\input amstex \documentstyle{amsppt} \loadmsbm \magnification=\magstephalf \hcorrection{1cm} \vcorrection{-6mm} \nologo \TagsOnRight \NoBlackBoxes \headline={\ifnum\pageno=1 \hfill\else% {\tenrm\ifodd\pageno\rightheadline \else \leftheadline\fi}\fi} \def\rightheadline{EJDE--1998/26\hfil Existence of axisymmetric weak solutions \hfil\folio} \def\leftheadline{\folio\hfil Dongho Chae \& Oleg Yu Imanuvilov \hfil EJDE--1998/26} \def\pretitle{\vbox{\eightrm\noindent\baselineskip 9pt % Electronic Journal of Differential Equations, Vol.\ {\eightbf 1998}(1998), No.~26, pp.~1--17.\hfil\break ISSN: 1072-6691. URL: http://ejde.math.swt.edu or http://ejde.math.unt.edu \hfill\break ftp (login: ftp) 147.26.103.110 or 129.120.3.113\bigskip} } \topmatter \title Existence of axisymmetric weak solutions of the 3-D Euler equations for near-vortex-sheet initial data \endtitle \thanks {\it 1991 Mathematics Subject Classifications:} 35Q35, 76C05.\hfil\break\indent {\it Key words and phrases:} Euler equations, axisymmetry, weak solution. \hfil\break\indent \copyright 1998 Southwest Texas State University and University of North Texas.\hfil\break\indent Submitted October 9, 1998. Published October 15, 1998.\hfil\break\indent Partially supported by GARC-KOSEF, BSRI-MOE, KOSEF(K950701), KIAS-M97003, \hfil\break\indent and the SNU Research Fund. \endthanks \author Dongho Chae \& Oleg Yu Imanuvilov\endauthor \address Dongho Chae\hfil\break Department of Mathematics, Seoul National University,\hfil\break Seoul 151-742, Korea \endaddress \email dhchae\@math.snu.ac.kr \endemail \address Oleg Yu Imanuvilov \hfil\break Korean Institute for Advanced Study, \hfil\break 207-43 Chungryangri-dong Dongdaemoon-ku, Seoul, Korea \endaddress \email oleg\@kias.kaist.ac.kr\endemail \abstract We study the initial value problem for the 3-D Euler equation when the fluid is inviscid and incompressible, and flows with axisymmetry and without swirl. On the initial vorticity $\omega_0$, we assumed that $\omega_0/r$ belongs to $L(\log L (\Bbb R^3))^{\alpha}$ with $\alpha >1/2$, where $r$ is the distance to an axis of symmetry. To prove the existence of weak global solutions, we prove first a new {\it a priori} estimate for the solution. \endabstract \endtopmatter \document \head Introduction \endhead We consider the Euler equations for homogeneous inviscid incompressible fluid flow in ${\Bbb R}^3$ $$ \gather \frac{\partial v}{\partial t}+ (v\cdot \nabla)v=-\nabla p\, , \quad \,\,\text{div}\,v =0 \,\,\quad \text{in}\,\, {\Bbb R}_+ \times {\Bbb R}^3\,, \tag 1 \\ v(0,\cdot)=v_0\,,\tag 2 \endgather $$ where $v(t,x)=(v_1(t,x),v_2(t,x),v_3(t,x))$ is the velocity of the fluid flow and $p(t,x)$ is the pressure. The problem of finite-time breakdown of smooth solutions to (1)-(2) for smooth initial data is a longstanding open problem in mathematical fluid mechanics. (See [6,13,14] for a detailed discussion of this problem.) The situation is similar even for the case of axisymmetry (see e.g.[11], [4]). In the case of axisymmetry without swirl velocity ($\theta$-component of velocity), however, we have a global unique smooth solution for smooth initial data [14,17]. In this case a crucial role is played by the fact that $\omega_\theta (t,x)/r$ (where $\omega =\text{curl}\, v$, $r={\sqrt{x_1 ^2 +x_2 ^2}}$) is preserved along the flow, and the problem looks similar to that of the 2-D Euler equations. This apparent similarity between the axisymmetric 3-D flow without swirl and the 2-D flow for smooth initial data breaks