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HAL Id: jpa-00247519

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Submitted on 1 Jan 1991

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Stability of permeative flows in 1 dimensionally ordered systems

Jacques Prost, Y. Pomeau, E. Guyon

To cite this version:

Jacques Prost, Y. Pomeau, E. Guyon. Stability of permeative flows in 1 dimensionally ordered systems.

Journal de Physique II, EDP Sciences, 1991, 1 (3), pp.289-309. �10.1051/jp2:1991169�. �jpa-00247519�

(2)

ClassificaUon

Physics

Abstracts

47.20 61 30

Stability of pernleative flows in I dimensionally ordered

systems

J. Prost

('),

Y. Pomeau

f)

and E.

Guyon (3)

(~) Laboratoire de Physico-Chlmle

Thkonque

(*)

f)

Laboratoire de

Physique StaUstique (**)

(3)

Physique

de la Matidre

Hktkrogdne (***)

(Received 28 December 1989, revised 6 June 1990, accepted 5 December 1990)

Rksumk. On rencontre des structures en couches dans des

systdmes thssipaUfs

tels que les rouleaux convectifs de

Rayleigh-Bdnard

et dans les cristaux

hquides (smectiques

et cholestkri-

ques)

Nous

prbsentons

in une

description gbnbrale

de la stabihtb de ces structures dans le cadre du forrnahsme de la diffusion de phase, lorsqu'elles sont sournlses I un

champ

de force extbneur

(bcoulement, champ klectnque)

aglssant I

angle

droit de la direction des rouleaux, en fonction des conditions aux hmltes La solution unidimensionnelle d'kquihbre avec des conditions aux hmltes

ngides

pour la

phase

conduit I un effet dkcouvert par Pocheau et

Croquette

~P C ) dans la

convecUon de R B. et mettant en jeu la coexistence de zones dilatke et

compnmke

Cet effet a un

analogue

dans les

cholestknques

Avec (es mdmes conditions aux hmltes, nous

gknkrahsons

l'instabilitk bien connue d'ondulation, obtenue dans les

smectiques

sous l'effet d'une thlatation,

au cas d'une force transverse I la fois du point de vue de la stabihtk hnkaire et dans le

rdglme

hautement non linkaire Nous

suggkrons

aussi la

possibilitk

d'obtenir des structures fractales Pour des condiUons aux hmltes mixtes, on

prkvoit

l'existence de

rkgimes dkpendant

du temps et

mettant en jeu la nuclkation de nouvelles couches alnsi que cela a aussi ktk observk dans les

expknences

de PC

Abstract.

Layered

structures are met in

dissipative

systems, such as

Rayleigh

Bknard rolls, as well as m

liquid crystalline phases (smectics

and

cholestencs)

We present here a

general

description, m the framework of

phase

dynamics, of the stability of these structures when

submitted to an extemal force field

(flow,

electnc field) acting

perpendicular

to the roll axis for

vanous

boundary

conditions The one-dimensional

equilibrium

soluUon with fixed

boundary

conthtions leads to an effect, discovered

expenmentally by

Pocheau and Croquette on

Rayleigh-

Bknard rolls in the presence of a transverse flow, and

involving

the coexistence of

compressed

and dilated rolls, this effect has a known counterpart in cholesterics

Using

the same

boundary

conthtions, we

generalize

the well known undulaUon

instability

obtained under a dilative stress to the case of the action of a transverse force both from the point of view of linear

stability

and m the

highly

nonlinear limit. The

possibility

of

observing

fractal structures is mthcated. For mixed

boundary

conditions, it is

possible

to have a sustained Ume

dependent

behavior

involving

the nucleation of new

layers

as also observed m the above mentioned expenments

(*)

URA 1382, ESPCI, 10 rue

Vauquehn,

F-75231 Pans Cedex05, France

(**)

URA 731, ENS, 24 rue Lhomond, F-75231 Pans Cedex 05, France

(***)

URA 857, ESPCI, 10 rue

Vauquehn,

F-75231 Pans Cedex05, France.

(3)

1. lntToducfion.

It is a priori not obvious that one can use the same

equations

for

describing

the

dynamics

of

out-of-equilibrium

and

thermodynamic systems. However, spatial symmetry

sets require-

ments on the structure of the

equations

which are the same m both cases The absence of

Onsager

relations and of a

thermodynamic

function m the case of

out-of-equilibrium systems

allows for a

larger variety

of terms than with

thermodynamic

systems, but those terms which exist with the latter also exist with the former. ThJs is

particularly

true with

layered

structures

(smectic

or cholestenc

liquid crystals, Rayleigh-Bknard

rolls

.)

for which the linearized

equations

of motion are

essentially

similar

[I].

