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HAL Id: jpa-00247897

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Submitted on 1 Jan 1993

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Linear growth of instabilities on a liquid metal under normal electric field

G. Néron de Surgy, J.-P. Chabrerie, O. Denoux, J.-E. Wesfreid

To cite this version:

G. Néron de Surgy, J.-P. Chabrerie, O. Denoux, J.-E. Wesfreid. Linear growth of instabilities on a

liquid metal under normal electric field. Journal de Physique II, EDP Sciences, 1993, 3 (8), pp.1201-

1225. �10.1051/jp2:1993192�. �jpa-00247897�

(2)

Classification Physics Abstracts

47.20 47.65 68. lo

Linear growth of instabilities

on a

liquid metal under normal electric field

G. N4ron de

Surgy(~)

,

J.-P.

Chabrerie(~)

,

O.

Denoux(~)

dud J.-E.

Wesfreid(~)

(~) Laboratoire de Gdifie Electrique de Paris

(LGEP)(*)

,

Plateau du Moulon, 91192 Gif sur

Yvette Cedex, France

(~) Laboratoire d'Hydrodynan~ique et M4canique Physique

(LHMP)

(**), Ecole S~lp6rieure de

Physique et Chin~ie Ind~lstrielles de Paris

(ESPCI),

lo rue Va~lq~lelin, 75231 Paris Cedex 05,

France

(Received

ii December1992, revised 27 April 1993, accepted 6

May1993)

Rdsum4. On salt q~l'~ln champ 41ectriq~le appliq~l6 normalement I la surface Ebre d'~ln fl~lide cond~lcte~lr a ~ln elfet d6stabifisant. En restant dons le cadre d'~lne th60rie lin6aire, no~ls

4t~ldions ici le d4veloppement des instabilit4s 41ectrocapillaires, dons le cas trbs g6n6ral off la viscosit6 d~lfluide et son 4paisse~lr sont q~lelconq~les. No~ls d4duisons di1f4rents comportements dons divers r6gimes et donnons des 6q~lations de dispersion analytiq~les dons le cas des couches 4paisses et minces, inertielles et visq~le~lses. No~ls pr4sentons alors ~ln diagramme des di1f4rentes

simplifications possibles et comme no~ls d4d~lisons ces simplifications directement de l'4q~lation g4n4rale il est plus facile de pr4ciser les limites de validit4 des hypothbses. No~ls montrons a~lssi les similarit4s et les di1f4rences avec le cas d'un liquide tombant d'un support solide plan

(instabilit6s

de

Rayleigh-Taylor)

en absence de champ 41ectrique ainsi qu'avec les instabilit4s dons les ferrofluides.

Abstract, It is well known that an electric field that is applied normally to the free surface of

a conducting fluid has a

destabilizing

effect. Here

we study the linear

growth

of electro-capillary

instabiEties in the very

generil

case where the viscosity of the fluid and its thickness are of any value. We derive the asymptotic behavio~lr in various regimes and give analytical dispersion equations in the case of thin or thick, inviscid or viscous films and compare with previous results.

Then we present a diagram of the corresponding simplifications of the dispersion relation and

as we derive them directly from the general equation, we are able to derive their conditions of

validity explicitly. We also show the simflarities and the differences with the case of a fiq~lid falling from a solid flat plane

(Rayleigh-Taylor instabilities)

without electric field and with

ferrofl~lid instabilities.

(* URA CNRS N°127

(** URA CNRS N°857

(3)

1. Introduction.

We shall consider

(see Fig. I)

a

conducting

and

incompre8sible

film of

liquid metal,

mercury for

instance, laying

on a metallic flat electrode. The undisturbed free surface of the

liquid

is at z = 0 and the electrode at

z = -a. Another electrode is

disposed

at z = b, with vacuum for 0 < z < b and a

potent1al

V is

applied

between the electrodes. The geometry will be

supposed

to be infinite for both ~ and g.

The linear

stability

of such a film under a normal electric field Eo "

V/b

has

already

been studied

(Tonks

[1], Frenkel [2],

Taylor

[3], Melcher

[4-5],

Nekrovskii

[6]).

The

study

of the thick

(a

and b

infinite)

inviscid case with normal modes of

perturbation

of the type

((r)

=

((~,y)

=

Aexp(st ik.r)

(where

s is the

growth

rate of

perturbation

and

k,

the modulus of

k,

is the horizontal wavenum-

ber)

is easy to

develop

and well

known, leading

to the

following dispersion

relation:

ps~

=

-Sk~

+

eoE(k~ pgk (1)

where

p is the

density

of the

liquid,

S the surface tension of the

liquid-vacuum interface,

go the

permittivity

of vacuum and g the

gravitational

field.