down for nonsmooth initial data. In particular, Delort [8] found the very interesting phenomenon that for a sequence of approximate solutions to the axisymmetric 3-D Euler equations with nonnegative vortex-sheet initial data, either the sequence converges strongly in $L^2 _{\text{loc}} ([0,\infty )\times {\Bbb R}^3 )$, or the weak limit of the sequence is not a weak solution of the equations. This is in contrast with Delort's proof of the existence of weak solutions for the 2-D Euler equations with the single-signed vortex-sheet initial data, where we have weak convergence for the approximate solution sequence. Due to the subtle concentration cancellation type of phenomena in the nonlinear term, the weak limit itself becomes a weak solution [7,10,15]. We refer to [13, Section 4.3] for an illuminating discussion on the differences between the the quasi 2-D Euler equations and the ``pure" 2-D Euler equations for weak initial data. In this paper we prove existence of weak solutions to (1)-(2) for the axisymmetric initial data without swirl in which the vorticity satisfies $$\left\vert \frac{\omega_{0}}{r}\right\vert \left[1+ \left(\log^+ \left\vert\frac{\omega_{0}} {r}\right\vert\right)^{\alpha} \right] \in L^1({\Bbb R}^3), \quad \alpha > \frac{1}{2}\,, $$ where $\log^+ t=\max\{ 0, \log t\}$. The idea of proof is as follows. We divide ${\Bbb R}^3$ into two parts: the region near the axis of symmetry, and the region away from the axis. For the latter region, using the 2-D structure of the equations expressed in cylindrical coordinate system, we obtain strong compactness for the approximate solution sequence using arguments previously used in the 2-D problem in [3]. For the region near axis, we could not adapt the previous 2-D arguments. See the next section for explicit comparison between the nonlinear terms in the pure 2-D Euler case and our case. Here we use a new {\it a priori} estimate for the axisymmetric flow, combined with Delort's argument in [8] to overcome these difficulties. To the authors' knowledge this {\it a priori} estimate (See Lemma 2.1) is completely new for the 3-D Euler equations with axisymmetry. On the other hand, the results obtained in this paper improve substantially the results in [5], where the authors proved existence of weak solutions for $$ \left\vert \frac{\omega_{0}}{r}\right\vert \in L^1 ({\Bbb R}^3) \cap L^{p}({\Bbb R}^3), \quad p > \frac{6}{5}\,. $$ It would be very interesting to study (1)-(2) with initial data in $L^1 ({\Bbb R}^3 )$. \heading 1. Preliminaries \endheading By a weak solution of the Euler equations with an initial data $v_0$, we mean the vector field $v\in L^{\infty}([0,T]; (L^2 _{\text{loc}} ({\Bbb R}^3))^3)$ with $\text{div}\, v=0$ such that $$ \int_0^T\!\!\int_{{\Bbb R}^3}[ v\cdot \varphi _t +v\otimes v : \nabla \varphi ]\, dx\,dt+\int_{{\Bbb R}^3}v_0 \cdot \varphi (0,x)\,dx=0\,, $$ for all $\varphi \in C^\infty([0,T];[C^\infty_0({\Bbb R}^3)]^3)$ with $ \text{div}\,\varphi\equiv 0$ and $\varphi (T,x)\equiv 0$ Here we have used the notation $v\otimes v : \nabla \varphi =\sum _{i,j =1} ^3 v_i v_j (\varphi _i )_{x_j}$. We are concerned with the axisymmetric solutions to the Euler equations. By an axisymmetric solution of equations (1)-(2) we mean a solution of the form $$ v(t,x)=v_r(r,x_3,t)e_r+v_\theta(r,x_3,t)e_\theta+v_3(r,x_3,t)e_3 $$ in the cylindrical coordinate system, using the canonical basis $$ e_r=(\frac{x_1}{r},\frac{x_2}{r},0),\quad e_\theta=(\frac{x_2}{r}, -\frac{x_1}{r},0), \quad