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Order parameter and amplitude equations for the Rayleigh-Bénard convection

W. Decker, W. Pesch

To cite this version:

W. Decker, W. Pesch. Order parameter and amplitude equations for the Rayleigh-Bénard convection.

Journal de Physique II, EDP Sciences, 1994, 4 (3), pp.419-438. �10.1051/jp2:1994137�. �jpa-00247971�

(2)

J- Pllys. II Hance 4

(1994)

419-438 MARCH 1994, PAGE 419

Classification

Physics Abstracts

47.10 47.20

Order parameter and amplitude equations for the

Rayleigh-B4nard convection

W. Decker and W. Pesch

Physikalisches Institut der Universitit Bayreuth, W-8580 Bayreuth, Germany

(Received

20 August 1993, revised 18 November 1993, accepted 6 December

1993)

Abstract. The reduced description of the roll patterns and their stability near onset is

investigated in detail for Rayleigh-Bdnard convection. The starting point is a novel order pa- rameter equation

(OPE)

in Fourier space that is rigorous up to cubic order in the amplitudes of the critical modes at threshold. Comparison with rigorous results from a Galerkin analysis ex-

hibits the range of validity of this order parameter description. In particular in the case of gases

(Prandtl

number

~ 1), the reduced description is fairly satisfactory. In

a next step the OPE are

used to derive coupled amplitude equations in real space. In this way

a complete description

of the mean drift mode is achieved for the first time. It is shown that at least for intermediate Prandtl numbers a large number of derivative terms is necessary to get good agreement with the rigorous results. I/rom the results one can also judge, under what conditions common model

equations are likely to describe the real systems.

1. Introduction.

Rayleigh-Bdnard

convection

(RBC)

in fluid

layers

heated from below

provides

a canonical ex-

ample

for

pattern-forming

transitions in

nonequilibrium

systems [1, 2]. It has been studied for

many years without

loosing

its attractiveness

(besides general

reviews, e.g. in

[3-7,

1, 2] very

recent

experimental

work may be

found,

e.g. in

[8-10]).

In a series of

important

papers the

destabilization mechanisms of the

periodic

roll pattern in ABC have been classified

by

Busse and coworkers and the stable wavenumber

regimes (the

~'Busse balloon" have been

mapped

out as a function of the two nondimensional parameters,

namely

the

Rayleigh

number R

(the

main external control

parameter)

and the Prandtl number Pr [3, 11].

Typical

destabilization mechanisms involve modulations of the roll

separation (Eckhaus instability (E) [12]),

undu- lations

along

the roll axis

(zigzag instability (ZZ))

and combinations of both types

(skewed

varicose

(SV))

[11, 13].

The present paper is devoted to

large-aspect-ratio

systems

slightly

above the onset of the convection

instability,

where a small expansion parameter e

(the

reduced distance of the ex- ternal control parameter R from threshold

R~)

is available. One can then

apply

the familiar

(3)

weakly

nonlinear

analysis,

which appears in several variants in the literature [1, 2]

(or

with

more

emphasis

on RBC

[14,

5, 6])-

The method can be

phrased

as a reduced

dynamical description

based on the space of the linear

modes~

which grow

exponentially

or are

only slightly damped

at threshold. With respect to the horizontal

directions~

in the idealized limit of

laterally

infinite

extension,

the modes are characterized in Fourier space. The

simplest

case is a

periodic

roll pattern near onset with

wavevector q. Then the Fourier

amplitude A(q) plays

the role of an order parameter, which is

determined

by expanding systematically

up to cubic order in terms of

A(q).

The

application

to RBC has been initiated in [15, 16] and culminated in the

comprehensive

work in [17].

Roll patterns observed in nature have the

tendency

to

display

slow modulations in space

(and possibly

also slow in

time)

apart from the appearance of defects

(foci, dislocations)

[1~ 2].

Such modulated patterns can be described as wave

packets

where several Fourier modes with

weights (A(q)(

interact.

Proceeding again

up to cubic

order,

the

complex

Fourier

amplitudes A(q)

become

coupled by

a nonlinear

integral equation,

the order parameter

equation (OPE) [18-20].

Our first main issue was the

rigorous

derivation of the OPE for RBC.

By

construction it becomes exact in the limit e - 0. But as an

important

result we found

by comparison

with the

rigorous

Busse

balloon,

that the order parameter concept remained

satisfactory

up to

fairly large

values of e in some cases

(e.g.

for Pr m 1

nearly

up to e

=

1).

That holds true for the

long-wavelength (E, ZZ, SV)

as well as for the

short-wavelength

cross-roll

(CR)

[3]

instability

boundaries. The results are

encouraging

to

apply

the order parameter

approach

as a semi-

quantitative

concept to more

complicated

pattern

forming

systems like

liquid crystals (21-23].

Here precise measurements near threshold have revealed a multitude of

interesting

scenarios, but a more

rigorous

treatment

beyond

the OPE is

practically precluded by

the

complexity

of the system.

