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Comparison between the Boussinesq and coupled Euler equations in two dimensions (Tosio Kato's Method and Principle for Evolution Equations in Mathematical Physics)

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Comparison between the Boussinesq and coupled

Euler

equations

in two

dimensions

Koji

Ohkitani

Research Institute

for

Mathematical

Sciences,

Kyoto University

ohkitani@kurims.kyoto-u.ac.jp

Dedicated

to the

memory of the late Professor Tosio Kato

Abstract

Amethod

of

successive

approximations is proposed

for

constructing asolution

of

the

ideal

tw0-dimensional

Boussinesq equations

on

the basis of

those

of

Euler equations.

Numerical experiments

on

the iteration scheme suggest that the coupled Euler

equa-tions approximate the Boussinesq equaequa-tions fairly well at the

fifth

iteration. The

fast

convergence of

the

successive

approximations is consistent with global regularity

of the Boussinesq equations,

as

long

as

the current

numerical results

are

concerned.

This

method will

serve as

asolid check in monitoring apossible singularity formation

numerically

at much higher spatial resolutions.

1

Introduction

In

1964 Professor

Tosio Kato published

an

elegant

paper

[1]

on

the global regularity

of the

tw0-dimensional

Euler equations subject to asmooth external forcing

$\frac{\partial u}{\partial t}+(u\cdot\nabla)u=-\nabla p+f$

,

(1)

$\nabla\cdot f=0$

.

(2)

Here

$u$

and

$p$

denote the velocity and the

pressure

and

$f$

is

an

external forcing

which

may

depend

on

space

and time. The incompressibility condition determines

the

pressure and

it has

the

following integral representation in

$\mathbb{R}^{2}$

$p= \frac{-1}{2\pi}\int_{\mathrm{R}^{2}}\frac{\partial u_{i}(y)}{\partial y_{j}}\frac{\partial u_{j}(y)}{\partial y_{i}}\log|x-y|dy$

,

(3)

which

can

be

obtained

by

solving

$\triangle p=-\frac{\partial u_{i}}{\partial x_{j}}\frac{\partial u_{j}}{\partial x_{i}}$

.

(4)

The vorticity

$\omega$

$=\partial_{1}u_{2}-\partial_{2}u_{1}$

obeys

$\frac{\partial\omega}{\partial t}+(u\cdot\nabla)\omega=\partial_{1}f_{2}-\partial_{2}f_{1}$

.

(5)

While the vorticity is not

conserved

because of the forcing

term,

it is

nevertheless

well controlled if the forcing

term

is assumed

to

be

sufficiently

smooth. An account

of

the

papers

on

the tw0-dimensional

Euler equations

can

be found

in [2],

wher

$\mathrm{e}$

数理解析研究所講究録 1234 巻 2001 年 127-145

(2)

[3],

[4]

are

surveyed.

See

also the

unpublished manuscript

[5] contained in this

vol-ume.

All the four papers

have used

successive

approximations to

construct classical

solutions of the tw0-dimensional Euler

equations.

To prove

convergence

of

succes-sive

approximations,

different methods have been

employed,

that

is,

Ascoli-Arzela’s

theorem

was

used in [3],

amore

direct

proof by

mathematical induction in [4]

and

Schauder’s fixed

point

theorem

in [1], [5].

In contrast

to

the

case

of Euler

equations,

the

question

whether

solutions

to

the

ideal Boussinesq

equations

with neither viscosity

nor

thermal conductivity, develop

spontaneous

singularity is

an

open

problem,

which has been

controversial, not only

theoretically but also

numerically.

In this paper in order

to

shed

some

light

on

this

unsolved problem,

we

compare the ideal Boussinesq

equations

with

the

coupled

tw0-dimensional Euler

equations,

the latter

of which

are

known

to

have

global smooth

solutions.

The tw0-dimensional

Boussinesq equations

can

be written

as

$\frac{\partial u}{\partial t}+(u\cdot\nabla)u=-\nabla q+(\begin{array}{l}0\theta\end{array})$

,

(6)

$\nabla\cdot u=0$

,

(7)

and the

temperature

0is

conserved

$\frac{\partial\theta}{\partial t}+(u\cdot\nabla)\theta=0$

,

(8)

where

we

have

used anotation

$q$

for the pressure. The initial data

$\omega(0)$

and

$\theta(0)$

are

assumed to be

smooth. It

should be

noted that

the second term

on

the

right-hand

side

of

(6)

is not divergence-free

(see

Section

4.2).

The

tw0-dimensional

Boussinesq equations

can

be written in vorticity form

as

$\frac{\partial\omega}{\partial t}+(u\cdot\nabla)\omega=\frac{\partial\theta}{\partial x_{1}}$

.

(9)

The vorticity is not conserved because of the presence of the

temperature gradient

in

atroublesome way. Needless

to mention,

it is not

possible

to

regard

this term

as a

smooth

external forcing because the

temperature not only

affects

the

flow field but

also

it is influenced

by

the

flow field. That

is,

there is aclosed

loop

of linkage

in

the

interaction between the variables

$\omega$

and

0. Because

of this feedback mechanism the

temperature

gradient

is out of control under time evolution.

Other

basic

properties

of the tw0-dimensional

Boussinesq equations

are

summarized

in the Appendices.

Indeed,

it has been

proved

in

$[6],[7]$

that the maximum

norm

of

$|\nabla\theta|$

controls

regularity

of

(9)

in

the

same

spirit

of acerebrated theorem established for the

three-dimensional Euler

equations

[8].

Anumber

of numerical simulations have

been

conducted

for

(6) (or,

for analogous

three-dimensional

axisymmetric

Euler

equa-tions,

see

Appendix

6.3)

$[9]-[14]$

.

Some

of them indicated blow-up in finite time.

But there is

no

proof

that shows

breakdown of smooth solutions for

(9),

that

is, not

asingle analytic

example

is known that blows up in

finite

time.

2Successive approximations

We show how

we can

construct

solutions

of the Boussinesq

equations

on

the basis

of the solutions of the Euler

equations by

successive

approximations.

That way

we

(3)

can assess

clearly

the

similarity

and difference between solutions of the Boussinesq

and Euler

$\mathrm{e}\mathrm{q}\mathrm{u}\mathrm{a}\mathrm{t}\mathrm{i}\mathrm{o}\mathrm{n}\mathrm{s}.[]$

2.1

The

kick-and-advect formalism

Suppose

we

compare

(8)

and

(9)

with

$\frac{\partial\omega^{0}}{\partial t}+(u^{0}\cdot\nabla)\omega^{0}=0$

,

(10)

$\frac{\partial\theta^{0}}{\partial t}+(u^{0}\cdot\nabla)\theta^{0}=0$

.

(11)

The above set

of

equations is just

atw0-dimensional Euler flow and

apassive

scalar

advected by it.

If

the

initial conditions

are

regular, both

$\omega^{0}$

and

$\theta^{0}$

remain

so

for

all

time.

Therefore

$\nabla\theta^{0}$

may

grow

in time

but

never

becomes unbounded

in

finite

time.

We

thus expect

that

growth

of

$\nabla\theta^{0}$

is much weaker than that

of

$\nabla\theta$

.

Then,

regard

$\nabla\theta^{0}$

as

aforcing term

and consider

yet

another tw0-dimensional

Euler

flow of

the

form

(the

kick stage)

$\frac{\partial\omega^{1}}{\partial t}+(u^{1}\cdot\nabla)\omega^{1}=\frac{\partial\theta^{0}}{\partial x_{1}}$

.