e_3=(0,0,1), r=\sqrt{x^2_1+x^2_2}\,. $$ For such flows the first equation in (1) can be written as $$ \gather \frac{\tilde{D} v_r}{D t} -\frac{(v_{\theta}) ^2}{r} = -\frac{\partial p}{\partial r}\,, \tag 3 \\ \frac{\tilde{D}}{D t}(r v_{\theta}) =0\,, \tag 4 \\ \frac{\tilde{D} v_3}{\partial t} = -\frac{\partial p}{\partial x_3}\,, \tag 5 \endgather $$ for each component of velocity in the cylindrical coordinate system, where $$ \frac{\tilde{D}}{Dt} =\frac{\partial}{\partial t} + v_r \frac{\partial}{\partial r} + v_3 \frac{\partial}{\partial x_3}\,. $$ On the other hand, the second equation of (1) becomes $$ \frac{\partial}{\partial r}(r v_r ) +\frac{\partial}{\partial x_3} (r v_3 ) =0\,. \tag 6 $$ We observe that $\theta$-component of the vorticity equation is written as $$ \frac{\tilde{D}}{Dt} \left( \frac{\omega _{\theta}}{r} \right) =\frac{1}{r^4} \frac{\partial}{\partial x_3 } ( r v_{\theta} )^2 \,, \tag 7 $$ where $$ \omega _{\theta} = \frac{\partial v_r}{\partial x_3} - \frac{\partial v_3}{\partial r} \tag 8 $$ is the $\theta -$component of the vorticity vector $\omega$. If we assume that the initial velocity $$ v_0 \in V^m =\{ v\in [\text{ H}^m ({\Bbb R}^3 )]^3 : \ \text{div} \ v =0 \} $$ with $m\geq 4$ is axisymmetric, then due to the symmetry properties of the Euler equations, and by the existence of local unique classical solutions [12], the solution remains axisymmetric during its existence. Here we used the standard Sobolev space $$ \text{H}^{m}({\Bbb R}^3)=\{u \in L^2({\Bbb R}^3 )\, : \, D^\alpha u\in L^2({\Bbb R}^3), \,\,\vert\alpha \vert\le m\}\,. $$ Furthermore, if $v_0$ has no \lq\lq swirl" component, i.e. $v_{0,\theta}$=0, then (4) and (7) imply that $$ \frac{\tilde{D}}{Dt} \left( \frac{\omega _{\theta}}{r} \right) =0 \quad \forall t>0\,. \tag 9 $$ We observe that in this case the vorticity becomes $\omega (t,x)=\omega_\theta (t, r, x_3 ) e_\theta$. Thus, we have, in particular, $$ |\omega (t,x) | = |\omega_\theta (t, r, x_3 )|\,, $$ where $|\cdot |$ denotes the Euclidean norm in ${\Bbb R}^3$ in the left hand side, and the absolute value in the right hand side of the equation. In [17] Saint-Raymond proved existence of a global unique smooth solution for smooth $v_0$ without swirl. Below we show explicitly the difference between the nonlinear terms for the 2-D Euler equations and those for 3-D Euler equations with axisymmetry and without swirl. In the weak formulation of the 2-D Euler equations, if we use a test function of the form $\varphi =(-\frac{\partial \psi}{\partial x_2} , \frac{\partial \psi}{\partial x_1} )$ in order to satisfy $\text{div}\,\varphi =0$, then $$ \int _0 ^T\!\!\int _{{{\Bbb R}^2}}[ v\otimes v : \nabla \varphi ] \,dx\,dt = \int _0^T\!\!\int _{{{\Bbb R}^2}} \left[(v_1 ^2 -v_2 ^2 )\frac{\partial ^2 \psi}{\partial x_1\partial x_2} -v_1 v_2 \left(\frac{\partial ^2 \psi}{\partial x_1 ^2}- \frac{\partial ^2 \psi}{\partial x_2 ^2} \right)\right]\,dx\,dt\,. $$ On the other hand, in the axisymmetric 3-D Euler equation without swirl, if we use as a test function $\varphi (t, x) =\varphi _r(t, r, x_3)e_r + \varphi _3(t, r, x_3)e_3$ with $$ \varphi _r =\frac{1}{r}\frac{\partial \psi}{\partial x_3}, \ \ \varphi _3 =-\frac{1}{r}\frac{\partial \psi}{\partial r} $$ to satisfy $\frac{\partial(r \varphi _r )}{\partial r} + \frac{\partial(r\varphi _3 )}{ \partial x_3} =0$, then $$ \align \int _0 ^T\!\!\int _{{{\Bbb R}}^3} [v\otimes v : \nabla \varphi ] \,dx\,dt = 2\pi \int _0 ^T\!\!