The OPE will serve as a convenient

starting

point for an additional

approximation

scheme

in our case. One scales the distance

(q~ q()

+~

e~/2 and introduces a time scale

+~ e.

By

switching

to real space one arrives at

leading

order in

e at the famous

Newell-Whitehead-Segel (NWS) (or amplitude) equation

[24,

25], commonly applied

to the

description

of modulated patterns near threshold. The NWS

equation

was obtained

originally by

a multi-scale

analysis,

all terms up to order e~/2 are balanced and no

explicit e-dependence

is left.

It was

recognized fairly early,

that in certain cases

(at

least for small Prandtl

numbers)

an

extension of the basic NWS equations is necessary

by taking

into account

higher

orders in e

[26, 27].

Otherwise a

quantitative description

of the

zigzag (ZZ) instability

[28,3] is

impossible

and the skewed varicose

(SV) instability

does not appear at all. Of

particular importance

is the inclusion of the mean-flow

(mean-drift)

mode which is excited in second order, if the pattern deviates from strict

periodicity.

It is characterized

by

a

typical length

scale much

larger

than the roll

spacing, by

nonzero vertical

vorticity

and a

nonvanishing spatial

average of the

velocity

fields across the fluid

layer.

Mean-flow effects in RBC in the context of

amplitude

equations

(AE)

have been considered at first for the

simplifying

situation of stress free

boundary

conditions

[26, 27].

After some refinements [29]

existing discrepancies

between the results obtained in

[26,

27] and others based on OPE

[30,

31] were reconciled.

For the realistic

rigid boundary

conditions the

appropriate procedure

has been outlined in

principle

in the literature [19, 32, 14,

6],

but has

surprisingly,

as far as we know, never been worked out in detail. Thus we wished to fill this gap for the standard ABC system, in order

to test the

approximation

scheme with a view to more

complicated

situations a~~ well as to

provide guidelines

on the way to

semi-quantitative

simulations of scenarios such as the

spiral

turbulence [10]. In the

resulting coupled amplitude

equations the mean flow

amplitude

is

(4)

N°3 AMPLITUDE EQUATIONS FOR THE MC 421

explicitly

isolated in contrast to the OPE equations. We find in

addition,

that also terms

arising

from the

elasticity

of the rolls

(higher

order derivative terms in the cubic part of the roll

amplitude equation ), play

an

important

role.

The paper is

organized

in the

following

manner. After this introduction we sketch in section 2 the derivation of the OPE and compare with

rigorous

results. Section 3 is devoted to the

presentation

of the

coupled amplitude equations.

The

resulting stability

boundaries are

briefly

discussed in section 4 and also

compared

with the OPE. After the conclusion in section 5 the

appendices

contain some additional more technical details.

2. Order parameter

equations.

2.I FORMULATION OF THE PROBLEM. Our

starting

point are the dimensionless

Boussinesq

equations

for the

velocity

field u and the deviation of the temperature from the static distribution

(see

e-g. [28] ):

V.u=0

,

(la)

V~6+Rk.u=u.V6+~6

,

(lc)

where k is the unit vector in z-direction

(opposite

to the direction of

gravity)

and 7r is the pressure.

We use the conventional dimensionless quantities,

namely

the

Rayleigh

number

(R)

as the main control parameter and the Prandtl number

(Pr)

and consider realistic

rigid boundary

conditions.

The

equations

are reformulated

by

the introduction of two

velocity potentials f

and g ap-

propriate

to the solenoidal vector field u

ill,

28]

u = 6

f

+ eg

,

6 =

(b(~, b(~, -b(~ b(~)

,

e =

(by, -b~, o) (2)

The

quiescent

state

corresponds

to

f

= g = 6

= o. In the

following

we will introduce the vector notation V

=

(6, f, g)

and use a

symbolic

notation for the basic equations.

£V =

N2(V(V)

+

B~~

(3)

The

explicit

form of various matrix operators in

(3)

which contain

spatial

derivatives is clear from

equations ii)

and

(2).

2.2 WEAKLY NONLINEAR ANALYSIS. The first step of the

analysis

is based on the behavior at threshold which is described in detail in the literature

(see

e-g-[33]

).

The onset of convection is determined with the

help

of the linear

eigenvalue problem

£V

=

B$f (3).

The modal

solutions have the

general

form:

viz,

g, Z,

t)

#

vi;nl~,

Z,

R)e~~~e~~,

q "

jq, p),

X

" IX,

g) j4)

The lowest value of R for which the linearized equation

(3)

has a nontrivial solution for I = o

yields

the neutral surface

Ro(q),

and the minimum of

Ro(q)

with respect to q

gives

the

(5)

critical wavevector q~ which is

degenerate

on a circle with radius q~. Because of the rotational invariance we can fix the direction of q~

arbitrarily.

The

corresponding

cut of the neutral surface

along

that direction is the neutral curve

R(q).