(12)

Since

$\theta^{0}$

is smooth all the time,

we

may

apply

the globally

existence theorem

of

forced

tw0-dimensional Euler equations to deduce that

$u^{1}$

is smooth all the

time.

Then the passive scalar

$\theta^{1}$

advected by it

(the

advect stage)

as

$\frac{\partial\theta^{1}}{\partial t}+(u^{1}\cdot\nabla)\theta^{1}=0$

(13)

remain

regular for all time.

We may

repeat

this argument

as many

times

as we

wish.

2.2

Coupled

Euler

equations

The above argument suggests how

we

may construct

’less

regular’ solutions

of

forced

Euler equations in

an

iterative

manner.

Thus,

in general

we are

led to

compare

(7)-(9)

with acoupled system

of tw0-dimensional Euler

equations of the

following form

$\frac{\partial\omega^{n}}{\partial t}+(u^{n}\cdot\nabla)\omega^{n}=\frac{\partial\theta^{n-1}}{\partial x_{1}}$

,

(14)

$\frac{\partial\theta^{n}}{\partial t}+(u^{n}\cdot\nabla)\theta^{n}=0$

,

(15)

$\nabla\cdot u^{0}=\nabla\cdot u^{n}=0$

,

(16)

for

$n=0,1,2$

,

$\ldots$

$N$

with

$\theta^{-1}\equiv 0$

,

1A

comparison

to

tw0-dimensional

Euler equations of another kind of active scalar equations

(surface

quasigeostrophic

equations)

has

been done in [15]. No successive approximations

were

not

introduced in that

case

(4)

where the superscript

$n$

denotes

the number of iterations. The initial data

are

taken

to be

$\omega^{0}(0)=\omega^{n}(0)$

and

$\theta^{0}(0)=\theta^{n}(0)$

,

for

$n=1,2$

,

$\ldots$

,

$N$

. As noted

above,

the zer0-th order solution

$(\omega^{0}, \theta^{0})$

is aset

of

the

solutions of the conventional tw0-dimensional Euler

equations

and

apassive scalar

advected

by

it.

While the

system (14), (15)

is big, i.e. made up of lots of

equations, the

interac-tion

among

the

variables

$\omega^{n}$

and

$\theta^{n}$

is one-way and there is

no

closed

loop in their

linkage, in

amarked

contrast to (8), (9).

2.3

Some properties of the

iteration

scheme

It should be noted that there

are

two limiting

processes involved in the

problem:

one

is the limit

of taking large

iteration number

$Narrow\infty$

and the other

one

is the

extension of the

time interval

$[0, T]$

over

which smooth solutions

exist. We

note the

following

basic

properties.

(i)

For fixed

$N$

,

the

system (14)-(16)

has

global

solutions,

that

is, smooth

solutions

persist

on

any time interval

$[0, T]$

,

no

matter

how large

$T$

is

([1]).

(ii)

For sufficiently large

$N$

,

(u,

$\theta^{N}$

)

is agood

approximation

to the

Boussinesq

equations, at

least

for short time development. If there is

no

blowup in

finite

time,

we

expect

that this

is

true

for

arbitrarily

large

$T$

.

(iii)

If

(u,

$\theta^{N}$

)

has alimit

in

some

sense

as

$Narrow\infty$

,

that

is,

the

system

(14)-(16)

has

akind of

’fixed-point property’,

it solves the

Boussinesq equations.

In this limit, the iteration scheme

retrieves the closed

interaction between

the

vorticity

and the

temperature. Below,

numerical results will be

presented

in

some

detail regarding this issue.

3Numerical experiments

3.1

Numerical Method

We

assume

periodic boundary

conditions in

$[0, 2\pi]^{2}$

for numerical

experiments.

We

use

astandard

pseud0-spectral

method for numerical solutions of

(14)-(16)

under

periodic boundary

conditions. The

2/3-rule

is used

for dealiasing and the maximum

wavenumber retained

is

$M/3$

for calculations with

$M^{2}$

grid

points.

We

use

$M=512$

and

1024

for solving

(14)-(16)

with the

iteration number

$N=10$

.

Time-marching

is performed by

aforth-0rder Runge-Kutta method. Two kinds of

initial

conditions

are

used.

3.2

Numerical results

The first

initial

condition

IC1

is

IC1

$\omega(x, \mathrm{O})=\theta(x, 0)=\sin x\sin y+\cos y$

(15)

(5)

$’=0$

$”..–\backslash \cdot\backslash \backslash //---==\simeq_{\backslash \backslash }.\backslash \sim.\cdot\backslash \cdot\backslash -’/\cdot’/\dot{i}$

,

$J-\backslash -J’^{\wedge}=\prime\prime-\backslash ^{\backslash }\backslash \backslash \prime\prime"$

$.,-\backslash \cdot.\simeq-$

$–\backslash -$

—,

$.\prime\prime\prime j^{\prime^{\prime-\sim\backslash }}\wedge=,----.\backslash ’\prime\prime,’=_{\sim}’\backslash \backslash \backslash \backslash \backslash \backslash$

$’—\wedge\sim-\nearrow\prime\prime.’\backslash$

$’./’\cdot$ $\backslash .\cdot.\backslash \backslash \backslash \backslash \backslash \backslash ^{\sim=}-\backslash \underline{-}\backslash ---=\backslash \cdot\backslash ,\prime j’\wedge/$

Fig. 1:

Contours

of vorticity

of

IC1

in

$[0, 2\pi]^{2}$

. Contour

levels

are

$\omega$

$=-1.4,$

-1.2, -1.0,

$\ldots$

1.4.

whose contours

are

depicted in

Fig.1. This is the initial

condition

used

in astudy

on

another kind

of

active

sealer equation

$[16, 17]$

.

The time evolution of contours of 0for

IC1

is

shown in Fig.2(a)-(e)

for the

iteration numbers $n=0,1,2,5$ and

$\infty$

.

In the Euler

case

$n=0$

(Fig.2(a)),

there is

arotational

symmetry

around apoint

$(\pi, \pi)$

which

is preserved under the Eulerian

dynamics (Fig.2(a)). For

$n=1$

such asymmetry is broken (Fig.2(b)) and the

pattern

is markedly

different from

that

of

$n=0$

.

The

difference

between

$n=1$

and

$n=2$

(Fig.2(c)) is

noticeable

but not

very

large. The

difference

between

$n=2$

and

$n=5$

(Fig.2(d))

is

even

smaller. It should be noted that the pattern for

$n=5$

is

virtually

indistinguishable

from

that

of

the Boussinesq

case

$n=\infty$

(Fig.2(e)).

To quantify the above similarity between the Boussinesq and Euler equations

we

show in Fig.3(a) the normalized correlation

coefficient

$C(\theta^{n}, \theta^{\infty})$

between

$\theta^{n}$

and

0”

for $n=0,1,2,3,4$ and

5.

It

is

defined

by

$C( \theta^{n}, \theta^{\infty})=\frac{\langle\theta^{n}\theta^{\infty}\rangle}{\sqrt{\langle(\theta^{n})^{2}\rangle\langle(\theta^{\infty})^{2}\rangle}}$

.

The

correlation coefficients

is 1initially because the two

fields

are

identical by

defi-nition.

As

expected, the

correlation between

$n=0$

(Euler)

and

$n=$

(Boussinesq)

decays quite quickly. Naturally, the time

interval

over

which the correlation

remains

close to unity extends

as

$n$

increases. However, it

should

be noted that at the

itera-tion

$n=5$

the

correlation survives fairly well,

e.g.,

$C(\theta^{5}, \theta^{\infty})=0.99997$

at

$t=4.0$

.