\int _{{\Bbb R}\times {\Bbb R}_+} \bigg[&(v_r ^2 -v_3 ^2 )\frac{\partial ^2 \psi}{\partial r \partial x_3} -v_r v_3\left (\frac{\partial ^2 \psi}{\partial r ^2}- \frac{\partial ^2 \psi}{\partial x_3 ^2}\right ) \\ &+ \frac{v_r v_3}{r} \frac{\partial \psi}{\partial r} -\frac{v_r ^2}{r} \frac{\partial \psi}{\partial x_3}\bigg]\,dr\,dx_3\, dt \,. \endalign $$ Here we have extra two nonlinear terms compared to the 2-D case, which have apparent singularities on the axis of symmetry. Before closing this section, we provide a brief introduction to the Orlicz spaces. For more details see [1,9], and for applications to the 2-D Euler equations, see [3,16]. By an N-function we mean a real valued function $A(t)$, $t\geq 0$ which is continuous, increasing, convex, and satisfies $$ \lim_{t\rightarrow 0} \frac{A(t)}{t} =0,\quad \lim_{t\rightarrow \infty} \frac{A(t)}{t}=+\infty \,. $$ We say that $A(t)$ satisfies $\Delta_2 $-condition near infinity if there exist $k>0$, $t_0 \geq 0$ such that $$ A(2t)\leq k A(t) \ \ \ \forall t \geq t_0\,. $$ We denote $A(t)\succ B(t)$ if for every $k>0$ $$ \lim_{t\rightarrow \infty} \frac{A(kt)}{B(t)} =\infty\,. $$ Let $\Omega $ be a domain in ${\Bbb R}^n$. Then the Orlicz class $K_A (\Omega )$ is defined as the set all functions $u$ such that $\int_{\Omega} A(| u(x) |) \,dx <\infty$. On the other hand, the Orlicz space $L_A (\Omega )$ is defined as the linear hull of the Orlicz class $K_A (\Omega )$. The set $L_A (\Omega )$ is a Banach space equipped with the Luxembourg norm $$ \Vert u \Vert_A =\inf\big\{k : \int_{\Omega} A(\frac{u}{k} )\,dx \leq 1 \big\}\,. $$ In general $K_A (\Omega ) \subset L_A (\Omega )$, but in case the domain $\Omega$ is bounded in ${\Bbb R}^n$, and the N-function $A$ satisfies the $\Delta _2 $-condition near infinity we have $K_A (\Omega ) = L_A (\Omega )$ (see [1]). For example $L^p (\Omega ), \ 1
0$. Let $A(\cdot), B(\cdot )$ be N-functions given by
$A(t)=t(\log^+ t)^{\alpha}$, $B(t)=\exp(t^{q/\alpha} ) -1$,
where $t\geq 0$. Then, we have
$$
L_B(\Omega )=L^*_A (\Omega )\,.
$$
\endproclaim
By the Orlicz-Sobolev space $W^m L_A (\Omega )$ we mean a subspace
of the Orlicz space $L_A (\Omega )$ consisting of functions $u$
such that the distributional derivatives
$D^{\alpha} u$ are contained in $L_A (\Omega )$ for all multi-index
$\alpha$'
with $|\alpha | \leq m$, equipped with a Banach space norm
$$
\| u\| _{m,A}
= \max_{\vert\alpha\vert\le m} \| D^{\alpha } u \| _A \, .
$$
The following lemma corresponds to a special case of the general result
by Donaldson and Trudinger [9].
\proclaim{Lemma 1.2}
Let $\Omega \subset {\Bbb R}^2$ be a bounded domain,
and $B(t)=\exp(t^2)-1$, then we have a continuous imbedding
$$
H^1_0(\Omega)\hookrightarrow L_B(\Omega ).
$$
Moreover, for any N-function $A(t)$ with $A(t)\prec B(t)$ we have a compact imbedding
$$
H^1_0(\Omega)\hookrightarrow \hookrightarrow L_A(\Omega ).
$$
\endproclaim
Combining dual of the compact imbedding in Lemma 1.2, and Lemma 1.1 we have
\proclaim{Corollary 1.1} Let $\Omega\subset {\Bbb R}^2$ be a bounded domain
and $A(t)=t(\log^+ t)^{\alpha}$ with $\alpha > \frac12$. Then we have the
compact imbedding
$$
L_A(\Omega)\hookrightarrow\hookrightarrow \text{H}^{-1}(\Omega).
$$
\endproclaim
\heading 2. Main Results \endheading
Our main result is as follows:
\proclaim {Theorem 2.1} Suppose $\alpha > \frac{1}{2}$ is given.
Let $v_0\in V^0 $ be an axisymmetric initial data
with $v_{0,\theta}\equiv 0,$ and
$\vert \frac{\omega_{0}}{r}\vert \left[1+ (\log^+
\vert\frac{\omega_{0}}{r}\vert)^{\alpha} \right] \in L^1({\Bbb R}^3)$.