The next step of the

weakly

nonlinear

analysis

[18,

34, 6,

1, 2],

(for

a recent more detailed

presentation,

see also [21, 22]

describing

the situation

slightly

above threshold is to reduce the

dimension of the system

by choosing

an appropriate "basis" set of states, characterized as the

"dynamical

active" ones in [6]. One

approximates

the solutions for R >

R~

at lowest order

by

a wave

packet

of the linear

eigenmodes

Vo

(+ li;n(q,

z, R

=

R(q))) (see (4)):

V Gt Vi "

/dq A(q, t) Vo(q,

z)e~~l~ + c-c-

(5)

D

Here

A(q) plays

the role of the order parameter

(amplitude),

which vanishes at threshold. The

integration

domain D is a small annulus centered around (q( = q~ which need not be

specified

in advance. The

amplitude A(q)

will be determined from

equation (3) by

a systematic

expansion

of V which is small near

threshold,

in the form V

=

Vi

+ V2 +

V3

+ .. The second order solution V2

-~

A~ is

explicitly

calculated as the solution of the

corresponding inhomogeneous

linear system derived from

equation (3):

£V2

= N2

(Vi [Vi ). (6)

The solution V2 contains contributions with wave vectors

ranging

from (q( m o up to (q( m

2q~.

Proceeding

to third order the

equations

are closed

by projecting

the third-order solutions

V3

-J

A~ onto the

subspace spanned by

the linear modes

(Vo(q, z),

see

(5)).

One obtains the order parameter

equations (OPE)

in Fourier space:

al

(q)~A(q, t)

=

a2(q)A(q, t)

+

/ dqi / dq2

£l3

(q,

qi,

q2)A(qi, t)A(q2, t)A(q

qi q2,

t), (7)

D D

Note that the coefficients

a~(q), (I

= 1, 2,

3) depend

on the Prandtl

number;

their

explicit

calculation is done

numerically.

The

approach

could be

generalized

if one uses the

eigenmodes

li;n

(Eq. (4),

1

#

o for E >

o)

and avoids the adiabatic

approximation

involved in

equation (6) (see Appendix

C of

[21]),

but

we detected no

significant changes

in our results.

2.3 STABILITY DOMAINS FROM OPE. To start with we are interested in

stationary

roll

solutions,

periodic

in space which are characterized

by

a wavevector qo. One uses the ansatz:

Ar(q)

" CT

6(q qo)

+ Cl

6(q

+

qo) (8)

in

equation (7).

The double

integral

on the

right

hand side of

(7)

then

collapses,

and the

amplitude

coefficient cr can

easily

be calculated. It is also obvious that (cr(~ is

proportional

to

(R Ro(qo))/Ro(qo),

the reduced distance from the neutral

surface,

which serves

essentially

as our small

expansion

parameter.

The

stability analysis

of the stationary roll solutions is

performed by introducing

a small

perturbation 6A(q, t)

of the

amplitude Ar (Eq. (8)):

6A(q,

S,

t)

= (Ci

iq,

S)

6(q

qo S) + C2

(q,

S)

6(q

+ qo

S))

e~~

(9)

(6)

N°3 AMPLITUDE EQUATIONS FOR THE ABC 423

and

linearizing equation (7).

The wavevector s denotes a modulation of the

qo-periodic

pattern.

One arrives at a linear

eigenvalue problem

for cl and c2 where the I with the maximal real part determines the

growth

rate a~~~j,~(qo, s,

R).

When the maximum of a~~~j,~

(with

respect

to

s)

crosses zero the values

(qo, R)

on the

stability

boundaries are identified.

The

perturbations

6A

(9)

are classified

by

the

magnitude

S and the orientation

angle

8 of the modulation wavevector s

(see Eq. (9)), according

to s =

S(cos 8,

sin

8).

One

distinguishes

between

long-wavelength perturbations (S

< q~, an

analysis

up to

O(s~)

is sufficient

),

among which are Eckhaus

(8

=

o), zigzag (8

=

7r/2)

and skewed-varicose

(o

< 8 <

7r/2) modes,

and

short-wavelength perturbations (S

m q~), such as the knot

(K)

and the cross-roll

(CR) instability

[3, II, 5]. For a roll pattern with wavevector qo "

(q, o)

m q~, the cross-roll insta-

bility

is obtained with s

=

(-q, p),

where p is of order q~. There exists also another

important short-wavelength instability, namely

the

oscillatory

one [3, 35,

36].

It appears

typically

at

higher

values of E and cannot be described in the approximation scheme of the

OPE,

because decisive modes are

neglected.

In the

following,

we will consider

separately

three

representative

values of the Prandtl number and compare with the

rigorous results,

which are

briefly recapitulated.

I) In the low Prandtl number

regime (see

[36] we took an extreme case

(Pr

=

o.ol),

which is realized e-g- in

liquid

sodium. The Busse balloon is limited on the left hand side

by

the Eckhaus

(for

very small

negative

values of q q~

by

the

zigzag)

and on the

right

side

by

the

skewed-varicose

instability.