One of the most remarkable char>ctenstics of the

dynamics

of

layered systems

is the existence of a mode called permeation. In its

simplest form,

it tells that a flow m a direction

orthogonal

to the

layers

tends to carry the whole

structure

along.

Whether it

really

can or cannot

depends

on

boundary

conditions It is clear

that this

tendency

to

drag

the structure

along

exists irrespective of the fact that one is

dealing

with a

thermodynamic

or an

out-of-equilibrium system [2]

More

generally,

the

permeation phenomenon

expresses the fact that an external force drives a difference between

layer

and

barycentnc velocitiis.

In the case of

cholesterics,

it is associated with the rotation of the local

axis as observed

long

ago

by

Lehmann m a temperature

gradient

at small

amplitude [3]

and revived m the nice

quantitative

expenments of Madhusudana and Pratiba

[4]

using a D-C electric field. A natural framework for

understanding

these observations is

provided by

the Leslie

hydrodynamic theory [5].

The connection made

by

Helfnch

[6]

between the local

rotation m a cholesteric and permeation makes it

possible

to

incorporate

the Lehmann effect

m the framework of the

hydrodynamics

of

layered systems [7,

8]: a

permanent

bulk rotation of the order

parameter (I.e.

local

optical

axis m cholestencs or the

phase

of the

layers

m the

smectic

case)

takes

place

with an

angular velocity proportional

to the

_extemal

field at small

amplitude

m the case of free

boundary

conditions. Direct observations of permeation in either

case have been found

extremely

difficult for reasons which will be discussed in the conclusion of'thJs paper. However a clear

experiment by

Clark

[9] provided

a convincing indirect evidence for the existence of

permeation

in smectics.

The case of out of

equihbnum

roll structures has been studied

by

Pocheau and

Croquette (P.C [10].

Their

analysis

of their

expenment

on the «compression » of

Rayleigh-Bdnard (R.B.)

rolls under the effect of a transverse

flow,

uses a

generahiation

of the

phase dynamics equation (

II whJch is identical to that

descnbmg thermodynamic systems.'The

very existence of the

non-homogeneous

compression m the P-C-

expenments

is a direct

proof

of the

validity

of the permeation concept in out of

equilibnum

systems

However thJs remark is not

only

of interest for what concems the

similarity

of the

equations,

but it has also some flesh on it as one

might

expect some s1mllarities in the

physics

too. In thJs respect, it should be noticed

that,

in their expenment, Pocheau and

Croquette

observed distorted but

steady patterns

as well as a

periodic

nucleation and destruction of the rolls at the ends of the convection cell. The

present

work was simulated

by

the above

experimenjs

It is a

general stability analysis,

in the framework of the

phase

diffusion

equations,

of the

stability

of

layered

structures submitted to a transverse extemal force field We introduce the

general equations

which will be used

throughout

the paper m section 2. In section

3,

we review the basic solutions

corresponding

to a flow normal to the

rolls, insisting

on the

importance

of

boundary

conditions

In section

4,

we show that the static deformation obtained

by

Pocheau and

Croquette

may

become

linearly unstable,

if a transverse modulation is allowed The

interpretation

of thJs effect is as follows m the

equation

of motion, some terms represent a kind of

elasticity

and express the

property

that the structure has a

preferred

wavenumber

[11]

In the P-C-

effect,

(4)

part

of the structure is

compressed

and part of it is under extension. Therein the wavenumber

may increase

locally

and so can opt1mlze the energy

by adding

a modulation m a transverse

direction. The

corresponding instability generahses

the well known undulation

instability

obtained under a dilative stress and m the absence of flow m smectics

[12, 13].

It is

analysed

m

section 3 both from the

point

of view of the linear

stability

and in the limit of a very

large

constraint A

key

feature of our

analysis

is that all

interesting phenomena

occur at

vamshJngly

small velocities thJs

corresponds

to the

large

box limit

(I.e.

a

large

number of

penods

N m the

system)

We

study

both the linear

stability

close to threshold V l

/N~)

and the

strongly

nonlinear regime

(keeping

V « I

IN).

The

instability

takes

place

when the

phase

is fixed at

both ends of the structure

(it

should also be

possible

to observe it with mixed

boundary

conditions)

In section 5 we will see that a sustained time

dependent

behavior is

possible

with different-

boundary conditions,

m the absence of transverse modulation of the

rolls,

it

corresponds

to the creation-annihilation of rolls as observed

ixpenmentally by

Pocheau

ind Croquette.

More

complicated phenomena

can also be observed and have been

analysed

using different

boundary conditions

on both sides In the presence of a flow whJch forces a

winding

of the

phase,

new rolls have to be

continuously

added inside the structure, thJs cannot be described within the framework of the

phase dynamics

which excludes fast events such as the nucleation of new

rolls,

in the

Rayleigh-Bdnard terminology

» that we shall use

throughout

this paper.