Note

that

$t=4$

is

the

maximal

time when the

flow

is resolved accurately and is not

to

be

considered

as

’short’. This

substantiates

the observation made in Fig.2(d) and

(e) that at the iteration

number

$n=5$

the contours

are

indistinguishable

between

the coupled Euler and Boussinesq equations.

Asimilar

coefficient

$C(\omega^{n}, \omega^{\infty})$

be-tween

$\omega^{n}$

and

$\omega^{\infty}$

is plotted in Fig.3(b).

Again,

at

$n=5$

the correlation

coefficient

remains close to unity up to

$t=5$

.

Next,

we

compare

the

growth

of the

passive scalar gradient with that of the

temperature

gradient.

In

Fig.4(a)

we

show

the

time evolution

of

the spatial

averages

of squared gradient of

$\theta^{n}$

$P_{n}(t)= \frac{1}{2}\langle|\nabla\theta^{n}|^{2}\rangle$

,

(6)

$\mathrm{i}’:0’=7$

$”,\simeq-,,.-\backslash \sim\backslash ’\prime’J’/.\cdot-\wedge\backslash j\acute{/j}’-\backslash ’\acute{\nearrow}\backslash _{\backslash /}^{\backslash \backslash \backslash arrow\acute{/}/^{}}----\sim/\backslash -\backslash \backslash -\sim\backslash /\prime^{-\backslash \backslash }\prime\prime-\backslash \backslash \prime\prime-’\wedge.\cdot\backslash \cdot\backslash \backslash \backslash \backslash =.,,.’.$

$.\grave{-}’.-\backslash ^{\backslash }\backslash \backslash \supset^{\backslash \check{\mathrm{C}}_{\backslash }’}\backslash \backslash \backslash \backslash \mathrm{x}_{\backslash \tilde{\tilde{\backslash }}}\backslash ..\grave{\grave{.}}\dot{\tilde{\grave{\tilde{\grave{\grave{C}}}}}}^{\vee}-_{\backslash \simeq\backslash \backslash /}^{\backslash }\prime\prime ’’\backslash \backslash /\backslash \backslash \backslash \backslash \backslash \backslash _{\backslash }^{\backslash }\sim\backslash \backslash \backslash \backslash \backslash \backslash \backslash \backslash --\backslash .-\vee’\vee\vee-\prime\prime$

.

$’=3$

$’=4$

$—–\backslash \wedge\cdot.\grave{\backslash \aleph}’\backslash \prime\prime\backslash _{\backslash }\backslash \backslash .\sigma’\acute{/^{t_{\backslash \backslash }’}\backslash \backslash }’\backslash /i’-’\overline{.}--.\sim_{\backslash }\mathrm{x}_{-}.\backslash .\backslash _{-}^{\backslash }\Im\cdot.-\backslash \backslash \backslash \backslash ^{\Im}\backslash \sim-\grave{\overline{i}}^{-}\backslash \backslash ,\backslash \backslash \backslash \backslash _{\backslash \backslash \backslash \backslash \equiv},\Leftarrow,-\backslash \backslash \backslash ^{\backslash }--\backslash \backslash \backslash \backslash ’\backslash \equiv\prime’\backslash 1\backslash \backslash \tilde{\backslash \prime\prime\prime}-$

$,-=\backslash ..\backslash ’\backslash ..’(_{\backslash }^{\Im_{j^{\backslash }}^{\backslash \backslash }}\backslash \backslash _{\backslash }\cdot\backslash \cdot.\cdot\Im^{\backslash }\backslash \backslash \backslash .\cdot.\cdot.,\cdot..\cdot..,’\backslash \backslash \backslash --/’\backslash \backslash ’\backslash \backslash \backslash \backslash \backslash \prime ^{\prime^{-}}’\backslash ’\wedge\backslash \backslash ’\backslash ’[searrow]^{-}\overline{\backslash \backslash }\backslash \backslash \backslash \mathrm{b}^{\backslash }\backslash \backslash \backslash \backslash -\backslash \backslash \prime\prime\prime\prime\prime\prime-\prime\prime\prime$

Fig.2(a):

Time evolution of contours

of

the temperature for

$n=0$

(the

Euler

case),

depicted

as

in Fig. 1

$\mathfrak{n}\dagger:\iota=1$ $\mathrm{t}=2$

$\mathrm{t}=3$ $\mathrm{t}=4$

Fig.2(b):

Time evolution of contours of the temperature for

$n=1$

.

(7)

$\mathrm{R}.\cdot 2\mathrm{t}=1$ $\mathrm{t}=2$

$|’,-,-, \backslash \backslash ---/\backslash _{\backslash _{\backslash }^{\backslash }}\backslash \backslash "\cdot..‘.\backslash ^{O}’\bigwedge_{\backslash \grave{\backslash }}^{\sim\backslash \backslash }’=\equiv\overline{\equiv=\simeq}\backslash -\backslash \backslash \sim\backslash ’/’----\backslash \backslash \prime\prime\Leftrightarrow^{\backslash }0\backslash i^{\prime^{--}-\simeq\backslash \backslash }\sim\backslash r^{1}\backslash \backslash \backslash \backslash .\cdot.\cdot\grave{\overline{\overline{O}}}_{J}^{_{\acute{l}}’}\backslash \backslash \grave{}\backslash \backslash \backslash \backslash \backslash \backslash \backslash \backslash ^{\backslash }\backslash \backslash \backslash ^{\backslash \backslash \sim}\backslash \cdot\simeq---,--\vee-\backslash \backslash \backslash \backslash \backslash ,.-\backslash \backslash \backslash .--\backslash \backslash ,-"-\backslash \approx-j.\wedge’\int^{-\sim}’\backslash -\prime\prime\acute{\acute{.}}$

.

$\cdot--\cdot\hat{---,}\backslash \sim^{\backslash }\ovalbox{\tt\small REJECT}_{\backslash }\sim_{\backslash \backslash \grave{\backslash \backslash ^{\grave{\grave{\mathrm{X}}}j}}}^{\mathrm{R}\backslash \backslash }\backslash \cdot.,.-i^{----}-\sim----\approx-\backslash \backslash \backslash _{\mathrm{I},\backslash _{\mathrm{t}^{1}}^{1\mathfrak{l}\mathrm{I}^{r\grave{\oint}}}}\grave{1}’\backslash \backslash ^{\backslash \backslash }\sim-\backslash _{\backslash \backslash \mathrm{s}’}\backslash \backslash _{\backslash }\simeq\backslash \backslash .’-\grave{\check{\acute{\overline{q}}}}_{\iota 1\backslash }^{J^{1}}\backslash ^{-\sim--\prime}\approx,-\overline{-}---=’|.|’.|\prime\prime||\dot{|}$

)’

$.’/$

\prime\prime\prime

$\mathrm{t}=3$ $\mathrm{t}=4$

$\backslash ,\backslash \cdot..\cdot\cdot...\cdot.\backslash -\backslash \backslash -\backslash \backslash \cdot..\wedge\backslash \backslash ^{\backslash \backslash }\backslash .\cdot.J\backslash ^{\mathit{1}1.\backslash ^{-}\vec{J}-}\grave{1}\hat{\backslash },\backslash ^{\iota_{\mathrm{I}}}\backslash ’\simeq^{\mathrm{Y}}\backslash \wedge^{:\backslash _{\backslash }^{\backslash }}\backslash \aleph_{\grave{\grave{\mathrm{v}}\mathrm{v}_{_{\backslash \backslash \backslash }}}}\backslash \backslash _{\backslash \backslash }\backslash \int^{/}\backslash \backslash _{\backslash }\backslash ^{-}\backslash _{\backslash }^{\backslash }-\prime J\backslash \prime 1’\prime\prime\prime’\nu_{1}\backslash -\backslash \cdot\backslash \acute{J}^{\prime/’}f’\prime\prime.\cdot.’$

,

$\prime\prime^{\prime\backslash \backslash }\mathfrak{l}_{\backslash }\int_{1/}^{1}\wedge\cdot.\backslash \sim\backslash \cdot.\cdot‘\backslash \backslash \backslash \backslash _{\mathfrak{l}\grave{|}}|\backslash \backslash \backslash \mathrm{i}_{\backslash \backslash }^{\backslash \backslash }\backslash \backslash \backslash \backslash \backslash ;0^{\nu_{l}}\backslash \mathrm{v}_{\acute{J}^{\prime.l^{\backslash }},\backslash \backslash -/^{\acute{l}}\backslash -\prime}\cdot‘\backslash -..\vee"/\prime r_{\# l}\backslash -^{\acute{l}}/\cdot/‘.’,|\mathit{1}_{j}^{r_{\acute{l}’}j^{-}},\neg$

.