It can be seen with this relation that a destabilization of the

liquid

surface

(Re(s)

>

0)

occurs

only

above a critical field

Ec:

Ec

= ~

ll

eo associated with a

critica1wavelength lc

lc

= 2gr

~ Pg

Let us consider a twc-dimensional

(~, z) problem,

where

((~)

=

Aexp(st ik~).

In order to introduce the thickness effects we shall first consider a horizontal

length

scale l~ =

1/2gr (with

I =

wavelength

=

2gr/k),

and a

vertica1length

scale noted lz. The value of lz will be taken as the lowest value between the film thickness a and

1/2gr.

For

2gra/1

» 1 the film will be called thick

(the

vertical scale is then the

wavelength),

for

2gra/1

< 1 the film will be called thin

(the

vertical scale is then the fluid

depth).

VaCUUIII Z

z=o ,fij ill /I.. ii

~

._.illi@1:(~' g v

: a

~

~

x

Fig,I.

Schematic view of the experimental device.

(4)

thin thick inertial inertial

i

thin thick

viscous viscous

2na/~

Fig.2.

Diagram of the different kinds of behaviours.

For the

study

of the effects of

viscosity,

we shall then consider a

Reynolds

number : Re

=

inertia forces

/

viscous forces. If Re » I we may

neglect viscosity

and call the film inertial or

inviscid,

dud if Re < I we may

neglect

inertia and call the film viscous.

We shall denote

by

q the

dynamic viscosity

of the

liquid

and v

=

q/p

the kinematic

viscosity

of the

liquid.

The

Reynolds

number is:

~~

~~~ l'~

q

(I/lz)~~~~l/lz)~j

U

Therefore we have in the extreme cases:

-for a thick

film,

where the vertical scale is

1/2gr:

j2 ~j

~~

2v(2gr)2

~ 2vk2 -for a thin

film,

where the vertical scale is a:

Re=

~a~jsj

v

This

Reynolds

number compares the viscous

penetration length (a

fundamental

length

in

hydrodynamics)

lvp

=

/@

with the film thickness and with the

wavelength.

It can be

written:

~~~~~ ~2

~~ ~

[(21r/1)~ $(l/lz)~j

On the

diagram

of

figure

2 we have noted the different kinds of

(asymptotic)

behaviour.

We can see four different

regions.

The inviscid

(thick

and

thin) regions

can be related to the inviscid

dispersion

relation. In this article we shall

give analytical

results for the two other

regions,

and also for the case of

high viscosity

and moderate thickness. We extend the asymptotic

analyses

of

Rayleigh-Taylor instability

of

Hynes

[7] and Limat [8] to the electrc-

capillary instability.

(5)

The

general

case, which takes into account the

viscosity

v of the

liquid metal,

its thickness

a and the vacuum thickness b between the free flat surface and the upper electrode is not

always

well treated.

Indeed,

some papers concerned with this

problem ([6,

9,

10])

contain a

faulty dispersion

relation.

Nevertheless,

a correct

expression

for the inviscid case and for the thick-film case

(the

thickness a - cc has

already

been

proposed.

For this last case, instead of

punctua1numerical

treatments of the thick

dispersion

relation [9], we propose to show the

asymptotic

behaviour of very viscous

liquids (corresponding

to the thick viscous case in

Fig.

2)

for which the dominant

wavelength

will be shown to be

independent

of the

applied

field. We shall use a method similar to that used in the

study

of

gravity

waves

by

Leblond and Mainardi

ill].

In order to compare the

respective properties

of different metals or

alloys,

we shall use

dimensionless values: we shall see that the results

depend

on a

capillary length

lc and a viscous

length

iv

(characteristic

of the

fluid),

on an electric

length

l~

(characteristic

of the fluid and of the

applied potent1al V)

and on the

geometrical lengths (thickness

a of the

liquid film,

distance b between the fluid and the upper

electrode).

We shall check that the

stability

domain

depends only

on the

capillary

and the electric

length

values

(and

is therefore

independent

of

viscosity

and

geometry),

while

dynamics (I.e.

the linear

selection of the most unstable

wavelength)

involves all the

lengths.

We shall also

point

out the

analogy

with the case of a fluid film in a

gravitationally

unstable situation

(Rayleigh-Taylor instability)

studied in the works of Chandrasekhar [12],

Hynes

[7]

and Limat [8].

2. The characteristic scales of the

problem.

Having

identified different

regimes (thin

and thick

layers,

inertial and

viscous),

we find it useful to compare the thickness a with different

typical

distances.

The

liquid

meta1is submitted to

capillary,

viscous and electric forces. For each force we can build a characteristic

length. By comparing

the effects of surface tension

(Sk~)

to those of

gravity (pgk)

in

(I)

we can construct a

capillary length:

i~ =

si/2p-1/2g-1/2

This

length

is

always

of the order of10~~cm for the usual

liquids

in the normal

gravitational

field.