Both

boundary

lines rise

steeply

with

E and the upper limitation of the Busse balloon is of the

oscillatory

type

(not

accessible

by

the

OPE),

found at E m o.08 for q = q~ [36]. As shown in

figure

la, the OPE

description gives acceptable quantitative

results

near onset, I-e- for E < o.ol

(see

e-g- the Eckhaus

line),

but the type of

destabilization,

and

more

generally

the orientation

angle

8 of the modulation wavevector, is well

represented by

the OPE in the whole q

regime

covered in the

figure.

ii)

As a

representative

case for moderate Prandtl numbers we have selected Pr

= o.71

(air,

see

[13]).

The results are shown in

figure

16.

Turning

from q~ to the left one has at first the

zigzag instability line,

which is soon

preempted (q

5 2.95

by

the Eckhaus

instability.

For q > q~

an SV-line

joins smoothly

into the E-line near threshold. With

increasing

E the

stability

line bends back to smaller q and reaches the value E

= o.46 for q

= q~.

With

regard

to the

rigorous

results one sees in

figure

16 that

stability boundaries,

in

partic-

ular the

SV-line,

are well

reproduced

in a

fairly large

E-range- Moreover the knot instability below the Eckhaus curve which it is not

important

in the present case is well described.

iii)

For

large

Prandtl

numbers,

like Pr

= 7.o

(water)

shown in

figure

lc the

stability region

is bounded from the left

by

the

zigzag

line and from the

right by

the knot

instability (K),

which

now lies above the Eckhaus curve

(see

[13]

).

We have also included the

CR-line,

which resides

on the left side of the Busse

balloon,

and the SV-line

(with

small

angle 8,

and very close to the Eckhaus

curve)

to the

right

of q~. The latter is

represented nearly exactly by

the

OPE,

while the rather moderate

discrepancies

for the other cases increase with E.

In the context of the OPE

approach,

medium Prandtl numbers Pr

(m I)

are the most

interesting

ones: otherwise

"upper"

limitations of the Busse balloon are neither described

by

the OPE for small Pr, because

they

are of the

oscillatory

type, nor for

higher

Pr, since the destabilization occurs at E-values too

large

for the

application

range of the OPE.

3. From order parameter to

amplitude equations.

In section 2 we have

investigated periodic

roll solutions of the order parameter

equations (7)

in Fourier space. The

description

of modulated patterns is

preferably

done in real space. It is then easier to

judge

the

importance

of mean-flow effects and the influence of terms

originating

(7)

ooff

Pr = 0.01

I

0Pt 0.06

GAL

0.04 ,'

,/

0.02

Nc

o.oo

a)

~ ~ ~.° ~.~ q ~

i o

Pr = 0.71 ', GAL Opt

I ',

~~ ,~ + o

o

~

".,

0 4

0 2 "~ ~

~

00 ~)

2.0 25 3.0 35 q 40

o

~ + GAL ---0Pt

~ ",

u sv o sv

0fl '.

+ cR o cR

o ',

+ ',

0.6

~~

o

~g +

° ~

~ k

+ v

0 2 ~~

°

°

6 a S~

O ~

~

0.0

~ ~~

2.0 25 30 3.5 q 40

Fig.

I.

a)

Stability domain for Pr

= o.01 calculated by OPE

(dashed line)

and by the Galerkin method

(GAL,

solid

line).

The dotted line represents the neutral curve

(NC).

To the left of the band center (qc =

3.l16),

we have E-destabilization, to the right SV, b) Stability domain for Pr

= 0.71

calculated by OPE

(dashed)

and by a Galerkin method (GAL, solid line). From bandcenter to the left one finds at first ZZ and for q < 2.9 E-destabilization. The E-curve

on the right is met by the the SV-curve which bends back towards qc. Included are also the knot instability curves (K) and the

neutral curve

(NC,dotted).

c) Stability domain for Pr

= 7.oo calculated by OPE

(dashed)

and by a Gaierkin method

(GAL,

solid

line).

Included are the ZZ-line (q < qc) an the neutral curve

(NC).

(8)

N°3 AMPLITUDE EQUATIONS FOR THE RBC 425

from the

elasticity

of the roll pattern. In this paper we confine ourselves to pattern

containing

wavevectors q near the critical wavevector q~

=

(q~,o).

For that purpose one introduces a modulation

amplitude A(x)

defined as:

A(x)

=

f dq

A(q)e~~~~~CJ~

(10)

D+

The

integration

domain

D+

covers wave vectors with

6q

=

(q

q~( small

compared

to (q~ and

correspondingly

the

amplitude A(x)

varies on a scale of the order

6q~~

The

explicit

construction of an

amplitude (or envelope)

equation is in

principle

done

by

a

transcription

of the OPE

(7)

into real space. The various coefficients a~ have to be

expanded

into

Taylor

series around q~ and translated into

spatial

derivatives of

A(x) according

to:

(-ib~)~ (-iby)" A(x)

=

fdq Q~

P" A(q)e~~~~~CJ~

(II)

With q qc "~

(Q,P).

This can be done

immediately

for the coefficients al and a2 of the linear part in equation

(7).