Fig.2(c):

Time evolution of contours of the temperature for

$n=2$

.

$\mathrm{i}\mathfrak{i}5.\cdot 1=1$ $\mathrm{t}=2$

$\mathrm{t}=3$

$’=4$

$’\backslash .\backslash _{\mathrm{i}}\backslash l\backslash \grave{A}_{\dot{\mathrm{j}}\backslash \backslash }\backslash \backslash \cdot.;\mathrm{t}$

$j$

$.\cdot-’-\prime\prime\backslash _{\mathrm{t}}\backslash \backslash \cdot \mathrm{i}\mathrm{l}$

;

$\mathrm{X}.-,\backslash \backslash -^{l}z^{J}I_{S}^{\backslash _{J}}$

]

$,\backslash -\cdot$

.

$-.\cdot/^{j_{\wedge}’},\prime l^{1_{1}}’.,\cdot$

Fig.2(d):

Time evolution of contours of the temperature for

$n=5$

.

(8)

$\mathrm{i}\dagger \mathrm{I}:\mathrm{t}=1$

$’=2$

$\iota=\mathrm{s}$ $\mathrm{t}=4$

$\mathrm{t}\backslash$ $|\mathrm{V}$

,

$\mathit{1},\grave,r_{;\cdot\backslash \backslash }-\prime\prime.\backslash \backslash \backslash \backslash ^{\backslash }\backslash \backslash \backslash \backslash \backslash \backslash \cdot.\cdot..’|-\cdot-\cdot\acute{j\prime}|.\cdot]_{\backslash }$

$\backslash \cdot\backslash \backslash \backslash \backslash ’.\prime j^{j’}\prime\prime$

Fig.2(e):

Time evolution of contours of the temperature for

$n=\infty$

(the

Boussinesq

case).

for

$n=0,1,2,5$

and

$\infty$

. All the

norms

show

slightly exponential growth in time.

Needless to

mention, apossibility

cannot be ruled

out

that

Poo(t)

becomes

singular

at

atime later than what is covered

by

the

present

calculations. As

expected,

the

temperature gradient

grows

more

intensely

than the

passive

scalar

gradient

does in

$L^{2}$

,

that

is,

$P_{1}(t)$

is larger than

$P_{0}(t)$

.

It

should be noted that

the

curves

$P_{1}(t)$

,

Po(t).

$P_{3}(t)$

,

$P_{\infty}(t)$

are

close

to

each

other. Actually,

$P_{2}(t)$

is

smaller

than

$P_{1}(t)$

and

it is

Poo(t)

that

is the smallest

of this

group.

This

means

that

growth of

passive

scalar gradient of the

coupled

Euler

equations

is not

always

intensified

with

increasing iteration number. This

suggests

that the

Boussinesq

flows

are no more

singular

than

the

coupled

Euler

flows.

We know that it is the maximum

norm

$\mathrm{o}\mathrm{f}|\nabla\theta|$

that controls regularity

or

singu-larity

of solutions of the Boussinesq

equations.

The possibility that the above

norm

$P_{\infty}(t)$

,

which

essentially corresponds

to

$H_{1}$

-norm, remains finite

at ablowup

can-not

be ruled

out mathematically. In

this

sense

$P_{\infty}(t)$

, despite

its

physical meaning

(as arate

of

dissipation

of

$\langle\theta^{2}\rangle$

in slightly viscous

cases),

may

not

be

particularly

suited

for detecting

singularity. Rather,

it is

$H_{3}$

-norm

that becomes unbounded

at

aputative

singularity. We

are

led to consider the following

quantities

which involve

higher spatial

derivatives

$S_{n}(t)= \frac{1}{2}\langle|D^{3}\theta^{n}|^{2}\rangle$

,

where

$D\equiv(-\triangle)^{1/2}$

can

be defined through Fourier

$\mathrm{t}\mathrm{r}\mathrm{a}\mathrm{n}\mathrm{s}\mathrm{f}\mathrm{o}\mathrm{r}\mathrm{m}\mathrm{s}.2$

The

Sobolev

$2\mathrm{I}\mathrm{n}$

practice, it

is

easier

to monitor this

norm

than to

$\mathrm{t}\mathrm{r}\mathrm{a}\mathrm{c}\mathrm{e}$

astructure

associated with the

maximum

of

$|\nabla\theta|$

.

(9)

(a)

(b)

Fig.3

(a) Time

evolution of the

correlation coefficient

$C(\theta^{n}, \theta^{\infty})$

for

$n=0(\mathrm{s}\mathrm{o}\mathrm{l}\mathrm{i}\mathrm{d})$

,

1 (dashed), 2(shortl(dashed),

$3(\mathrm{d}\mathrm{o}\mathrm{t}\mathrm{t}\mathrm{e}\mathrm{d})$

,

$4$

(dash5(d0tted) and 5(short-dash-dotted), from left

to right,

(b)

That of

$C(\omega^{n}, \omega^{\infty})$

, depicted similarly.

Fig.4(a) Time

evolution of Pn

(t)

for

$n=0(\mathrm{s}\mathrm{o}\mathrm{l}\mathrm{i}\mathrm{d})$

, 1 (dashed), 2(shortl(dashed),

$5(\mathrm{d}\mathrm{o}\mathrm{t}\mathrm{t}\mathrm{e}\mathrm{d})$

and

$\infty$

(dash-dotted).

The

Euler

case

$n=0$

is

significantly

smaller than

others.

lemma

$\max_{X}|\nabla\theta(x, t)|\leq C\langle|D^{3}\theta(x, t)|^{2}\rangle^{1/2}$

ensures

that

$S_{\infty}(t)$

becomes

unbounded

simultaneously if the temperature gradient

does

so.

The time

evolution of

$S_{n}(t)$

for

$n=0,1,2,5$

and

$\infty$

is shown in Fig.4(b).

As

in

the

case

of

$P_{n}(t)$

,

$S_{1}(t)$

is larger than

$S_{0}(t)$

,

but

$S_{\infty}(t)$

is

smaller

than any

of

$S_{1}(t)$

,

$S_{2}(t)$

,

$\ldots$

,

$S_{5}(t)$

.

In

particular

we

have

$\langle|D^{3}\theta^{\infty}(x, t)|^{2}\rangle<\langle|D^{3}\theta^{1}(x, t)|^{2}\rangle$

,

(18)

as

far

as

the

numerical

solutions

are

regarded

as

well resolved.

Because

$S_{1}(t)$

never

become

unbounded

in finite

time,

this

result indicates that

the

solution of

the

Boussinesq

equations starting

from

IC1

shows

no

trend of

tending

to finite time

blowup.