In a similar way, we can compare the effects of the electric field

(eoE]k~)

to those of

gravity

to build an electric

length:

le =

(eo/2)E(p~~g~~

For the critica1field

(Eo

"

Ec)

this

length

is

equal

to the

capillary length

and is greater than

lc for

larger

fields.

Near the critical field the

wavelength

is of the order of lc in the inviscid case

(in

fact

equal

to

2grlc).

It will be shown that it remains true at finite

viscosity.

For greater electric fields the value of the

linearly

most unstable

wavelength

includes a combination of lc and l~, it will be

shown to be

usually

of the order of

I(/le

for le »

lc.

In fact we have

le/lc

=

El /E(

which is the control parameter of our

problem,

and that will be noted 4l. Then we shall see that

lc/4l

scales the

wavelength

and that

increasing

the field will shorten the

wavelength (but

not in the thick viscous

case).

We can also build a viscous

length.

For this we consider a dimensionless number built

(as

a

Stokes number for

particles) by comparing

a time of stabilization due to

viscosity (Tsta)

with

a time of destabilization due to

gravity

for a free

falling drop

(Tdesta)1

(6)

Table I.

-Physical

vdues for different

liquids.

(g/cm~)

S

(dyn/cm)

v

(cm~ Is) (cm)

iv

(cm)

d

Li 0.5 400 lA x 0.88 1.2 x 5.5 x

Ga 6.1 718 3.5 x

10~~

0.34 2.3 x

10~~

5A

x

10~~

Sn 7.0 612 2.8 x

10~~

0.30 2.0

x

10~~

x

10~~

Al 2.4 914 3.I x

10~~

0.63 2.I x

10~~

x

10T~

Au 17.3 l140 2.7 x

10~~

0.26 2.0 x

10~~

x

10~~

Hg

13.5 470 1-1 x

10~~

0.17 1.0

x

10~~

x

10~~

Silicon oil 1.0 21 10 0.15 0.56 5.7

Water 1.0 70

10~~

0.27

10~~

x

10~~

fluid 1.0 10 0.5 0.1 6.3 x

10~~

x

10~~

Tsta " l~

IV

Tdesta "

