_{r}+v^{\theta}_{(n),k}\sin k\theta\boldsymbol{e}_{\theta}+u^{z}_{(n),k}\cos k\theta\boldsymbol{e}_{z}\Bigr).

This completes the proof of Theorem 1.3 by induction.

Acknowledgments. Y. Liu is supported by NSF of China under grant 12101053, and the Fundamental Research Funds for the Central Universities under Grant 310421118. L. Xu is supported by NSF of China under grant 11671383 and 12171019.

References

  • [1] D. Chae and J. Lee, On the regularity of the axisymmetric solutions of the Navier-Stokes equations, Math. Z. 239 (2002), 645–671.
  • [2] C.-C. Chen, R. Strain, H.-T. Yau and T.-P. Tsai, Lower bound on the blow-up rate of the axisymmetric Navier-Stokes equations. Int. Math. Res. Not. IMRN 2008, no. 9, Art. ID rnn016, 31 pp.
  • [3] C.-C. Chen, R. Strain, T.-P. Tsai and H.-T. Yau, Lower bounds on the blow-up rate of the axisymmetric Navier-Stokes equations. II. Comm. Partial Differential Equations 34 (2009), no. 1-3, 203–232.
  • [4] H. Chen, D. Fang and T. Zhang, Regularity of 3D axisymmetric Navier-Stokes equations. Discrete Contin. Dyn. Syst. 37 (2017), no. 4, 1923–1939.
  • [5] I. Gallagher, D. Iftimie and F. Planchon, Asymptotics and stability for global solutions to the Navier-Stokes equations. Ann. Inst. Fourier (Grenoble) 53 (2003), no. 5, 1387–1424.
  • [6] O. A. Ladyzhenskaja, Unique global solvability of the three-dimensional Cauchy problem for the Navier-Stokes equations in the presence of axial symmetry, (Russian) Zap. Naučn. Sem. Leningrad. Otdel. Mat. Inst. Steklov. (LOMI), 7 (1968), 155–177.
  • [7] Z. Lei and Q. S. Zhang, Criticality of the axially symmetric Navier-Stokes equations. Pacific J. Math. 289 (2017), no. 1, 169–187.
  • [8] S. Leonardi, J. Málek, J. Nečas and M. Pokorny, On axially symmetric flows in 3,\mathbb{R}^{3}, Z. Anal. Anwendungen, 18 (1999), 639–649.
  • [9] Y. Liu and P. Zhang, On the global well-posedness of 3-D axi-symmetric Navier-Stokes system with small swirl component. Calc. Var. Partial Differential Equations 57 (2018), no. 1, Paper No. 17, 31 pp.
  • [10] G. Ponce, R. Racke, T. C. Sideris, E. S. Titi, Global stability of large solutions to the 3D Navier-Stokes equations. Comm. Math. Phys. 159 (1994), no. 2, 329–341.
  • [11] M. R. Ukhovskii and V. I. Yudovich, Axially symmetric flows of ideal and viscous fluids filling the whole space, J. Appl. Math. Mech. 32 (1968) 52–61.
  • [12] D. Wei, Regularity criterion to the axially symmetric Navier-Stokes equations. J. Math. Anal. Appl. 435 (2016), no. 1, 402–413.
  • [13] P. Zhang and T. Zhang, Global axisymmetric solutions to three-dimensional Navier-Stokes System, Int. Math. Res. Not. IMRN, 2014, No. 3, 610–642.