The

leading

contributions from the cubic part

a3(q

" qc, qi " +q~, q2 "

~qc) reproduce

the

usual

(A(~A nonlinearity

in real space. The direct attempt to generate derivatives in the cubic term

fails,

because the coefficient a3 turns out to have

nonanalytic

contributions.

They

are

immediately

identified

by divergencies,

if the

corresponding

derivative terms are constructed

numerically.

It is

possible

to trace back the

origin

of the

nonanalyticity [26,

27, 19, 37] to the second-order

terms

V2(q)

with q e s m o

(see Eq.(6)).

It will become clear in the

following

that the non-

analyticity

is

intimately

tied to the

velocity fields,

in

particular

to contributions characterized

by

a

nonvanishing spatial

average across the convection

cell,

the mean-flow terms.

They

need

a

special

treatment, which will be demonstrated in the

following.

CALCULATION OF THE MEAN FLow PART. The

starting point

for the calculation of the

mean-flow contributions is the

slowly-varying

part of the

inhomogeneous

system

(6)

in the adiabatic

approximation (at

"

o).

This is needed to derive the OPE

(7).

Thus we consider

the equation:

£(s)V2(s)

=

Inh(s)

or

£(s)(62, f2,g2)

"

(lo, Ii, Ig) (12)

The

inhomogeneity Inh(s)

derives from N2

(Vi,

Vi

(see Eq. (6)) by pairwise superposition

of contributions with

nearly opposite

wavevectors

(m

q~),

resulting

in slow variations with small wavevector s.

The

explicit

form of

(12)

is

presented

in

Appendix

A

(27).

It is shown there that the horizontal velocities

(u~,

My

(or correspondingly

the

potentials f, g)

behave

nonanalytically

in the limit s - o. One finds

finally

that the

nonanalytic

terms can be derived from a

"singular"

velocity potential

gj'~~(z, x)

=

B(x)(z~ 1/4)

with

B(x)

=

f dsB(s)e~~~

,

(13)

where

B(s)

fulfills the equation:

s~B(s)

=<

Ig

>

(14)

The

symbol

< > denotes an average

weighted

with a

Hagen-Poisseuille velocity profile

(see Eq. (40)).

After

isolating

the non-smooth part of the solution

V2(s)

and

subtracting

the

(9)

corresponding

contribution to the coefficient a3 a smooth

gradient expansion

in cubic order exists.

One arrives at a

complicated looking

system of two

coupled amplitude

equations:

(1 +

lTl~~

+ T2~~~ + T3~(~

~tA

#

E

(I ieib~ e2b] e3b(

+

ie4b(

+

iesb~b()

A

+

(~

b~

)b(

~ + in

al

+

r2bj

+

r3b]b(

A

~~

(A(~A-iai(A(~b~A-ia2A~b~A*

a3(A(~b(A a4A~b]A*

a5

(b~A)~

A*

a6(b~A(~A a7(A(~b(A a8A~b(A*

ag

(byA)~

A*

aio(byA(~A

+

iaii(A(~b~b(A

+

iai2A~b~b(A*

+ ia13

(b~byA) (byA)

A*

+ ia14

(b~byA) AbyA*

+

iai5A (byA) b~byA*

+ ia16

(b(A) (b~A)

A*

+ ia17

(b(A) Ab~A*

+

iai8A (b~A) b(A*

+

ia19(byA(~b~A

+ ia20

(byA)~ b~A*

+

ia21(A(~b(A

+

ia22A~b(A*

+ ia23

(b(A) (b~A)

A*

+ ia24

(b(A)

Ab~A* + ia25A

(b~A) b(A*

+ ia26

(b~A(~b~A

isi

AbyB

s2

(b~A) (byB)

s3

(byA) (b~B) s4Ab~byB

,

(isa)

(b(

+

b()

B

=

qiby A

b~ ~

b(

A* + c-c- +

q2b~ (iAb~byA*

+ c-c-

2qc

+q3by (iA*b(A

+

c-c-)

+ q4

(A*b(byA

+

c-c-)

+ q5

(b~A*b(byA

+

c-c-)

+q6

(b(A*b~byA

+

c-c-)

+ q7

(b(A*byA

+

c-c-)

+ q8

(A*b~b(A

+

c-c-)

+ qg

(b~A*b(A

+

c-c-) (15b)

One should

keep

in mind that the derivative terms

correspond partly

to the horizontal

gradients

in the

Boussinesq equation (1),

but are also

generated by expanding

the linear

eigenvectors

in powers of

(q~ q]),

which are involved in the derivation of the OPE

(7).

The numerical values of the coefficients have been calculated as rational functions in the Prandtl number

using

Galerkin methods and are available from the authors upon request.