However this fast

dynamics

may be considered as instantaneous

(compared

to the

phase dynamics).

This allows us to include it m a consistent fashJon into the

phase dynamics

equations, as shown m the last section, where we also sketch an

analysis

of_the behavior when

nucleation of new

wavelengths

occurs

2. General

equations.

It is worth

starting

with the smectic

hydrodynamic equations. They

are valid m the

long wavelength,

low

frequency,

small distortions

limit,

and can be derived using standard

procedures [8].

In the isothermal

incompressible

case, which is relevant to our current

considerations, they read,

in their hneanzed version

~"

V~

=

Ao

~~ +

pE~ (I)

at _8u

p

~~~

=

V~P

8~~ ~~ +

V~«]~ (2)

(

=

«E~

+ p

~~

(3)

Div V

=

0

(4)

~~

+ Div J

=

0

(5)

u is the

layer displacement

variable as

defined'in

the

appendix,

z the

unperturbed layers

normal axis, V the

barycentnc velocity,

F the elastic free energy of the smectlc

[7, 8]

F

=

I B °"

~

+ K

~~

+

~~

~

dr

(6)

2 3z ax

by

The first term describes the

compressional

energy of the smectic

layers,

and the second their

bending

energy. The ratio A

=

(K/B)~'~

has the dimensions of a

length.

It is a « microscopic »

(5)

quantity

of the order of the

penod

of the structure and is called the de Gennes

screening length [7].

This is the existence of thJs

microscopic length

which is the source of the

originality

of one-dimensional order in two or three dimensions.

E~

is the z

component

of any extemal force

having

the sytnmetry of an electric field

(it

could be a

temperature gradient

for

instance),

p

the mass

density,

P the pressure,

«]~

the

dissipative

part of the stress tensor and

£

the flux conjugate to the force

E~ A~,

p and « are

dissipative

coefficients. Note that because of

Onsager relations,

p enters both

equations (I)

and

(3).

Equation (I)

is the permeation

equation:

a

velocity

field V~ or an extemal field E- may either set the structure into motion via

~",

or distort it vta

~~. Equation (2)

is a

at 8u

generalization

of Namer Stokes

equations.

The

dissipative

stress tensor involves three viscosities m the

incompressible

limit. Note that ~~

is a force acting

along

the z direction 8u

Equation (3)

expresses the current

and/or

the

layer

distorsion

resulting

from the action of the field.

Equation (4)

gives the

incompressibility

condition and equation

(5)

is the conservation law for the

extenjive

quantity

Q (charge

if

E~

is an electnc

field)

the flux of which is

£.

As discussed m the

introduction,

the

expenmental

relevance of these

equations

has been

reasonably

well established

[14].

What about out of

equihbnum

structures ? A

frequent description

involves the use of a

complex

order parameter :

#

=

#o e'4 (7)

This is

really

not different from a smectic A

phase

for which such an order

parameter

has been

widely

used to describe the nematic-smectic A transition

[7]. Equations (1)-(5)

are valid in the so-called

hydrodynamtc ltmit,

where

#o

may be considered constant, that is for

wavelengths large compared

to correlation

length charactenzlng

the modulus fluctuations and

controlling

the size of the core of dislocations. In out of

equihbnum

systems it is called the

large

box

limit, similarly

to the smectic case, the use of a roll

displacement

vanable is

meaningful

in

what is called the

phase

approximation

[11]

fb =

qo(z

+

U) (8)

Can one use equations

(1)-(5)

without any precaution m the latter case? As

already announced,

expressions which result from

spatial

symmetry are

necessanly

s1mllar

However, Onsager

relations have no reason to be satisfied. As a

result,

instead of one coefficient p, one has to use two different coefficients p and

p'

m

(I)

and

(3) Similarly,

attention has to be

paid

to the viscous term in

(2)

m an infinite smectic it reads (1~, are

viscos1tles)

°~~j " ~ 'i2

~ij ~l'i3

'i

2)(Viz ~jz

+

~jz ~iz)

I'll+'i2~~'i3~~'i5+'i4)~iz~jz~zz~1'i5~'i4+'i2)~ij~zz. (~)

The same expression cannot be used m the case of roll systems with

rigid boundary

conditions,

such as m standard

Rayleigh-Bdnard

cells.

Indeed,

fnction results from the existence of an

averaged

fluid

velocity

with respect to that of the walls.

Thus,

m the reference

frame,

where the walls are at rest, one has the

relationships Vjtr~j

=

iii

U~

Vjtr~j

= ~ U~

~~~~

In which

iii

and

A~

have the dimensions of a

viscosity

per

length squared iii

=1~ max

(d~~, (A~I~)~~)

A~ =l~d~~.