In other

words,

unless

(18) is

reversed

at later time,

finite

time

blowup

cannot

occur.

To make

the point

more

clearly,

we

confider

the following

ratio

$R_{n}(t)= \frac{\langle|D^{3}\theta^{n}|^{2}\rangle}{\langle|D^{3}\theta^{\infty}|^{2}\rangle}$

.

(10)

$100000\{\infty 0_{1}0_{00.51152253354}1\mathrm{e}+061\epsilon+071\epsilon+0\epsilon|0\infty|\infty 10\ovalbox{\tt\small REJECT},’.\cdot.\cdot.\cdot.\cdot.\cdot.\cdot.\cdot.\cdot.\cdot\prime\prime\prime ’/\prime\prime/\cdot\prime’\cdot.\cdot.’.\cdot$ $021345\epsilon_{0}7$

05

1

$\tau \mathrm{s}$

2,

$-’\cdot’.\cdot.\cdot.\cdot-^{l’}\cdot.\cdot.-,-2.5335^{\cdot}$

.

$4”^{}\prime’j\prime\prime\prime\prime\prime\prime$ \prime\prime\prime

(b)

(c)

Fig.4

(b)

Time

evolution of

$Sn(t)$

for

$n=0(\mathrm{s}\mathrm{o}\mathrm{l}\mathrm{i}\mathrm{d})$

, 1(dashed),

2(shortl(dashed),

$5(\mathrm{d}\mathrm{o}\mathrm{t}\mathrm{t}\mathrm{e}\mathrm{d})$

and

$\infty$

(dash-dotted).

(c)

Time evolution

of

Rn{t)

for

$n=0(\mathrm{s}\mathrm{o}\mathrm{l}\mathrm{i}\mathrm{d})$

,

1(dashed),

$2(\mathrm{s}\mathrm{h}\mathrm{o}\mathrm{r}\mathrm{t}-$

dashed),

5(dotted) and 10(dash-dotted).

.

”.

” ’ ’ $\prime\prime’.\prime\prime$

.

.,

$\prime^{\prime^{\prime^{\prime’}}}$

.’.

$\cdot$

.’.

$-,.’.\cdot’.\cdot.\cdot=$

——-If there is blowup at

finite

time,

$R_{n}(t)$

must tend to 0,

since

the

denominator

be-comes

unbounded

while the numerator remains

finite.

In

Fig.4(c)

we

show the time

evolution of

$Sn(t)$

for

$n=0,1,2,5$

and

10. At

late times only

$R_{0}(t)$

converges

to 0,

but Rn

{

$\mathrm{t})$

and

$R_{2}(t)$

stay

significantly above 1. It

should

be noted

Rs(t)

is close

to

1. This

confirms

again that

at

$n=5$

,

the

coupled

Euler

equations approximates

the

Boussinesq

equations quite nicely.

In order to examine the

convergence

of the iteration

scheme

in

more

detail, in

Fig.5(a)

we

show the time evolution of the

complement

of the normalized correlation

coefficient,

defined

by

$1-C(\theta^{n}, \theta^{\infty})$

(19)

as a

$\log$

-linear

plot

for

$n=0,1,2$

,

$\ldots$

,

10.

From this

we

see

how

correlation

survives

longer with the

increasing iteration

numbers.

0

$\mathrm{o}\circ$

.

.

$\mathrm{o}$ $\mathrm{o}$ $\mathrm{o}$

$o$

$\mathrm{o}$ $\mathrm{o}$ $\circ$

.,0

$\mathrm{o}$

.

$\circ$ $.,\mathrm{s}$

,

2

$*$ $\cdot$

6

.

7

.

,

,0

(a)

(b)

Fig.5

(a)

Time evolution

of

$1-\mathrm{C}(0\mathrm{n}, \theta^{\infty})$

in

a

$\log$

-linear

plot,

for $n=0,1,2$,

$\ldots$

, 10 from

left

to

right,

(b)

${\rm Log}$

-linear

plots of

$1-\mathrm{C}(0\mathrm{n}, \theta^{\infty})$

against

$n$

at

times

$t=4(\mathrm{d}\mathrm{i}\mathrm{a}\mathrm{m}\mathrm{o}\mathrm{n}\mathrm{d}\mathrm{s})$

,

4.5(solid diamonds)

and

$5(\mathrm{s}\mathrm{q}\mathrm{u}\mathrm{a}\mathrm{r}\mathrm{e}\mathrm{s})$

.

To

check the

functional

dependence of

$1-C(\theta^{n}$

,

?”

$)$

on

$n$

at

fixed

times,

we

show

$1-C(\theta^{n}, \theta^{\infty})$

in

Fig.5(b)

against

$n$

at

times

$t=4.0,4.5$

and

5.0.

This

suggests

that

convergence

is

exponential

with

respect to

$n$

,

that

is,

$1-C(\theta^{n}, \theta^{\infty})\propto\exp(-a(t)n)$

(11)

for

some

positive function

$a(t)>0$

which

decreases with t.

Fig.6

Time evolution

of

the

Fourier spectra

of

the

temperature

for the Euler

case

$n=0(\mathrm{s}\mathrm{o}\mathrm{l}\mathrm{i}\mathrm{d})$

,

1(dashed), 2(short-dashed)

and the

Boussinesq

case

$n=\mathrm{o}\mathrm{o}(\mathrm{d}\mathrm{o}\mathrm{t}\mathrm{t}\mathrm{e}\mathrm{d})$

.

To monitor

how

the

higher

wave

number components

are

resolved

it is

useful

to

monitor the Fourier spectra

of

temperature

defined

by

$Q(k)= \sum_{k\leq|k|<k+1}|\tilde{\theta}^{n}(k)|^{2}$

,

where

$\tilde{\theta}^{n}(k)$

is the

Fourier

transform of

$\theta^{n}(x)$

. We show their time

evolution

for

$n=0,1,2,4$ and

oo

in

Fig.6.

We

see

that the Euler flow is the

most

regular of

all and that the

coupled

Euler flows and the

Boussinesq

flows

are

comparable

in

excitation

at

higher wavenumber

components.

All

in all,

we

have found that the

solution of

the Boussinesq equations

for

IC1

shows

no

hint

of going singular in finit

$\mathrm{e}$

(12)

$’=0$

$\backslash \backslash \prime\prime\backslash ..\cdot-\backslash .\cdot.\cdot.\prime\prime$

$\mathrm{I}_{\backslash ^{\iota_{\backslash \backslash \cdot\prime’}^{|||}},;,}^{jf_{\mathit{1}_{\acute{|}}}^{,}}\backslash \backslash \backslash ’\}-/\cdot\prime\prime\prime‘’\nearrow’,\cdot---\backslash \backslash \backslash \backslash _{\backslash }^{\backslash }\backslash .\backslash$

$\prime\prime’.’.\nearrow_{--\cdot-\backslash }^{\prime\backslash ^{\backslash \backslash \backslash \backslash =^{--j’}}}/’.----\sim^{\backslash }\backslash \cdot...\cdot..\cdot..\cdot.\cdot.\cdot.,,J/\backslash \backslash _{\backslash \backslash }^{\backslash }\wedge-\backslash \backslash \backslash \backslash \backslash \cdot’\backslash \backslash ’\backslash \backslash \backslash \backslash \backslash \backslash \backslash \backslash /\backslash ’.J$

\prime\prime\prime

$\backslash \backslash \backslash$

$\cdot/’\cdot/,\cdot,.",,’\cdot,-/.\backslash \backslash \backslash |)^{\backslash .\prime\prime\prime},|J/_{J’}\cdot.\backslash \cdot.\backslash \backslash |^{\prime|l^{1}}’\backslash \backslash ’\backslash ^{\backslash \backslash }11’\backslash \backslash \backslash$

Fig.7:

Contours

of vorticity

of

IC2

$[0, 2\pi]^{2}$

.