In the

following

we shall refer from time to time to the

simplest

form of the

amplitude equation including

mean-flow effects [27,

38],

which is obtained from

(15) by disregarding

all

higher

derivative terms I-e- with e~, rj, a~ e

o), namely:

btA=EA+(~ b~-

~

b(

2

A-(A(~A-isiAbyB

,

(16a)

2q~

(bj

+

b()

B

=

qiby

(A

b~ ~b(lA*

+

-c-j (16b)

2qc The coefficients are

given

in that case

by:

(

= o.38476, si " o.01741 +

°'°°)~~,

~

-14.45439 Pr ~~~~

~ 0.27149

Pr~

0.00183 Pr + 0.00323'

(10)

N°3 AMPLITUDE EQUATIONS FOR THE ABC 427

Note that after a

rescaling (B

-

B/si) only

the combination siqi determines the

coupling strength

to the mean-flow.

In order to

display

the

amplitude equations

in the usual form we have rescaled time in terms of a characteristic time To (39, 34] and the

amplitude

A in terms of

(cr(qo

"

qc)( (see (8)).

A

strictly periodic

roll pattern with q

= q~

corresponds

to a solution

(A(x)(~

+ E and

B(s)

+ 0.

With the use of that convention the convective heat transport H normalized with respect to the conductive one

(H

+ Nu I, Nu: Nusselt

number,

[3]) near threshold reads as follows:

~

l ciP

~+

c2P-2

' ~~~~

The numerical constants obtained within our calculational scheme agree quite well with values

presented

in the literature (co " 2441.68, cl " 6.74845 x

10~~,

c2

" 1.18956 x 10~~

[39,

3]),

The derivation of the

amplitude equations (15)

is based on a

systematic expansion

up to cubic order in the convection

amplitude A,

which behaves near threshold as E~/~. The fact that

we have

kept

more derivative terms than is

usually

done needs

justification. Indeed,

if

lengths

in x-direction are scaled like

E~~/~,

in

y-direction

like

E~~H

and time like E~~, one obtains at

leading

order in E the conventional

NWS-amplitude equation.

All terms

+~ T~,e~, r~, a~ would lead to

higher

order terms in E and are therefore

disregarded.

Also the

amplitude

B

plays

no role at that order.

The

remaining higher-order

terms are of various nature.

Firstly

one has corrections to the time-derivative terms on the left-hand side of

equation (Isa) (coefficients

T~), which are of rather minor importance.

Secondly

in the linear operator one has on the

right-hand

side of

(Isa)

corrections

corresponding

to modifications of the

parabolically-shaped

neutral curve

(coefficients

e~ and r~

). Especially

the terms

involving al

and

al

are needed to describe

properly

the neutral curve for wavevectors not

directly

near q~. Furthermore derivative terms in the cubic terms of

(Isa)

are

included,

which will be motivated below in more detail. Of

particular importance

is the

coupling

to the mean-flow

amplitude

B

produced by

the four last terms in

(Isa),

where B is determined from

(lsb).

It is obvious that the inversion of the

Laplacian

on

the left-hand side of

equation (lsb)

leads to

nonanalytic long-range velocity

fields.

In the

following

section 4 it will be shown that the

amplitude equations

in the form

presented

in equations

(15)

lead to a

satisfactory

description of

stability regimes

of rolls with respect to

long-wavelength

disturbances when

compared

with the

rigorous

results

(see

Sect.

2).

More

specifically

it will turn out that

high-order

derivatives of the type

al, b~b( (see

the coefficients all

a26)

are, e-g-, necessary for the calculation of the

SV-instability boundaries,

e-g-, for

Pr = 0.71.

Anticipating

the detailed discussion in section

4,

we want to

emphasize already

here that the

importance

of

higher-order gradients

cannot be assessed

by simple

power

counting

arguments with respect to E.

There exist also

consistency

reasons,

why

derivative terms in the cubic part of

equation (Isa)

should appear. The

equation

for B contains

by

construction the

singular

contributions of the horizontal

velocity

fields. Their separation from the

analytic

parts is not unique. One could, e-g-, add

polynomials

in

b~, by multiplied

with

(b]~

+

b(~) applied

to (A~( on the

right-hand

side of

(lsb).

The

corresponding nonsingular

contributions for B can be

directly

calculated and inserted into

(Isa) leading

to modified derivative terms in the cubic

order, by

which the

changes

in the

B-equation

are

compensated. By

this method we could

partially

redistribute the coefficients. In any case terms +~ a~ have to appear, as

they

describe also the internal

"elasticity"

of the rolls.

Let us summarize what has been achieved so far. An

amplitude equation systematically

up

to cubic order in A without additional

assumptions

with respect to

length

and time scales has

(11)

been derived. The number of derivative terms

kept

can be

judged by comparison

with

rigorous stability

calculations and

by consistency

requirements. In that respect the

coupled amplitude equations

serve as a kind of normal form

description [40-42]

of the

stability regimes

of ABC

near threshold.

They

can be used as a

simplified

version of the

Boussinesq

equations in some cases, but are not

directly

accurate to some definite order of a small parameter

[32].

4.

Stability analysis

of roll solutions.

In this section we shall examine the

stability

of the roll solutions Ao

"

Fe~Q~

of the AE'S

(15) against long-wavelength perturbations

of the form

6A

= e~Q~

(cie~(~~

~+~YYJ + c2e~~(~~

+~YY))

e"~

(19)

The

quantity Q

+ q qc denotes the distance from band center. The

stability analysis

can

in

principle

at the best

reproduce

the

rigorous

Busse Balloon but

competing

destabilisation

mechanism, namely

mean-flow and

higher

derivative terms can more

easily

be

disentangled.