(6)

Equation (10)

holds as well for smectics bounded

by parallel plates

with the

layers perpendicular

to the walls

[9].

Note

that, conversely,

m the case of an

instability

with free

boundary

conditions

equation (9) holds,

because of Gahlean invariance

(i

e.

only gradients

of

v can

play

a

role, and,

because of

spatial sytnmetry, they

have to be second

denvative).

The last point concems the difference ~"

v~)

The occurrence of this term in

(I)

at

results from Gahlean invanance

looking

at the

system

from a moving frame of reference should not

change

the

physics.

In an

out-of-equilibnum system,

one can construct Gahlean

invariant

expressions involving

not

only

the

background

fluid

velocity,

but also the walls

velocity.

TbJs

implies that,

m a frame in which the walls are at rest, the coefficient

affecting

u~ is not

necessarily

one. The

tendency

for a flow to

drag

the structure is

certainly

there

(and

allowed

by symmetry) but,

in the ideal case, the limit

drag velocity

needs not be

u~.

The lmeanzed

equations

read now :

~-AvUz=-Ap( ~( +HEz (")

3u~

~ SF

~ ~

(12)

P

$

"

~'~

'z

$

" ~

£

=

«E~

+

p'

~~

(13)

3u~

3v~

G

~

G

~ ~ ~~~~

~~+DivJ=0.

(15)

Equation (14)

results from the fact that

u~ is zero at the walls. F is a

Lyapunov

functional which is identical to

(6)

because of

spatial

sytnmetry Note that the expression

(6)

would not be relevant for

Taylor-Couette

Tolls or convection m

planar

nematics

[20] because,

m these two

problems,

there is an intnnsic direction of the rolls Note that the x

component

of

(12)

could exhibit a term

~~"

It does exist in smectics, but is included m the pressure

[7].

In

ax 3z

what

follows,

its inclusion would

simply change

the elastic constant B. In order to discuss the instabilities of section

4,

we will need a nonlinear version of equations

(I1)-(15).

For the same

reason as m smectics

[7, 12],

the essential non

linearity

comes from the

rotationally

invariant

expression

of F as described in the

appendix.

The

rotationally

invariant F involves

E(u)

=

~"

+

(Vu

)~ instead of ~"

),

and the covanant expression of the curvature term

3z 2 3z

Div n, can be

replaced by A~u [7, 19]

:

F

=

( (E(u)

+ A

~(Ai u)~)

dr.

(16)

There are many other nonlinear terms to be added to equations

(I I)-(15),

the most obvious of which expresses convection in equation

(11), namely

:

A

~ u~

V~u (17)

It has to be

compared

to u~ in order to estimate its

relevance,

that is

V~u

has to be

compared

to unity. We will show

that,

except m

boundary layers,

the

description

of which is

beyond

the

(7)

scope of this

article, V~u (A IL

Since A is a «

microscopic length,

L can

always

be chosen

large enough

for~ that ratio to be small

compared

to

unity.

It is worth

giving

another

example illustrating

the role of the small

parameter AIL

equation

(11), together

with the defi-

nition(16)

of

F,

involves the

product A~B

=

D,

whJch has the dimension a of diffusion

constant. In a

complete

nonlinear treatment one should

keep

track of the

dependence

of D,on

u From

sytnmetry,

one should write expressions of the

type.

'

D(~)

~

D0

+

Dl ~]

+

('8)

Dimensional

analysis implies

Dj ~/Do

'

(19)

We will show that the critical

velocity

for

setting

the

instability

is given

by

:

u~ ~

DA

IL

~

(20)

which

immediately yields

D(u Do

+

~

(21)

L

Again

in the «

large

box » limit thJs term is

entirely negl1glble.

ThJs

possibility

of

keeping only

the nonlinear terms due to rotational invariance in

F,

is a unique feature of one

dimensionnally

ordered systems.

3. Onedimensional

equilibrium

solutions.

In the present section we consider one-dimensional deformations u

(z,

t

)

which

correspond

to

translation,

dilation or

compression

of rolls. The

incompressibility

cond1tlon

requires

a

uniform

velocity

field u~

= uo the flow is then

impoied by

the inlet and outlet fluxes at the

extremities of the system as in the P-C- expenment. The z component of

(12)

defines the

pressure,

whilq

u~ + 0 satisfies the x component.

Steady

state solutions involve constant currents

~"

find

£

As a

result,

we are left with just two equations

t

J~

=

«E~

D' ~

~ (23)

(with

D'

=

lip').