(I/g)~/~

~~

~a li~~/~ ~/~~~~/~

~~~

where a viscous

length

[13] can be defined:

iv "

V~/~g~~/~

This

length

is

only

determined

by

the

physical properties

of the fluid

(contrary

to the above introduced viscous penetration

length).

It is of the order of 10~~cm for

a

liquid

metal like mercury at room temperature.

We shall write St

=

d~~

when

= lc:

d

=

(iv/ic)~/~

which will

play

an

important

role in our

problem.

The other

lengths

in the

problem

are the

geometrical lengths

a and b, and the

wavelength

1

(= 2gr/k).

We can use the different

length

scales to build dimensionless

values;

we shall use the

capillary

scale as the reference scale as it will be seen that this scale is the most

important

in

defining

the

wavelength.

We therefore expect

a/lc

and d to be cruc1al parameters. In table I we

give

a list of values of

density,

surface tension and kinematic

viscosity,

the

corresponding capillary

and viscous

lengths

and the

corresponding

value of the parameter d

(we

took the same elements

as [9] and added silicon oil to compare with

Rayleigh-Taylor instability

and

magnetic

fluid to compare with the similar situation of

magnetic

fluid under

magnetic field).

We can

similarly

introduce characteristic times. The more

usefil

will be the

capillary time, typical

of a free

falling drop,

and defined before as Tdesta

tc =

(lc/g)~/~

=

S~/~p~~/~g~~/~

(7)

The other time in the

problem

is the

growth

time or inverse of the

growth

rate of

perturbation:

~

j-1

3. General case.

We shall now solve the more

general

case of a viscous

layer,

and we shall leave open the

possibility

to be in the case of

Rayleigh-Taylor instability (we

then suppose the

density

of the upper fluid to be greater than the

density

of the

underlying

fluid: oil

falling

in air for

example).

With g directed from the fluid to the vacuum, g

=

(0,

0,

g),

we are in the case of a fluid located under a solid flat

plate,

which is the

Rayleigh-Taylor

case. We shall let the

possibility

to choose this in the

equations by using

a constant x

equal

to I if g =

(0,

0,

-g)

and to -I if g =

(0,

0,

g).

In the

following

we shall denote

by ((~, y)

the vertical

displacement

of the

interface, v(~,

y,

z)

the

velocity

of the

fluid, e(~,

y,

z)

the electric field in vacuum and n, the unit vector normal to the

interface,

=

(8~(, 8y(, -1)

ci

(8~(, dy(, -I)

at first order

/1

+

(8~()~

+

(8y()~

The system is

represented by

the

following equations (for

an

incompressible fluid,

with q and S

constants):

div

v = 0

)for

z <

((~,y) (in the1iquid metal)

p[$v

+

(v grad)v]

=

-grad

p +

nAv

+ pg

curl e = 0

for z >

((~,y) (in

the

vacuum)

div e

= o

which mean bulk conservation, the Navier-Stokes

equation

dud Maxwell equations

(without magnetic field).

The

boundary

conditions

(where [Xi

= value of X above the interface value of X under the

interface)

are:

1(

= uz

u~8~( uy8y(

at z =

( (free

surface

condition)

-~j]n;

+

[T,k

+

~(~]nk (S/R)n,

at z =

( (stress

balance at the

interface)

n x e = 0 at z =

( (liquid

metal

condition)

v = 0 at z = -a

(velocity equal

to zero at the

electrode)

e~ = ey = 0 at z = b

(electric

field normal to the

electrode)

where we defined the stress tensor:

the viscous rate-of-strain tensor:

~ik " 11

(~~k~t

+

~~k~k)

and R~~. curvature of the interface

(positive

if directed towards the

fluid) R~

=

()

+

))

m

iai~

+

aj~)

We

shall,

from now on, use dimensionless values with

capillary

scales as references:

lc for

length,

tc for the time, the

capillary Laplace

pressure pc =

S/lc

=

/@

for pressure,

Eo "

V/b

for electric field.

In this case, we note:

(8)

~'

=

~/lc, y'

=

y/lc,

z' =

z/lc, I'

"

(/lc,

a'

=

a/lc,

b' =

b/lc,

t'

#

t/tc>

P'

=

(P+ xPgz)/Pc,

e'

=

e/Eo

We recall that 4l

=

(1/2)eoE](pgs)~~/~

=

E( /E(

and d

=

(lv /lc)~/~

as was

previously defined,

with x

= I if g is directed like

(o, 0, -1),

which is our

problem,

and x

= -I if g is directed like

(0, 0, 1),

which

corresponds

to a film in a

gravitationally

unstable

position (Rayleigh-Taylor).

To make the different

expressions

easier to read we shall

drop

the

primes:

We obtain

j~~ v~ grad)v

=

-grad

P + dAV

l~~~

~ ~ ~~~~ ~~

curl e

= 0

for z >

((~,

Y)

div e

= 0

with the

following boundary conditions,

where for the curvature we have restricted calcula- tion to the first order term:

81(

= Uz

U~8~( Uy8y(

at z =

(

-(-P

+

x(

81~

( 8(~ (

+

)8~(

+

~l(el e( el)8~(

+

2e~ey8y( 2e~ezl+

-2d(8~u~ )8~( d(8~uy

+

8yu~)8y(

+

d(8~uz

+

8zu~)

= 0 at z =

( -(-p

+

x( 8]~ ( 8(2 (

+

)8y(

+

4l[2e~ey8~(

+

(-e]

+

e( e])8y( 2eyez]+

-2d(8yuy)8y( d(8~uy

+

8yu~ )8~(

+

d(8~uz

+

8zu~

= 0 at z =

(

-P +

x( 8]2( 8(2(

+

=

=

4l(-2e~ez8~( 2eyez8y(

+

(-e] e(

+

e()]+

-2d8zuz

+

d(8~uz

+

8zu~)8~(

+

d(8yuz

+

8zuy)8y(

= 0 at z =

(

e~ +

d~(

= 0 at z =

(

ey

+dy(

= 0 at z =

(

uz = up = uz = 0 at z = -a

e~ = ey = 0 at z = b

P(o)

" -4l

At zeroth order we have: ejo) "

(0, 0,1)

~(o) " °

At first order the

problem

is solved in

Appendix

A and we obtain a system of six equations for six unknown constants.

This leads to annulate the

following

determinant:

sinh(ka)

0

sinh(qa)

0 0 -s

2k~

sinh(ka)

0

(k~

+ q~)

sinh(qa)

0 0 0

((

+

2dk) cosh(ka) f

+ 2dk

2dq cosh(qa) 2dq

-214l

cosh(kb)

x + k~

0 0 0 0

sinh(kb)

ik

k k

cosh(ka)

q q

cosh(qa)

0 0

0

sinh(ka)

0

sinh(qa)

0 0

(9)

with q~ = k~ + s

Id.

The formal wavenumber q relates the horizontal wavenumber k of the

perturbation

and the vertical wavenumber

/fi, giving

an idea of the penetration of the viscous

dissipation

inside the

layer (with

dimensions it reads q~ = k~ +s

Iv).

This determinant has

already

been obtained in reference [9] with a

slight typographical

error. It leads to the

following

transcendental

equation as an

implicit dispersion

relation between the dimensionless

perturbation growth

rate s and the dimensionless wavenumber

k,

for different values of the external

applied

field Eo

written in terms of the ratio 4l:

4qk~[q

k

coth(ka) coth(qa)] (k~

+

q~)~[q coth(ka) coth(qa) k]+

~~~

~~ ~ ~

= [k~

24lk~ coth(kb)

+

Xk][q coth(qa)

k

coth(ka)] (2) inh(~a)~inh~qa)

d~

The parameter x is I in a

gravitational

stable

layer

and -I in a

gravitational

unstable

layer.