The thresholds

are

$\omega=$

$1.4$

.

-1.2,

Also,

$\ldots$

1.4.

Now

we

turn

our

attention

to

the second initial condition

IC2

to

see

whether

the

case

of

IC1

is accidental

or

not. The initial

condition

IC2

is given

by

IC2

$0(\mathrm{x}, 0)=0(\mathrm{x}, 0)=\sin x+\cos y$

,

(20)

which is shown in Fig.7. It is

astationary

solution

of the usual Euler

equations but

is

not astationary

solution of the

Boussinesq

equation.

Therefore

we can see

the

difference

between the two equations by

examining

the

solution

starting from

$\mathrm{I}\mathrm{C}2$

.

We show in Fig.8 the time evolution of

$Pn\{t$

)

for

$n=2,5,10$

and

$\infty$

.

Fig.8:

$Pn(t)$

for

$\mathrm{I}\mathrm{C}2;n=2$

(solid),

$5(\mathrm{d}\mathrm{a}\mathrm{s}\mathrm{h}\mathrm{e}\mathrm{d})$

,

$10$

(short-dashed)

and the Boussinesq

case

$n=\infty(\mathrm{d}\mathrm{o}\mathrm{t}\mathrm{t}\mathrm{e}\mathrm{d})$

.

The Euler

case

$(n=0)$

is

omitted,

because

it

is aconstant.

Because

IC2

is

astationary solution,

$\omega^{0}$

and

$\theta^{0}$

has

non

zero

Fourier

component

only

at the smallest

wavenumber,

that

is wavenumber 1.

Also,

$\omega^{1}$

has excitation

only

at the smallest wavenumber. For

$n\geq 2$

, it is remarkable that

they virtually

collapse

on

each other. This suggests the iteration scheme

converges

quite rapidly

with

$n$

for

IC2

as

well.

We show the time evolution of

contour plots

of

passive

scalar

at

$n=5$

in Fig.9(a).

For

comparison,

similar

plots

of the

temperature

$(n=\infty)$

are

shown

in Fig.9(b)

(13)

$j\prime 5.\mathfrak{i}=1$ $\mathrm{t}=2$

$’-f_{t}^{\acute{l},\wedge\downarrow_{\acute{\mathfrak{l}}j^{\acute{/}^{l}}\prime}\nearrow\backslash }/_{\acute{\mathrm{r}},}^{\prime\prime’}./^{i^{\backslash }--}\backslash .\acute,/\sim/.\prime\prime\prime^{\mathrm{I}}/^{\grave{J}_{\iota^{\mathrm{I}}}^{\nwarrow \mathfrak{l}_{\mathrm{t}^{1’\}}}}’}’/--\backslash$

$\cdot.-||!|\backslash ^{1^{1}}\backslash "\backslash --\backslash \backslash \cdot\backslash i\prime\prime \mathrm{I}^{r_{\mathfrak{l}}}(\backslash ^{\backslash }-\backslash ’/^{\prime\backslash }\acute{|}j\wedge\backslash \backslash \backslash ’[searrow]\vee\backslash \backslash \backslash \backslash /’\backslash .\mathit{4}l\backslash ^{\mathrm{t}}|\backslash --|_{1\backslash }\vee$

$\mathrm{t}=3$ $\mathrm{t}=4$

$–=_{jr^{\backslash }\backslash }^{\sim_{i^{\backslash }}}1\prime i\mathrm{I}.j\acute{.}...\backslash \backslash _{\backslash }^{1}\backslash \backslash \nearrow^{\prime \mathrm{I}}\downarrow\neq\prime 4\mathit{1}/\acute{\acute{\mathrm{r}}\prime}\mathrm{t}_{\backslash /}\mathrm{I}^{\mathfrak{l}}\backslash \wedge\backslash |-\backslash _{\backslash }_{\backslash }’\overline{-}\backslash _{\backslash \backslash }\backslash /|’\wedge\backslash \backslash \backslash \grave{\backslash }\overline{\backslash \backslash \backslash \backslash }\backslash \backslash \backslash ^{\backslash ^{1\backslash \overline{r}_{d}}}\simeq_{\tau_{\mathfrak{l}^{\acute{\mathrm{t}}}\backslash -}}^{\mathrm{I}}\backslash _{\backslash }\backslash \cdot\sim\backslash _{\backslash }^{\backslash }’\backslash \backslash ’\wedge\backslash \backslash ,||\backslash \backslash \backslash J\vee’-$

$\backslash \backslash \grave{\grave{\mathrm{c}_{\backslash }}},arrow-\grave{\simeq}_{\sim}^{\mathrm{s}}\sim\backslash \prime\prime A\backslash _{j}|\backslash /$

$(_{\backslash }^{1_{7.\prime}\prime}\backslash \cdot\cdot.\backslash l\cdot.,’\backslash J_{1\grave{\iota}’}\nearrow\backslash \backslash /\backslash ^{\mathrm{Y}\backslash }\backslash \prime’\backslash \prime\prime\gamma^{\mathrm{t}}",\cdot 1\backslash -\prime^{l}\backslash ^{\backslash }_{\backslash \langle’\acute{|}}\backslash \backslash ’,’(_{}\backslash \backslash$

Fig.9(a): Time

evolution of contour of

the

temperature for

$n=5(\mathrm{t}\mathrm{h}\mathrm{e}$

coupled

Euler

case),

depicted

as

in Fig.8

It is impossible to distinguish these contour plots at corresponding times, which

substantiates

the rapid

convergence

of the

iteration

scheme. In the

case

of

$\mathrm{I}\mathrm{C}2$

,

the

coupled Euler equations at

$n=5$

reproduce

solutions of

the

Boussinesq

equations

fairly

well.

4Theoretical

considerations

4.1

Difficulty

in

showing

convergence

of

the

iterations

At

present, it is not possible to

prove

that apair

of

solutions

$(\omega^{N}, \theta^{N})$

of

(14)-(16)

has

alimit

as

$Narrow\infty$

.

It

is

nevertheless useful

to point out the

cause

of the

difficulty

more

specifically.

As mentioned

above,

for

fixed

$N$

the system

$(\omega^{N}, \theta^{N})$

has aregular

solution for

all

time. This

means

that their values together with their

higher

derivatives of any

order

remain finite all

the time. Therefore,

for

example,

$||\omega^{N}||_{\infty}||\nabla\theta^{N}||_{\infty}$

(or,

with

other suitable

norms)

are

bounded from

above

on

any

time

interval

$[0, T]$

. If these bounds

are

shown

to be

uniform

in

$N$

,

then it is possible

to

argue

that there

exists

apair of

convergent

subsequences

$(\omega^{\infty}, \theta^{\infty})$

on

$[0, T]$

, to

obtain

asolution

to the Boussinesq equations (see

for

example [2]

and references

cited

therein). According to the

numerical

experiments the

norms

used appear

to

be uniformly

bounded

in

$N$

(see, Fig.4(a)&(b)

and

Fig.8). Unfortunately,

so

far

we

have not been able to

prove

such

uniform boundedness

by working directly with

the equations

of motion

(14)