Then there exists a weak solution of problem
(1)-(2). Moreover, the solution satisfies
$$
\| v(t,\cdot)\|_{V^0} \leq \|v_0 \|_{V^0},
$$
and
$$
\int_{{\Bbb R}^3} \left\vert \frac{\omega (t,\cdot)}{r}\right\vert \left[1+ \left( \log^+
\left\vert\frac{\omega (t,\cdot)}{r}\right\vert \right)^{\alpha} \right]\, dx \leq
\int_{{\Bbb R}^3} \left\vert \frac{\omega_{0}}{r}\right\vert \left[1+ \left(\log^+
\left\vert\frac{\omega_{0}}{r}\right\vert \right)^{\alpha} \right]\, dx
$$
for almost every $t\in [0, \infty)$.
\endproclaim
In this section our aim is to prove the above theorem.
Below we denote
$$
Q=[0,T]\times {\Bbb R}^3 , \quad G=\{ (r, x_3 )\in {\Bbb R}^2 \, |\, r>0,
x_3 \in {\Bbb R} \}.
$$
We start from establishment of the following a priori estimate.
\proclaim{Lemma 2.1} Let $v(t,x)\in C([0,T];[C^1(\overline{{\Bbb R}^3})\bigcap
H^1({\Bbb R}^3)]^3)\bigcap C([0,T]; V^0) $
be the classical solution of the Euler equations for the axisymmetric initial
data $v_0$ without the swirl
component, and with the vorticity satisfying
$\frac{\omega_{0}}{r}\in L^1({\Bbb R}^3)$.
Then the following estimate holds:
$$
\int^T_0\!\!\int_{{\Bbb R}^3}\frac{1}{1+x^2_3}\left
(\frac{v_r}{r}\right)^2\,dx\,dt\le C\left(\Vert v_0\Vert_{
V^0}^2+\left\Vert \frac{\omega_{0}}{r}\right\Vert_{L^1({\Bbb R}^3)}\right)\,.
\tag 10
$$\endproclaim
\noindent{\bf Proof}. The velocity conservation law for the Euler equations
implies the estimate
$$
\Vert \sqrt{r} v_r\Vert_{L^\infty(0,T;L^2(G))}+\Vert \sqrt{r} v_3\Vert_{
L^\infty(0,T;L^2(G))}\le C\Vert v_0\Vert_{V^0}.\tag 11
$$
Moreover, (9) immediately yields the estimate for $L^1$-norm of vorticity
$$
\Vert \omega(t,\cdot)\Vert_{L^1(G)}
\le\Vert \omega_0\Vert_{L^1(G)}.
$$
We set $\rho(x_3)=\int^{x_3}_{-\infty} 1/(1+\tau^2)\, d\tau$.
Multiplying (9) by $2\pi r \rho (x_3)$ scalarly in \hfill\break
$L^2(0,T;L^2(G))$ and integrating by parts, we obtain
$$\aligned
0=&\int_{{\Bbb R}^3}\frac{\rho\omega_\theta}{r}\,dx\bigg\vert^T_0
-\int_0^T\!\!\int_{G}2\pi \rho' v_3 \omega_\theta \,dr\,dx_3\,dt \\
=&\int_{{\Bbb R}^3}\frac{\rho\omega_\theta}{r}dx\bigg\vert^T_0
+\int_0^T\!\!\int_G
2\pi \rho' v_3\left(\frac{\partial v_3}{\partial r}-\frac{\partial v_r}{
\partial x_3}\right)\,dr\,dx_3\,dt \\
=&\int_{{\Bbb R}^3}\frac{\rho\omega_\theta}{r}dx\bigg\vert^T_0
-\int_0^T\!\!\int^{+\infty}_{-\infty}\pi \rho' v^2_3(t,0,x_3)\,dx_3\,dt \\
&+\int_0^T\!\!\int_G 2\pi\left(\rho''v_3v_r+\rho' v_r\frac{\partial v_3}{
\partial x_3}\right)\,dr\,dx_3\,dt\,,\endaligned \tag 12
$$
where we used the regularity assumption of solution $v$, and the
integration by parts used above can be
justified easily. Indeed,
$$\align
\int_0^T\!\!\int_G &2\pi \rho' v_3\left(\frac{\partial v_3}{\partial r}-
\frac{\partial v_r}{\partial x_3}\right) \,dr\,dx_3\,dt\\
=&\lim_{r_k\rightarrow +\infty}2\pi\int_0^T\!\!\int^{+\infty}_{-\infty}\!\!