For 4l

= 0

(no applied

electric

field)

and X

" -I we retrieve the results of Chandrasekhar [12]

for the

Rayleigh-Taylor instability

4.

Asymptotic

behaviour of the

dispersion

relation.

We recall that we use dimensionless values

(relatively

to

capillary

values and without

primes)

unless otherwise stated.

We can first see that if

(k, q)

is a solution of

equation (2)

then

(k, q)

is also

solution,

q

being

the

conjugate

of q. We shall limit our

study

to solutions where

Im(q)

>

0,

with k real as is usual in the

temporal theory

of linear

stability.

We can also see that s

= 0

(which

means q

=

k)

is

always

solution of

equation (2).

Apart

from this trivia1solution we look for the unstable

regime,

therefore

Real(s)

> 0, which

implies Real(q~)

> k~ and

Real(q)

> k. We can

numerically

check that the sc-called

'principle

of

exchange

of stabilities'

(Real(s)

= 0

implies Im(s)

=

0) applies

in our

problem (Appendix B).

As s

= 0 is

already solution,

we shall first obtain the limit of equation

(2)

when s - 0.

In this case Sk

= q k

+~

)

can be factorised in

equation (2)

and after

simplification by

6k 2 k

we obtain a

dispersion

relation of the type: Sk

+~

P(k),

valid near s

= 0, and for which s = 0

(which

is then

equivalent

to Sk

=

0)

is not a triv1al solution.

In fact we then obtain the

dispersion

relation of the very viscous case

(as

qa -

ka,

obtained if Sk - 0 for a

given,

which allows the

simplified equation (14)

of the viscous case, can be

obtained

by doing

either s - 0 or d -

cc). Performing

s = 0 in this relation

gives

the

equation

of the curve of

marginal stability:

P(k)

= k~ 24l

coth(kb)k

+ x

= 0

which is therefore

independent

of the

viscosity

and of the

depth

a of the

layer.

In

Appendix

B we also show that if

P(k)

< 0

(unstable region),

then

Im(s)

= 0 and there exists a solution with

Real(s)

>

0,

while if

P(k)

> 0

(stable region),

then

Real(s)

< 0.

In the

following

we try to find the

asymptotic

behaviour of the

growth

rate s in the different

regimes,

thick and

thin,

viscous and

inviscid,

in the

spirit

of the studies of

Hynes

and Limat.

For the different

asymptotic dispersion

relations s =

s(k),

the condition for

instability

is always that k should

belong

to the linear allowed band where

P(k)

< 0.

(10)

Outside this

band,

we are not

always

allowed to use the

simplified dispersion

relations: for

example,

in the well-known inuiscid case the

dispersion

relation of type

(I)

s~

=

-kP(k)

cannot

strictly

be

applied

for

P(k)

> 0: s~ would be

negative, giving

a

purely imaginary

growth

rate s = iw

but,

for any finite

viscosity,

the

imaginary

part of the

dispersion

relation would

give Im(s)

= 0,

introducing

a contradiction

(in

fact there is a real part of s that will

damp

the

wave).

We have nevertheless

plotted

curves for 4l < 1 where

P(k)

is never

negative

and for the

regions

where

P(k)

< 0 for 4l > 1 in order to show how the curves evolve with the field.

One of the interests in

analyzing

the

asymptotic regimes

is to derive

explicit

relations for the fastest

growth

rate s*

= sm~x obtained for

ds/dk

= 0. Indeed if the external field reaches

a

supercritical

value

Eo

>

Ec sufficiently quickly

(T =

Eli

< I

/s*)

it is

possible

to

achieve,

t

at least

transiently,

a wavenumber selection mechanism of linear type

following

the s* = s*

(E)

curve. If the field is

applied

too

slowly

the transition will occur before the "desired" field Eo

will be reached

(for

a very

slowly applied

field the transition occurs near the critical

field)

and

once the instabilities have

begun

to grow, a full non-linear treatment would be needed in order to

predict

how the structures evolve.

We know

experimentally (see [14])

that a

quicker

installation of the field

(if

the field is greater than the critical

field) produces

more

peaks

for mercury under a normal electric field.

In numerous related

problems

we can encounter similar

dispersion

equations: for instance in

magnetic liquids (see [15]), formally equivalent

when the

magnetic permeability

p - cc, and in the case of

ripplons

at the

charged

interface of

phase-separated

~He -~ He mixtures excited

by

an electric field

(see

Leiderer

[16])

the

dispersion

equation is

analog

to the inviscid case.