$\mathrm{K}1.\cdot’=1$ $\mathrm{t}=2$

$’,\cdot\prime\prime\backslash \backslash ,.\cdot,\cdot\backslash _{\mathrm{x}’/}J^{\prime i^{P}}\backslash \overline{\backslash .},/’.\sqrt{\prime}’’\backslash ’-\backslash \backslash _{J\backslash }iarrow\backslash _{\backslash ^{\backslash }}^{\backslash \backslash \backslash \backslash _{\backslash }}--’\backslash ^{11}\backslash \backslash \rangle^{\backslash }\backslash \rangle\backslash \backslash (\begin{array}{l}\acute{\backslash \backslash \backslash .\backslash \backslash \prime’}\mathrm{o}(\backslash \backslash \backslash j\prime\end{array}$

$’=3$

$’=4$

$\neg-\prime^{-\backslash \cdot,\sim}\sim\prime\prime\backslash |\cdot,’....\cdot\backslash |||\cap^{\backslash \backslash }||\acute{|}\backslash \downarrow^{\sim}\backslash \dagger\prime 1^{\prime\backslash }1’\wedge^{\backslash }---\backslash -.’.\nearrow..||\iota_{j\backslash _{\mathrm{v}}},\backslash !\grave{\backslash }^{|\mathrm{t}_{-}}\overline{\grave{\backslash }}\gamma_{(^{\iota}}^{\mathrm{i}1\backslash }|\prime \mathrm{I}||\backslash \backslash _{-}\backslash \backslash \cdot$

Fig.9(b):

Time

evolution

of contour of the temperature for

$n=\circ 0$

(the

Boussinesq

case),

depicted similarly.

4.2

Anote

on

aresult

of Cordoba and Fefferman

The numerical results

presented

in the

previous

section

suggests

regularity of the

solutions of the Boussinesq

equations

rather than their

singularity.

As

mentioned

in Introduction, global

regularity of the Boussinesq has

not yet

been demonstrated.

Nevertheless there

are some

mathematical results that restrict

possible

formation

of singularity.

One

recent

result

[18]

claims that if asingularity is

formed

in

finite

time by coalescence of level sets of 0, then not only

$\nabla\theta$

but also the

velocity must

become

unbounded at that time. Their result is valid for any active scalar

equations.

Here

we

consider the what this result

means

in the

particular

case

of the Boussinesq

equations.

Retaining the integral

representation (3)

we

may

rewrite

(6)

as

$\frac{\partial u}{\partial t}+(u\cdot\nabla)u=-\nabla p+$

$(\begin{array}{l}R_{1}R_{2}[\theta]R_{2}R_{2}[\theta]+\theta\end{array})$

,

(21)

where

$R_{\dot{\mathrm{e}}}=(-\triangle)^{-1/2}\partial_{i}$

is

the Riesz transform. The second term

on

the right-hand

side of

(21)

is not bounded by

aconstant,

but it

satisfies

the

following

inequality

$[19, 20]$

$||R.R_{j}[ \theta]||_{\infty}\leq C||\theta||_{\infty}[1+\log_{+}(L\frac{||\nabla\theta||_{\infty}}{||\theta||_{\infty}})]$

where

$i,j=1$

or

2,

$\log_{+}x=\max(\log x, 0)$

and

(15)

$C(>0)$

,

L

$=\sqrt{\frac{||\theta||_{1}}{||\theta||_{\infty}}}$

are

constants.

Suppose that

we

attempt

to reconstruct the velocity of the Boussinesq

equations

by solving

forced Euler

equations

with

an

appropriate

external

force

$\frac{\partial u}{\partial t}=-\{(u\cdot\nabla)u\}^{\mathrm{t}\mathrm{r}}+f$

,

(22)

where

we

have

put

$\{(u\cdot\nabla)u\}^{\mathrm{t}\mathrm{r}}\equiv(u\cdot\nabla)u+\nabla p$

.

Given

$\theta(x, t)$

,

we can

choose the

forcing term

a

posteori

as

$f=(\begin{array}{l}R_{1}R_{2}[\theta]R_{2}R_{2}[\theta]+\theta\end{array})$

.

If asingularity

is formed

by

coalescence of level

sets

of 0,

by

atheorem

[18]

we

have

$||u||_{\infty}=\mathcal{O}((t_{*}-t)^{-n})$

with

$n\geq 1$

or

$|| \frac{\partial u}{\partial t}||_{\infty}=\mathcal{O}((t_{*}-t)^{-(n+1)})$

.

On

the

other

hand

we

have by

$[6, 7]$

$||\nabla\theta||_{\infty}$

must

diverge

at

least

as

$(t_{*}-t)^{-2}$

for

apossible

blowup.

Assuming

an

algebraic

$\mathrm{b}1\mathrm{o}\mathrm{w}- \mathrm{u}\mathrm{p}^{3}$

$||\nabla\theta||_{\infty}=\mathcal{O}((t_{*}-t)^{-m})$

, with

$m\geq 2$

,

the

forcing term is

bounded

as

follows

$||f||_{\infty} \leq C\log(\frac{1}{t_{*}-t})$

,

with apositive constant

$C$

.

Then,

$\frac{\partial u}{\partial t}$

must

be

balanced

with

$\{(u\cdot\nabla)u\}^{\mathrm{t}\mathrm{r}}$

. This

is acontradiction,

since

as

$tarrow t_{*}$

,

the

forcing term

becomes

negligible and

the

forced Euler equations

become

unforced

in the limit

$tarrow t_{*}$

.

It

is impossible

for

the

Boussinesq equations to

go

singular by the mechanism of coalescence of level sets of

0associated

with

algebraically singular

$||\nabla\theta||_{\infty}$

.

5Summary and discussion

We have proposed

asuccessive

approximation

scheme that

generates

asolution

of

the Boussinesq equations

on

the basis of solutions tw0-dimensional Euler

equations.

If

$(u^{N}, \theta^{N})$

has alimit

in

some

sense as

$Narrow\infty$

,

that

is, the system (14)-(16)

has

akind of ’fixed-point property’, it solves the Boussinesq equations.

Whether

the

Boussinesq equations remain

regular for all

time

or

not depends

on

the

convergence

of

the

iteration scheme. Because such

convergence

is not

obvious mathematically

we

have

performed

some

numerical

experiments

using

apseud0-spectral

method.

$3\mathrm{M}\mathrm{u}\mathrm{c}\mathrm{h}$

stronger

singularities,

e.g.

$\exp(t_{*}-t)^{-n}(n>0)$

, cannot

be

ruled

out.

But

such

a

behavior has not

been

reported

to

occur

in

numerical

experiments

(16)

The iteration scheme turned

out to

converge

rapidly

as

far

as

the

current numerical

results

are

concerned,

suggesting global regularity

of the

Boussinesq equations.

On

the other

hand,

if asolution to the

Boussinesq equations

goes

singular at

some

later time which cannot be

covered at

the

present resolutions,

then

convergence

of

asolution of the

coupled

Euler

equations to

that

of the

Boussinesq equations must

be

invalidated

by

the

time of

blowup. Therefore,

numerical

experiments supporting

blowup

for the

Boussinesq equations

should observe

abehavior

in

$\nabla\theta$

markedly

different from acorresponding

quantity

of the

coupled

Euler

equations. In this

sense, the

present

method will

serve

as

asolid

criterion for monitoring

singularity

formation

in

the

Boussinesq

equations.

In

place

of

(14)-(16)

we

may consider

yet

another method of successive

approxi-mations

$\frac{\partial\omega^{n}}{\partial t}+(u^{n-1}\cdot\nabla)\omega^{n}=\frac{\partial\theta^{n-1}}{\partial x_{1}}$

,

(23)

$\frac{\partial\theta^{n}}{\partial t}+(u^{n-1}\cdot\nabla)\theta^{n}=0$

,

(24)

$\nabla\cdot u^{0}=\nabla\cdot u^{n}=0$

,

(25)

which is astraightforward

generalization

of Kato’s idea

[1].