The calculation of the

amplitude

F is

straightforward

and when 6A is inserted into

(15),

the

growth

rate a can

easily

be determined from a 2 x 2

eigenvalue problem.

We express the modulation wavevectors s~ and sy in

polar

coordinates

s~ = Scos

8,

sy

= S sin

8, (20)

and

keep only

the

leading

terms in S The various

stability

boundaries E~tab

(a

=

0)

are then determined

by

the solutions of a

quadratic equation

in E

(S~

is factored out ):

C(~J

(Q, 8)E~

+

C(~J(Q, 8)E

+

C~°~(Q, 8)

= 0

(21)

The coefficients

C(°

can be calculated without

difficulty

from the

coupled amplitude

equations

(15):

C~°~

(Q, 8)

= -6 Q~

cos~8(~~ (22a)

C(~~(Q, 8)

= 2

cos~8(~

+

Q(-2 j2 sin~8

~c

+

(6

ei

f~

6 ri + 4 al

f~) cos~8

+ 4

sin~8 cos~8si

qi

f~) (22b)

C(~J(Q, 8)

=

(-2a7

2e3 +

2a8) sin~8

+

(-2

a3 + 2 a4 2 ei al +

a2~ ei~ ai~ 2e2) cos~8

+ -2

sin~8

~~ ~~ +

(2

a2 si qi 4 si q2 2 al si qi + 4q3 si 2 ei si qi

cos~8 sin~8

qc

+

Q(... (22c)

We have not detailed the

lengthy

and

complicated

contribution to C(~~ linear in

Q,

which

involves all coefficients of the AE'S

(15). They

are needed to ensure that the

stability

boundaries calculated from the OPE are

reproduced rigorously

to order

O(S~)

and linear in

Q.

The standard destabilization mechanisms are obtained

easily

from equation

(21)

and the

explicit expressions

for the coefficients

C(°

(12)

N°3 AMPLITUDE EQUATIONS FOR THE ABC 429

The Eckhaus

stability boundary (8

=

0)

E~tab +

EEck(Q),

which starts

quadratically

in

Q

from band center (E

= 0,

Q

"

0)

is

given

up to order

tJ(Q~) by:

c(I)(Q

e

~) ~j2Q2

~~~~~~~

C~~~(Q,

#

7r/2) (1 Q(~~3/~~

2£l1

3el))

~~~~

In comparison with the neutral curve

(Eneutr(Q)

"

f~Q~

+ the curvature of EE~k at

Q

= 0

is

larger by

the well-known factor three.

The

zigzag-instability

line

Ezz(Q) (8

=

7r/2)

starts with nonzero

slope

at bandcenter

(Q

=

o)

in contrast to the E~line and is

given by:

~~~~~~

~~~~~~

=

~~~ ~qisi

+

qc(~+

a7

a8)

~~~~

The last term in the denominator of

(24)

is

negligible

for not too

large

Prandtl numbers Pr 5 10 and a calculation based upon

equation (16)

is sufficient.

The

general

expression for Ezz

(Q)

in

equation (24)

is

equivalent

to the criterion

given

in

[39],

when the numerical expressions for the coefficients are introduced.

(q

qc 10.76

0.073Pr~~

+

0.128Pr~~

~~~

qc 0.166 +

23.04Pr~~

+

6.196Pr~~

~~~~

The

SV-instability

line

Esv(q),

which emanates from

bandcenter,

is

given by

the maximum of the

following expression

with respect to

8,

which is

easily

obtained from the ratio of C~°~

and

C(~J

~~~~~'~~

cos2

8(1 3Q(3r3 /f~

a~~-~e~~~ ~iqi

sin~ 8)) 3Qqp~ sin~ 8'

~~~~

It is evident that the SV-destabilization can dominate the Eckhaus process

only

for

Q

> 0 as

a result of contributions of order

tJ(Q~)

from the denominator.

An interesting question concerns the

back-bending

of the SV-line for Prandtl numbers Pr m I.

In

particular

the value and

slope

at q = q~

(Q

=

0)

is obtained

analogously

to

(24)

from the relation

Esv(Q,8)

=

-C~~J(Q,8)/C(~J(Q,8). By

minimization with respect to 8 we find

always

8 to be near ~ for Pr near I and

Q

near zero. For the

simplified

version

(16)

a

4

backbending

of the SV-curve cannot be achieved.

Because of the

interplay

of the

higher

derivative terms, which

decisively

govern the

stability

boundaries for Pr m I, it

might

be

questionable

if numerical model simulation of

amplitude equations

or their

isotropic

counterparts

(Swift-Hohenberg equations) (see Appendix B),

where

typically

many

higher

order-terms are

neglected

[43] can be

reliably

related to the

experimental

situation.