Equation (23)

defines the flux due to the extemal force

(heat

flux if

E~

is a temperature

gradient,

electric current flux if

E~

is an electric

field)

we assume that the system is

impedance

matched for J~.

Equation (22)

is

interesting

in that it illustrates very

simply

how

boundary

conditions on

u are important in

determining

the type of behavior which will be observed

expenmentally Equation (22)

can be rewntten

= V + D ~

(24)

t

~

in which- we have set V

= A

~

Vo

+

pE~,

which insists on the

equivalent

role

played by

a flow and -an extemal field

(althougll

their

physical

ongm and time reversal behavior is

different).

(8)

Equation (24)

is a linear version of the convection diffusion

equation

for the

phase dynamics [11, 15-17]

and has also been discussed in the context of cholestencs and smectics

[5-9].

Let us consider a

sample

of thJckness L

(0

< z < L

)

We can calculate

easily

a number of

unperturbed

solutions for vanous

boundary

conditions.

They

are obtained quite

naturally

in

experiments.

In

liquid crystals,

free

bouqdary

conditions

correspond usually

to free

liquid

surfaces and

ngld

B-C- to the material in contact with a solid surface with

appropriate

surface

treatment. In R.B.

rolls, ngld

B.C.

correspond

to solid lateral walls whereas free B-C- can be obtained with

smoothly

varying

properties (18).

i)

For free or Neuman

boundary

conditions

~"

(z

=

0)

=

~"

(z

=

L)

= 0

(25)

3z 3z

we

get

the solution of the Lehmann rotation :

u = Vi

(26)

ii)

For

ngld

or Dinchlet

boundary

conditions :

u(z

=

0)

=

0,

u

(z

=

L)

= uo

(27)

the solution is static :

v zuo

"

2 D ~

~~

~ ~

L ~~~~

~

It describes the P-C- effect. An

equivalent

effect had been

predicted by

Leshe

[5l'for

cholestencs lvhen L is

equal

to an

integer

number of 2

ar/qo,

the

equation (28)

descnbes a compression of rolls m the downstream region

(z

<

L/2)

and a dilation m the

upstream

one as

observed in the P.C.

expenments.

Note

that,

m these

expenments,

the

change

m

wavenumber induced

by

the flow was not

always

small.

ii)

For mixed conditions :

u(z=0)

=0

)(z=L)=0 (29)

a

steady

solution is obtained

u =

~'

z(2

L z

(30)

In the

following paragraphs,

we will

study

the

stability

of some of those

simple

solutions

by considering

two dimensional

perturbations

m case

ii) (chapter 4),

defect nucleation in one dimension in case

iii) (chapter 5)

4.

Beyond

the one-dimensional situation.

4.I FORMULATION. In this section we consider the same

problem

as m the

preceding

one

with

rigid boundary conditions,

m a system of infinite extent m the x direction. To look for the

stability

of the solution

(28) (called

uo in the

following),

we allow for the

possibility

of fluctuations

depending

on coordinates x and z. For the sake of

simplicity

we do not add the extemal field

E~.

(9)

The

equations

reduce to :