Savignac

and Leiderer [17] studied the case of an interface

crystalline-superfluid He; they

have

experimentally

shown that the

instability, again

similar to ours, grows with

ds/dk

= 0 and

gives

many more

peaks

for

higher

fields than for onset.

This situation is

extremely important

for

technological applications

in order to obtain

Liquid

Metal Ion Sources

(LMIS)

with a

typica1wavelength

smaller than lc.

4.I. THICK FILM. We first

study

the case of a thick film of

liquid

metal. The thick film

hypothesis implies

that ka » I and Real

(qa)

» I, so that

coth(ka)

ci I and

coth(qa)

ci I, the

dispersion

relation

(2)

leads to:

4qk~ (k~

+

q~)~

=

j[k~ 24lk~ coth(kb)

+

xk] (3)

It is

possible

to solve q =

q(k)

and there are four roots. It is also easy in this case to

verify analytically

the

principle

of

exchange

stabilities. In order to solve the

equation

it is more

convenient to write it as:

16

(k~

+

j)

k~

=

(2k~

+

j)~ j [-k~

+

24lk~ coth(kb) xk] ~

(4)

It is now

possible

to solve s

=

s(k).

If q is solution of

(3)

then

(4) just

adds its

opposite

since solution but since we are

only

interested in s

(which

varies like q~) it is of no

importance.

Equation (4)

has four solutions for s, not all of which

correspond

to

growing perturbations

(with Real(s)

>

0).

We shall

study simplifications

of

(4), corresponding

to the different thick film

regimes.

(11)

4.I.I. Thick inertial

(inviscid)

fiIni. In the case of a

vanishing viscosity,

Re » I (j s

/(2dk~)

» for a thick

layer), equation (4)

can be

simplified, leading

to the well-known

case of an inviscid thick

liquid

film

(also

valid if d

= 0

exactly)

s(~_; =

-k~

+

24lk~ coth(kb) xk (5)

Instabilities exist if the

growth

rate s is real and

positive.

When the distance b between the fluid and the upper electrode is

large compared

with the

wavelength

so that

coth(kb)

m I this condition is fulfilled without onset for x = -I

(Rayleigh-Taylor instability)

and for 4l > 1 when x

= I. The allowed wavenumber k

belongs

to the linear band

C(4l)

defined

by:

4l-

x<k<4l+

x

The maximum

growth

rate

(ds/dk

=

0)

is

given by

the relation:

obtained for the wavenumber

~* 24~ + 44~~ 3X

tk.I ~

The

validity

conditions for this

regime

become

l~~a

» I thick

hypothesis

d~(2~~~

~ ~~~~~~~~ ~~~~~~~~~~

Near onset (4l -

1)

s - 0 and k - kc = I, which is

only possible

for the limit of inviscid

film iv - o

(d

-

0),

so for non-zero d we cannot

apply

the inviscid

hypothesis

in the limit

4l - 1. In other terms the viscous

penetration length

lvp - cc near onset and the viscous

dissipation

then exists on all the finite

layers.

In

figure

3a we

plot s~(k)

(X

" I, electric

case), keeping

in mind that the above-mentioned

conditions of

validity,

even if

they

hold for

k*,

are not

necessarily

verified far from the maximum.

4.1.2. Thick non-inertial film. We shall now

study

the corrections introduced

by

a finite

viscosity.

For this case we can write

equation (4)

in the

following

form:

16

(k~

+

II

k~

=

(2k~

+

II

~

(~l" j

~

(6)

Let US ~~~~°~~~~'

~

2dk~

1

~d

j

~

8tk.I i~~i ~~~"

where Re; is a

Reynolds

for a fluid where the

dispersion

relation is

supposed

to be the same as in the inviscid case and

(

is the ratio between the effective viscous

growth

rate and the

growth

rate for the fluid

supposed

to be inviscid and is

always

smaller than I

(as

will be seen

later).

We have therefore Re

=

(Re;

=

(IS:

this

Reynolds

should be much greater than I to allow the inertia1film

approximation.

If the

viscosity

does not affect much the

dispersion

relation

we have

f

ci I and Re ci Re;.

We obtain the

following equivalent equation:

(12)

s2 /fl

Thick s I Thick

~I~<I

~I~=1 4~<1

~l~=0 '°' j~

o-o o-S I-o I-S 2.o 2.5 3.o o-o o-S I-o I-S 2.o 2.5 3.o

a b

~

fi T

o.2

(~=o 5)

S

(a=Q,5

o-o ~ ,~

~~~

~~~~~~

.o.2 4$=1

~

~ ~

~J~<i ~l~<I

~l~=0 ~l~=0

o-o o-S I-o I-S 2-o 2-5 3.o o-o o-S I-o I-S 2.o 2.5 3.o

d

lll ~~

~J~>1

%

~

~

«>i

fi

-o,os

'(

m=i

d=20)

_~ ~~ ~D<1 4~<1_

~ ~~

4~=o

k

°"°

k

o-o o-S I-o I-S 2-o 2-S 3.o o-o o-S I-o 1-5 2.o 2-S 3-o

e f

Fig.3.