COMPARISON BETWEEN ORDER PARAMETER AND AMPLITUDE EQUATION. In this Sectiou

we want to compare in more detail the

stability

domains calculated from the

amplitude

equa- tions

(15)

and the OPE

(7).

Our main concern is the influence of the additional

approximations

involved in the derivation of

amplitude equations, namely

the truncated expansion in powers of

(q q~), leading

to the derivative terms in

(15). By

construction all three methods referred to in this paper

(rigorous

Galerkin [3], OPE and

AE)

are equivalent for small E and q m q~, if

one considers

long-wavelength

disturbancies (s( < qc of a

periodic

pattern. It is therefore not

(13)

surprising

that

directly

above

threshold,

in a narrow

region

around q~, a

satisfying descrip-

tion of the

corresponding stability

boundaries

(E, ZZ,SV)

is

always

achieved

by

means of the

amplitude equation.

For the detailed discussion it will be

advantageous

to consider

separately

the different values of the Prandtl number used in

figures

la-lc. The

figures

may also be

consulted,

when

judging

in

principle

the range of

validity

of the APE for

increasing

values of E, because one is limited in any case

by

the

reliability

of the OPE. One also should

keep

in mind that there must

always

exist a

description

in terms of the

AE,

which coincides up to

arbitrary

accuracy with the

OPE,

if

sufficiently

many derivative terms are

kept,

since all

nonanalytical

contributions are absorbed in the

B-equation (lsb).

Let us start with the extreme low Prandtl number case

(Pr

= 0.01, see

Fig.

la for the

rigorous results).

The upper part of the

rigorous stability regime

is not accessible

by

the OPE and the AE. The lower part of the

stability

domain calculated from the AE is shown in

figure

2a

(solid line).

Included are the results from the OPE

(triangles,

see

Fig. la).

One sees that near q~

=

3.ll the

amplitude

equation works quite well. For (q q~( > 0.I the

stability boundary

starts to deviate downwards from the OPE

(triangles).

A more detailed

analysis

shows that with

increasing

distance from q~ some of the

higher

derivative terms have a rather

disadvantageous

effect. The best agreement between OPE and the

amplitude

equation is

obtained,

if some cubic derivative terms

(a~,

I = 21

26)

in

(Isa)

are set zero. One gets the short-dashed curve, which coincides in the whole

q-regime

shown

perfectly

with the OPE results. In

comparison

to the OPE one concludes that some nonlinear derivative terms

apparently

balance each

other,

one would have to include even fourth-order derivative terms in the cubic part of the

A-equation

to compensate the third-order

derivatives,

which lead to unwanted effects for q < q~.

Finally

we would like to

mention,

that

by keeping only

the

leading

terms as done in

equation (3.),

one gets an E~line

(crosses)

in the whole

q-regime

in contrast to the

rigorous

SV-line to

the

right.

One has to include at least the

rib(A

term of the linear operator and obtains a

stability boundary

which deviates from the solid curve

only quantitatively.

Let us now turn our attention to intermediate Prandtl numbers

(Pr

= 0.71, see

Fig.

lb for

rigorous results).

The boundaries

(solid line)

of the

stability

domain calculated from the AE

(15)

is shown in

figure

2b.

Clearly

one has

satisfactory

agreement with

rigorous

results and the OPE

(triangles)

up to

fairly high

values of E

+~ 0.8 near the bandcenter. In

particular

the

general

behavior of the

backbending SV-line,

which is

typical

for Prandtl numbers

-J I,

(see

e-g-

ii Ii)

fits well and the

slope

at q~ is

reproduced rigorously.

For the SV-curve the

higher

order derivative terms are of

particular importance.

If for

example

all contributions from the

coefficients a~, I

= 21,.

,

26 and q~,I

= 4,.

,

9 are left out one gets a

stability regime (long dash),

which is

closed,

in contrast to the

rigorous results,

but which agrees

satisfactorily

for

E > 0A on the

right

and E > 0.3 on the left.

If the

higher

derivative terms are left out

totally,

as in equation

(16),

the

stability

boundaries

are of the

E~type

for all q

(short

dashed

line).

But for q < q~ the agreement with the OPE results is even then

improved,

because

analogously

to the Pr

= 0.01 case the a~, I = 21,.

,

26 contributions are rather unfavorable for q~ q < 0.5.

Finally

we come to the

large

Prandtl number case

(Pr

=

7,

see

Fig.

lc for the

rigorous results).

The solid line in

figure

2c describes

again

the lower

stability

limit obtained from the full

amplitude

equation

(15).

One should

keep

in mind that the

limiting

curves

(E)

for q > q~

are in

principle irrelevant,

because the

short-wavelength

CR

instability

dominates

(see Fig. lc).

The new feature is introduced

by

the ZZ-line for q < q~. The best

description

of the

rigorous

results is achieved

by

the

simplest

form of the

amplitude

equations in

(16), corresponding

to the

analytical expression (24).

The ZZ-line increases

nearly linearly

as function of q. Because with

increasing

E lower values of q come into

play,

the inclusion of the

higher

derivative terms

Références

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