~

~

~~ ~

P

~~

~~~~

~

~i $ ~i f

~~ ~~ ~~~~

P

(I

"

$

~

xx ~x ~~~~

3v~

3U~

~

+

~

= o.

(34)

In view of translational invariance and the autonomous character of

equations (31)-(34)

with respect to time, we choose to

study perturbations

of the form

u(z,

x

t)

=

uo(z)

+ w

(z) Cxp(iqx

+

)~

([ii i i iiiiiii~~iii ii~i ~~~

.-

(35)

P

(Z,

x t

)

=

Po

+ 8P

(Z,

x

,

t

)

Since we will be

looking

at the onset of

instability

and at nonlinear

steady

states, we can

neglect

the acceleration terms in

(32)

and

(33)

We then eliminate p and

V~

and transform

equation

(32)

in

O=-~~-A~~V~(z)+~)~~ (36)

8u q

z

Again anticipating

~

~

(

,

q~

~

(

AL

)~

~, one obtains : 3z

V~(z)

=

~~

l + O ~ ~~

(u)

~~

(uo) (37)

L 8u 8u

That is for

(31)

:

~'~

= D

~~ ~"°

q~

+ A~

q~)

w

(38)

at az °z

IA

~

where D

=

A~

+

B,

and terms of order

AIL

smaller than those retained have been

Azz again omitted.

4 2 LINEAR STABILITY With the chosen form

(35),

« becomes an

eigenvalue

of a linear

differential operator with q as a parameter :

(« M~)

wo = o

(39)

with the

boundary

conditions wo

= 0 at z

=

0 and

L,

and the

following

definition for the linear

operator M~

:

M~

= D

(3~/3~ q~[-

V

(z L/2 ID

+

uo/L]

A~q~)

(40)

m which

again

V

= A~

Vo

(10)

As equation

(39)

has a coefficient linear m z, it can be solved

by Laplace's

method Tlus

yields A1ry

functions that become

simple

circular functions if the external constraint V is zero.

4.2.I V

= 0 case. The

quantized

« values are

"n "

Dl'T~lL(2~+1)l~~+ "0qiL

+

A~q~),

where n is a natural integer.

The less

damped

or most unstable mode is at n

=

0 and for a wavevector

q~" ~"0/(2LA~)>

with the

eigenvalue

"0 ~ D

l'TiL~ Uil(4 L~ ~)j

,

which shows that the

parallel layered

system can become unstable in the absence of an extemal force field V if a

large enough imposed

dilation uo is

putting

the

systeit~

out of

equihbnum («

~ 0

).

The

marginal stability

is reached with uo

= 2 vi and

corresponds

to a dilation with respect to

equilibrium (the

definition of the sign of uo is discussed in the

appendix)

The

corresponding instability

tends to restore the

optimal

and shorter

wavelength by building

an undulation as

permitted

in the x direction This situation has been well studied

in smectlcs

(m particular

see

(12)).

4.2.2 V # 0.

Coming

back now to the

original problem,

that is to

perturbations

around the

basic solution given in

(28),

we shall use as a new vanable

z'=z-zo

with zo=

L/2

+

D(uo/L

+ A

~q~+ «/Dq~/V

The coordinate zo

corresponds

to a

turning point

for the

problem

and defines the domain of existence of the dilation

instability.

This

change

of coordinates allows us to recover the familiar

Airy equation

:

d~w/dz'~

+ bz' w

= 0

with b

=

Vq~/D.

It has the

general

solution.

w = z

~'iaJjj~(2 b~'~z'~'~/3)

+

flNjj~(2 b~'~z'~'~/3)]

where a and

fl

are

arbitrary

constants for the moment and J and N are Bessel functions.

Putting

zj

= L zo, one finds that the

boundary

conditions for w impose a transcendental

equation

to be satisfied

by

«.

~l/3(~

b

~~~Z)13) fi~l/3[~

b~~~(~20)~~~/3) "