The different dispersion relations:

s~(k)

for thick inviscid, non-thick inviscid and thin in- viscid

s(k)

for thick-viscous, non-thin viscous and thin-viscous.

@~(@ +

2f)

= 1(@ +

f)~ ii

~

(7)

which is a well known

quartic equation

obtained in the

study

of

gravity

waves

[18, 11].

The difference between

gravity

waves and our

problem

is that we consider solutions where s is

real,

while for

gravity

waves s is

purely imaginary (in

this case solutions are

sought

for a

purely

(13)

(

~~

i

~

o o

', 2 4 6 8 10

-1

-2

-3

(

m -0.46 6

-4

Fig.4.

The real solutions of the q~lartic equation

(7).

imaginary 9).

Since we are interested

only

in the unstable

regime,

we

plot (

versus in

figure

4

only

for

>

0, showing

two real branches

(for

which

(

<

I).

The condition

ds/dk

= 0

(maximum growth perturbation) leads, together

with

(7)

to the condition:

l~

%~~

@~(2@ +

3()

= [(@ +

()~ l] 2(9

+

()9

8~

(8)

sik.;

4.1.2.I Thick

quasi-inviscid

film. If the

liquid

has a very low

viscosity,

iv < lc

(d

<

I),

the

dispersion

relation is not

strongly

modified and this is the reason

why

we call the

regime quasi

inviscid. As the value of d is small for

liquid

metals this case is

interesting

from a

practical point

of view.

For this condition 9 < 1, which means that we are in the case where the thick inviscid

hypothesis

can be

applied,

equation

(7)

leads to

(=1-9+O(9~)

when9-0

(9)

or:

sik.qi "

[-k~

+

24lk~ coth(kb) xk]

~~~

2dk~ (lo)

This

corresponds

to the

region

9 < 1 in

figure

4 where the two branches

collapse.

The term 9 in

equation (9)

describes the viscous attenuation of

growth

in the quasi-inviscid

regime,

it

shows how the dispersion equation is affected

by

a small viscosity. It should nevertheless be

(14)

noted that this relation is not valid near s

=

0,

and cannot be

used,

in

particular,

to determine the linear band of

stability.

This correction

brings slight changes

to the

dispersion

relation which also

slightly

affect the value of

k(~,;.

In the case of

gravity

waves the viscous attenuation is real and does not

change

the

pulsation

of the wave

(s

is

purely imaginary

in the inviscid

case):

the waves are attenuated but the

pulsation

is the inviscid one. Here it affects the

growth

rate because s is a rea1number.

4.1.2.2 Thick very viscous film. If the

viscosity

is very

large,

we expect a different behaviour.

If Re < I

(the

film is

viscous)

we should have

f16

< 1 which

implies (see Fig. 4)

9 » 1,

so

Re;

< I.

Reciprocally,

for

Re;

<

I,

as

f

< I, we have Re

=

f

Re; < I so that Re < I is

equivalent

to Re; < I. In this viscous case

equation (7)

leads to:

~3

~ ~

~4

~

~~'

~~~~ ~

~ ~~~~

the other branch of solution

being f

= -0.46 9 when 9 - cc,

corresponding

to a stable

regime.

We can write

equation (II)

to first order in the form

(which

is valid

only

for x

=

I,

as it

tends to cc for k - 0 if x

=

-1):

sik.~ "

i-k

+ 24l

coth(kb) ~j (12)

We can note that sik.v

"

Re;sik.;

and as

Re;

< I, the value of s is much smaller than in the

inviscid case.

In

figure

3b we

plot s(k)

for x

= I.

When the distance between the fluid and the upper electrode is

large compared

with the

wavelength (coth(kb)

m

I), instability

exists if 4l > 1 for x

= I. Allowed wavenumbers k

belong

to the linear band

C(4l).

The maximum

growth

rate

(ds/dk

=

0)

is

given by

the relation:

S~k,v "

(~ l)

obtained for the critical wavenumber

~tk.v

" ~c " 1

The existence of this

regime

is

governed by

the

following

conditions:

la ~

» I thick

hypothesis

(4l

1)

< viscous

hypothesis

2d

The second condition holds for fields near the critical one (4l almost

equal

to

I),

but d values

are

usually

too small for it to be valid in strong fields.

Let us stress an

important point:

for fields not far above the critical field (4l m

I)

the

unstable

region

is around k

= I, as the

instability

domain is the same for all kinds of

behaviour, corresponding

to k in the linear band

C(4l).