Note that

they

are

linear with

respect

to

$\omega^{n}$

and

$\theta^{n}$

, respectively.

We

can

prove local existence for

the

Boussinesq equations by

repeating the

arguments

used in

[1].

However

we

do not

know if it is

possible

to

extend the time interval of local

existence,

because of

lack

of

vorticity conservation,

as

pointed out to

the author

by

Prof. H.

Okamoto.

Acknowledgments

The author would like to thank Professor H.

Okamoto and Dr. M. lima for

useful

comments.

This work has been

partially supported by

Grant-in-Aid

for

scientific

research

from the

Ministry

of

Education,

Culture,

Sports,

Science

and Technology of

Japan,

under Nos. 11304005 and

11214204.

6Appendices

([21],[22])

6.1

Conserved quantities

There

are

obvious conservation laws

to (6)

$\int_{\mathrm{R}^{2}}$

or

$\mathrm{T}^{2}F_{1}(\theta(x))dxx$

,

(26)

where

the domain

of integration extends

over

$\mathbb{R}^{2}$

(infinite plane)

or

in

$\mathrm{T}^{2}$

(for periodic

boundary conditions). Moreover, (6)

conserves

$\int_{\mathrm{R}^{2}}(\frac{|u|^{2}}{2}-y\theta)dx$

(27)

for the

infinite

plane

case

and

$\int_{\mathrm{T}^{2}}(\frac{|u|^{2}}{2}-(y-b)\theta)$

idea

(24)

under

periodic boundary conditions,

where

$(a, b)$

is aset

of Lagrangian marker

variables such that

$(a, b)=(x, y)$

at

$t=0$

.

(17)

6.2

Stationary

solutions

It

is

well-known

that

stationary

solutions

of tw0-dimensional Euler

equations

are

characterized

by

afamily

of

one

arbitrary

function

relating vorticity

$\omega$

and stream

function

$\psi$

.

In

contrast,

it

requires

two

arbitrary

functions

to specify

stationary

solutions

of tw0-dimensional

Boussinesq

equations,

say

$F$

and

$G$

.

In

$\mathbb{R}^{2}$

,

stationary

solutions

of

$(8,9)$

have the following representation

$\theta=F(\psi)$

,

(29)

$\omega$

$+F’(\psi)y=G(\psi)$

.

(30)

The

second relation is derived

as

follows

$\frac{\partial(\omega,\psi)}{\partial(x,y)}=F’(\psi)\frac{\partial(\psi,y)}{\partial(x,y)}=\frac{\partial(\psi,F’(\psi)y)}{\partial(x,y)}$

.

(31)

In

$\mathbb{T}^{2}$

such

an

representation

is not valid.

6.3

Analogy with three-dimensional

axisymmetric flows

In

the axisymmetric

case

$\frac{\partial}{\partial\phi}=0$

,

the

th

$\mathrm{r}\mathrm{e}\mathrm{e}$

-dimensional

Euler

equations

can

be

written in cylindrical coordinates

$(r, \phi, z)$

as

$( \frac{\partial}{\partial t}+u\cdot\nabla)u=\frac{1}{r^{3}}(ru_{\phi})^{2}e_{r}-\nabla p$

,

$( \frac{\partial}{\partial t}+u\cdot\nabla)(ru_{\phi})=0$

,

and

$( \frac{\partial}{\partial t}+u\cdot\nabla)\frac{\omega_{\phi}}{r}=\frac{1}{r^{4}}\frac{\partial}{\partial z}(ru_{\phi})^{2}$

,

where

$u=(u_{r}, u_{\phi}, u_{z})$

.

If

we

accept

the

following correspondence

$ru_{\phi}\Leftrightarrow\theta$

,

$\frac{\omega_{\phi}}{r}\Leftrightarrow\omega$

,

then

the three-dimensional axisymmetric equations

are

similar to the

tw0-dimensional

Boussinesq

equations

(except

at

$r=0$

).

The work [10] regarding the

three-dimensional

axisymmetric Euler equations

is based

on

this analogy.

References

[1] Kato, T.(1964).

On

classical solutions

of

the

tw0-dimensional

non-stationary

Euler equation,

Arch. Rat.

Mech. Anal, 25,

302.

[2] Sulem,

C. and

Sulem, P.-L. (1983). The well-posedness

of

the

tw0-dimensional

ideal flow,

J.

M\’ec.

Theor. Appliqu.(Paris)

Special

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(18)

[3]

Wolibner, W.(1933).

Un theorem

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Schaeffer,

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Shu, Ch.-W.(1994).

Small-scale structures in

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[8] Beale, J.T., Kato,

T and

Majda A.(1984).

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[9] Grabowski,

W.W. and

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Cloud-environment

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instabil-ity:

rising thermal calculations in two

spatial dimensions,

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[10] Pumir,

A. and Siggia,

$\mathrm{E}.\mathrm{D}.(1992)$

.

Development

of singular solutions

to

the

axisymmetric Euler

equations, Phys.

Fluids A,

4,

1772.

[11] Pumir, A., Shraiman,

B.I.

and

Siggia,

$\mathrm{E}.\mathrm{D}.(1992)$

. Vortex

morphology and

Kelvin’s

theorem,

Phys.

Rev.

A, 45,

R5351.

[12] Grauer,

R. and

Sideris,

$\mathrm{T}.\mathrm{C}.(1995)$

. Finite time singularities in ideal fluids

with

swirl,

Physica D, 88,

116.

[13]

Carmack,

$\mathrm{L}.\mathrm{A}.(1997)$

.

Vorticity

amplification in

incompressible

ideal

swirling

flow without

aboundary, Phys. Fluids, 9,

1379.

[14]

Toh, S.,

Matsumoto

T.,

Miyashita

H. and

Yamada, Y.(2001)

Intermittency

and

singularity

in

an

active scalar turbulence

-finite

time singular

.ty

in

the two

dirnensional

ideal

Boussinesq

approximation equations-(in Japanese), Reports

of

RIAM

Symposium,

$\mathrm{N}\mathrm{o}.12\mathrm{M}\mathrm{E}$

-Sl,

20.

[15] Majda,

A.J. and

Tabak, E.G.(1996).

AtwO-dimensional model for

quasi-geostrophic flow:

comparison

with

the tw0-dimensional Euler flow.

Physica D,

98,

515.

[16]

Constantin,

P.,

Majda,

A.J.

and

Tabak, E.(1994).

Formation

of strong fronts

in

the 2-D quasigeostrophic thermal active

scalar,

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1495.

[17]

Ohkitani,

K. and

$\mathrm{Y}\mathrm{a}\mathrm{m}\mathrm{a}\mathrm{d}\mathrm{a},\mathrm{M}.(1997)$

.

Inviscid and inviscid-limit behavior of

a

surface

quasi-geostrophic

flow, Phys. Fluids, 9,

876.

[18] Cordoba,

D.

and

Fefferman, C.(2001).

Scalars convected

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flow,

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[19] Constantin,

P.

and

Wu, J.(1996).

The inviscid limit

for non-smooth

vorticity

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(1998).

Absence of proper nondegenerate generalized

self-similar

singularities,

J.

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Phys.,

93,

777.

[21] Abarbanel, H.D., Holm, D.D., Marsden,

J.E. and

Ratiu, T.S.(1986).

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stability analysis

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Szeri A. and

Holmes,

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