fi~l/3(~

b

~~~z/~13) ~l/3[~

b ~~~(~20)~~~/3)

(41) Indeed,

this last expression allows us m

pnnciple

to find

numencally

the unknown

quantity

«.

Let us consider for the moment the onset of

instability.

ThJs is reached when

« = 0 is a solution of

(41)

which then gives a relation between the

quantities

uo, L, V and q at

threshold. We know

already that,

if

V=0,

the onset of

instability

is reached at

uo = 2 vi and

q$

=

ar/(AL)

We

expect

thJs to remain true as

long

as V is

negligible.

In scaled quantities,

by comparing

terms in

M~

we can express this cond1tlon

(V negligible)

as

V « V~ = «DA

IL

~ or as C « ar

,

the dimensionless number C

=

VL~/(DA

will be used in

the

following

to charactenze the relative

efficiency

of the

dnving

force

(it plays

the role of a Pedet number for the

problem).

If thJs

inequality

is true, the source of the

instability

is m the

boundary

cond1tlons

imposed

upon u.

On the other

hand,

if V

~ V~ or C

~

l,

the source of

instability

is the field V. In thJs

limit,

and at threshold «

=

0,

one has zo m

L/2

+ DA ~

q~/V

and zj m

L/2

DA

~q~/V.

(11)

If

Vi V~,

the last term

on the

right

hand side of the expressions of zo and zj is

negligible

as

compared

to the first one.

Thus,

one can

replace

the

equation (41) by

:

~l/3(Q~~~) Nl/3(~ lQ~~~)

"

~l/3(~ lQ/~ fi~l/3(Q~i (~2)

where

Q~

is defined

by Q~

=

q~(VL~/D)"~

The pure number

Q~

is the smallest root of

(42), corresponding

to the onset of linear

instability.

One can check

that,

m the crossover region

(V

m

V~),

the expressions q~~ and q~o

coincide,

up to a numencal factor In the absence of

imposed

dilation

(uo=0),

thJs

implies

that the

instability

sets up for

VmV~

with q~ m

(ar IA L)"~

One

expects that,

if V is much

bigger

than this threshold

value,

a whole band

of wavenumbers will become unstable.

Let us estimate the

shape

of those two borders. Let us assume first that the argument of the Bessel functions m

(42)

remains finite on one side of the band of unstable wavenumbers. ThJs

yields the,long wavelength

limit q

m

Q~(D/VL~)"~

as obtained above.

The other side of the unstable band is reached when the two terms

m'zo

and

zj

( =,L zo)

are of the same order of

magnitude.

ThJs

implies

q m

(LV/DA ~)"~

and allows to use the

asymptotic

WKB-like expression for the Bessel functions m

(41).

However it is

more, transparent to come back to the

onginal

equations With the

scaling

Z

=

z'/L

and

q =

Q(LV/DA

~)~'~, one transforms

(38)

into

d~wjdZ~

+

Q~( VjV~)~ (Z lj2 Q~)

w

=

0,

with the

boundary

conditions w

= 0 at Z

=

0,1.

This has solutions at

large (V/V~)~

if a

« classical »

region

of the

potential Q~( VI

V~)~

(Z 1/2 Q~

exists, that js if thJs

potential

is

attractive somewhere~ for

particles

w~th energy zero. Otherwise one would have

purely

exponential (non oscillating)

solutions which would not fit both

boundary

conditions. As the

largest

value of the

potential

is reached for Z

=

I, having

a pos1tlve value of the

potential

imposes

Q~<1/2.

This condition defines

completely

the short

wavelength

border of the

stability

domain at

large

C's with a variation

of_the

cntical wavevector as V~'~

ThJs ends the linear

stability analysis

of our

equatioii (36).

Below We shall consider the domain of very

strong nonlineanties,

reached at

large

C's

(but

still m

agreement

with the

inequality

C «

L/A ).

4.3

I~ONLINEAR

REGIME. The

study

of the nonlinear domain is made

formally simpler by keeping

the order of

magnitude

coming from the above

developments:

u~c

A,

xx

(AL)~'~,

z~cL Then the intensity of the extemal constraint V is measured

bf

the

dimensionless number

C,

and the nonlinear equation for the

steady

solution

reads,

after

making

a

change

of variables uA

- u,

x/(AL)~'~

- x,

z/L'$z~

c

=

(ui

+

U]/2)z

+

lUx(Uz

+

U]/2)lx

Uxxxx

(43)

In the

following,

we restrict our

analysis

to the

boundary

conditions u

= 0 at z = 0 and I such

that -no dilation is

imposed by

the

boundary

conditions .~

We

already

established that a threshold value of C exists such that the

x-independent

solution of

(43)

bifurcates to a

sqlution depending

on x m a non tnvial fashion. Moreover thJs

equation

is the

Euler-Lagrange copdition

expressing that a functional G is

stationary Indeed, relaxing

the e'~~

dependence (but

still

looking

at the same

scale),

the

equation

for u may be

wntten

au SF

at ~

~P

8u

(12)

m which §

=

V(I

+ A~/A==

A~)

and

i~

=

A~(I

+

A~/A-= A~),

or

au 8G

I

8u

where G

= F +

l'dr

flu.

Thus it makes sense to look at the

optimal

solution with the lowest « energy » As G contains

a term which is linear m u m thJs energy and is

multiplied by

the

large

quantity

C,

one

expects

that this

optimal

solution has the

largest possible

order of

magnitude

m C.

We can use a dimensional argument to evaluate the order of

magnitude

of the different

terms m

(43)

More

§recisely

we look for solutions of the form

u«c«, z«cfl,

x«cY.

(44)

If we look first for extended solutions

along

z, the

scaling

of the reduced z variable as I should

correspond

to

fl

= 0. It is

possible

to

satisfy

the

scaling

of the four first terms m equation

(43)

with u ~c

C,

z ~c I and xx

C~'~ (a

=

I, p

=

0,

y

=

).

ThJs choice makes

negligible

the 2

higher

denvative in the

right

hand side of

(43)

which is of order

C~~.

It also

yields

the

parameterless

equation, deduced from

(43)

with the

scalings

given

by (44)

but with the

change