\int_0^{r_k} \rho'v_3\frac{\partial v_3}{\partial r}\,dr\,dx_3\,dt\\
&-\lim_{b_k\rightarrow +\infty}2 \pi \int_0^T \int_{-b_k}^{b_k}\int_0^{\infty}
\rho' v_3\frac{\partial v_r}{\partial x_3}\,dr\,dx_3\,dt\\
=&-\int_0^T\!\!\int^{+\infty}_{-\infty}\pi\rho'v^2_3(t,0,x_3)\,dx\,dt
+\lim_{r_k\rightarrow +\infty}\int_0^T\!\!\int^{+\infty}_{-\infty} \pi
\rho' v^2_3(t,r_k,x_3)\,dx_3\,dt\\
&-\lim_{b_k\rightarrow +\infty}
\int_0^T\!\!\int^\infty_0 2\pi \rho' v_3v_rdrdt\bigg\vert^{b_k}_{-b_k}\\
&+\lim_{b_k \rightarrow +\infty}\int_0^T\!\!\int^{b_k}_{-b_k}\int_0^\infty 2
\pi\left(\rho''v_3v_r+\rho' v_r\frac{\partial v_3}{
\partial x_3}\right)\,dr\,dx_3\,dt\,.
\endalign
$$
for all sequence $r_k\rightarrow +\infty$. Since
$v\in C([0,T];(C^1(\overline{R^3}))^3)$,
$$\align
\int_{(0,T)\times{\Bbb R}^3} \vert v\vert^2\,dx\,dt
=&2\pi \int_0^{+\infty}\left (\int_0^T\!\!\int_{-\infty}^{+\infty}
\vert v\vert^2\,dx_3\,dt\right)r\,dr \\
=&2\pi\int_{-\infty}^{\infty}\left(\int_0^T\!\!\int_0^{+\infty}
\vert v\vert^2r\,dr\,dt\right)\,dx_3< \infty \,,\endalign
$$
and $\lim_{x_3\rightarrow \infty} \rho'(x_3)=0$
one can find a sequence $r_k \rightarrow +\infty$ and $b_k\rightarrow +\infty$
such that
$$
\int_0^T\!\!\int_{-\infty}^{\infty} \rho' v^2_3(t,r_k,x_3) \,dx_3\,dt
\rightarrow 0,\quad \lim_{b_k\rightarrow +\infty}\int_0^T\!\!\int_0^\infty
2\pi\rho v_3v_r\,dt\,dr\bigg\vert^{b_k}_{-b_k}\rightarrow 0\,.
$$
From (6) we have
$$
\frac{\partial v_3}{\partial x_3}=-\frac{v_r}{r} -\frac{\partial v_r}{
\partial r}\,.\tag 13
$$
Therefore (12) and (13) imply
$$\multline
0=\int_{{\Bbb R}^3}\rho\frac{\omega_\theta}{r}dx\bigg\vert^T_0-\int_0^T\!\!\int^{+\infty}_{
-\infty} \pi\rho' v^2_3(t,0,x_3)\,dx_3\,dt\\
+\int_0^T\!\!\int_G 2\pi\left(\rho'' v_3v_r-\rho'\frac{(v_r)^2}{r}-\rho'v_r
\frac{\partial v_r}{\partial r}\right)\,dr\,dx_3\,dt\,. \endmultline\tag 14
$$
Since, by assumption, $v(t,x)$ is a smooth and axisymmetric vector field
$$
v_r(t,0,x_3)=0\quad \forall \,t\in {\Bbb R}^1_{+},\,\, x_3\in
{\Bbb R}^1.
$$
Thus integration by parts in (14), which can be justified similarly to the
above, implies
$$\multline
\int_0^T\!\!\int^{+\infty}_{-\infty}\pi\rho' v^2_3(t,0,x_3)\,dx_3\,dt+
\int_0^T\!\!\int_G 2 \pi\rho'(x_3) \frac{(v_r)^2}{r}\,dr\,dx_3\,dt\\
=\int_0^T\!\!\int_G2\pi \rho'' v_3 v_r \,dr\,dx_3\,dt+\int_{{\Bbb R}^3}
\rho\frac{\omega_\theta}{r}dx\bigg\vert^T_0\,.
\endmultline
$$
Since $\rho'(x_3)>0,\vert \rho(x_3)\vert