of notations u m

Cu,

f m z, x m

C~'~x

:

I

=

(uz

+

ul/2)z

+

lux(uz

+

u]/2)lx (45)

with the b.c. u

=

0 at

z = 0 and I The

scaling (44)

with the above choice of

exponents

indicates that the

preferred wavelength

of the

optimal

structure increases like

C~'~

at

large C's, although

the

amplitude

of the

perturbation

m u varies as C. This seems to be

incompatible

at first with the

general

assumptions of small

gradients

u made m the

calculations,

m

particular,

the

phase

fluctuations has to be small m some sense m order to

permit

to write the

equations

in the coordinates of the

unperturbed

system. However this can be done

consistently

even in the limit where C goes to

infinity

because there is a smallness

parameter

independent

on

C,

which is

again

the ratio

AIL

The tilt of the

equiphase

lines

remains

small,

as

required

if the dimensionless quantity u~

(resp

u~) is

small,

m the

large

C

limit,

this

gradient

scales as

(

CA

IL

)~'~

(resp

CA

IL ))

and thus can remain small even with a

large

C as

long

as

AIL

is smaller than C~

This

scaling

does not give much information on the detailed structure of the solution of

(45)

The

following arguments suggest

that it results from a cascade of instabilities down to scales where a different

scaling corresponding

to

boun"dary layers

takes over The cascade

results from the fact

that,

as V increases,

undulating

rolls become

again

unstable when

they

are

sufficiently

dilated. Thus

they

tend to

develop

an undulation withJn the undulation. ThJs process can

only stop

when a

sensitivity

to curvature is recovered In order to demonstrate this

possibility,

we show that any solution u of

(45)

is at least

locally

unstable. Since there is no

length

scale m

(45),

it is also

globally

unstable.

First,

we know that the solution

uo(z)

=

z(f z)/2

does not

represent

the

minimum of the

energy, since we have

already

shown its

instability.

Let again w be thJs fluctuation with the wavenumber q m the x direction. If

neutral,

this fluctuation has to be the solution of

w~~ +

q~

w

(z 1/2)/2

=

0 with w

=

0 and z

= 0 and

This

Airy equation

imposes

quantized

values of q~ and those values exist, as can be shown in the WKB limit for instance. Since the solution

uo(z)

is

neutrally

stable

against

some

(13)

perturbations,

a

weakly

nonlinear

analysis

would show that some small

amplitude pertur-

bation with a wavenumber close to the ones given

by

the

abovej eigenvalue problem yields

a

solution with a lower energy.

Let us come now to the smoothness of the solution of

equation (45).

Th1s

equatiin

is

the Euler-Lagrange

cond1tlon for the statlonanty of the functional :

£(u)= dr(-u+ (u~+uj/2)~), together

with the

boundary

conditions u=0 and

z = 0 and I.

Suppose

that one has found a smooth solution

U(x, z) making

thJs functional

stationary

and as

negative

as

possible

with our choice of

sign

for the definition of

£(u).

Consider now the second variation of

£(u)

around thJs solution. Let

w(x, y)

be the

corresponding

fluctuation of u near

U,

then thJs second variation has the form :

(w

=

ldr (w)

+ 2 w~ w~

U~

+ w

j(

U~ +

3/2 Uj)/2) (46)

This expression is

quite

remarkable m the sense that it is

homogeneous

as far as the denvation order of w is concerned. Tins

implies

that the

sign

of d£

(w)

is

completely

determined

by

the

one of the

quadratic

form m the variable w~ and w~ that appears in the

integrand

of

d£(w).

This

quadratic

form may get

positive

values

(and

the initial solution may become

unstable)

if the determinant

(U~

+

1/2 Uj

is

positive

somewhere in the

physical

domain.

Before going to the

physical meaning

of thJs last

condition,

let us show that thJs

happens

for

a smooth solution U. Let us consider the

following change

of

vanables, kindly suggested by

Haklm :

dz=dT, dx=dT.UJ2.

In terms of the new variable T, we can express the variation of U as

dU

=

Uz

dz +

U~

dx

=

dT(U~

+

Uj2)

The vanation of U between z

=

0,1

is given m the new running variable T as

lgradU.dT=o

since the

boundary

cond1tlons U

= 0 holds at both ends.

Thus,

either U is zero

everywhere,

or

it has a maximum m

the mte~val.

In such a case, the quantity

(U~

+

1/2 Uj

must be positive somewhere in the

interval

z

=

0,

On the

other,hand,

U cannot be zero

everywhere

on the line indexed

by

T

IS.

Near z

=

0

(or

z

=

I,

but with a

slight change

of sign and of

vanable),

the

Taylor

expansion of a solution of equation

(45)

should include a

quadratic

term

(- z~/2), and,

as the line under consideration merges with the z

=

0 line at

nght angle,

U cannot vanish

everywhere

on it.

The

physical

meaning of thJs result may be understood as follows : the determinant of the

quadratic

form is

precisely equal

to the local variation of the

wavelength expressed

m intrinsic coordinates as shown in the

appendix

Thus the

possibility

of

having locally

an unstable fluctuation is j manifestation that a

locally

dilated roll will tend to reduce this dilation

by

a local modulation in the transverse direction. Here we have the remarkable situation that thJs

process may be continued down to

arbitrary

small scales

This

unphysical

result

implies

that

equation (45)

cannot be

uniformly valid,

because the

onginal equation (43)

had

actually

a built-in small space

scale, represented by

the fourth denvative m

(43),

that has

precisely disappeared

m

(45)

after the

rescahngs

motivated

by

the

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