Then we cannot expect to find a dominant mode for which the

wavelength

will be of the

order of the thickness a or the viscous

length

iv, at least near the critical field. For

higher

fields we see here that in the viscous

infinitely

thick case the

capillary length

is still the

typical

(15)

scale.

Moreover,

as d is

usually

very small for

liquid

metals

(10~~),

this case

only applies

in

practice

very close to the threshold field.

In the

Rayleigh-Taylor

case the situation is

completely

different:

for x

= -I and 4l

= 0 there is no

dispersion

relation

giving

us the fastest

growth

rate: the

corresponding

maximum of s

(we

should moreover go further in the

k-expansion

as k

= 0 is the

maximum of

(12))

does not

satisfy

the

hypothesis

9 » 1, which leads to a different behaviour.

Let us assume that d » I

(viscous length

»

capillary length)

for k < I

(wavelength

»

capillary length),

sik.;

"

k~/~,

therefore:

(a similar simple relation cannotbe btained

in

the

203(20

+

3t)

=

j(o

+

t)2

11

j4(o

+

t)o

11

(13)

Relations

(7)

and

(13) give:

Sri 0.66

so that

k ci

0.49d~~/~

or, in dimensional form k ci ~'~~

iv

s ci

0.46d~/~

or, in dimensional form s ci 0.46 ~ iv

as obtained in [12]. This is the

typica1situation

when surface tension can be

neglected

in the interface of miscible

layers,

as occurs in many

geophysical applications.

One checks that k < I for d » I. The thick

hypothesis

reads

0.49a/lv

» I so that the thickness effects are more

important

than those of

viscosity.

Here we see that we are in a case where the

wavelength

is of the order of the viscous

length,

an

important

difference with the electric case. We can also note that Re < I but we have not

exactly

Re < 1.

4.2. VERY vIscous FILM. If the

depth

a has a finite

value,

it is still

possible

to

simplify

the

problem

when the influence of

viscosity

is

large enough.

If the condition a~ s

Id

< I is

satisfied,

I-e- if the viscous

penetration length

lvp

=

@

is

larger

than the film thickness

a, them the bottom friction can reach the interface and a

Taylor

expansion in powers of

(qa ka)

leads to:

1 ~ ~~ ~ ~~

xj sinh(ka)cosh(ka)-ka

~~'~ ~

2d ~ ~°~ k

cosh~(ka)

+

(ka)~

~~

If k satisfies ka < I, a~ s

Id

< I is

equivalent

to Re < I.

When ka » I,

equation (14)

reduces to

equation (12),

which can be used for x = I. That is, the very viscous thick case is

equivalent

to the

infinitely deep

viscous one. As we have seen that

Rayleigh-Taylor

instabilities exhibit a different behaviour in the

infinitely deep

viscous case, we expect a difference with the electric case for

large

film thicknesses in the

very-viscous

regime.

(16)

4.2.1. Thin viscous fiIni In the case of very thin films

(ka

<

1)

the viscous

dispersion

relation

simplifies

and leads to:

sin_v =

[-k~

+

24lk~ coth(kb) xk~] (15)

which can be

directely

obtained from lubrication

theory.

Indeed this is the case when the

dissipation

exists in all the

layer depth.

The lubrication

approximation

of

creeping

flow

implies

that the deformation of the interface induces a

tangent1al gradient

of pressure, with a half- Poiseuille flow for the

boundary

conditions of our

problem.

One

important

feature of this limit is the cubic

dependence

of the

growth

rate on thickness. This result is very useful in the

problem

of

charged

thin membranes

(see

also [19] where thickness a is very small and van der Waals forces need to be included. We call this the very thin

layer case).

When the distance between the fluid and the upper electrode is

large compared

to the

wavelength (coth(kb)

m

I)

this condition is fulfilled without onset for x

= -1

(Rayleigh-Taylor instability)

and if 4l > 1 for X

" I. The allowed wavenumber k

belongs

as usual to the linear

band

C(4l).

The maximum

growth

rate

(ds/dk

=

0)

is

given by

the relation:

s(~,v

=

$

(34l

+

8x)~ 8x 4l)

obtained for the wavenumber

~~ 34~ +

-

~"'~ 4

The

validity

conditions become

l~~~

< I thin

hypothesis

d~ (34l

+

@)~ (h

4l)

< 1 viscous

hypothesis

In the case of

liquid metals,

since the value of d is

small,

the value of a should be very small for the second condition to hold if we are not near onset. We

plot s(k)

in

figure

3f for the

electric case.

4.2.2.

Very

viscous "non thin" film.

Figure

3d shows the

plot

of

s(k) (for coth(kb)

=

I,

x = I: electric

case)

in a case where the film is neither thick nor thin. We shall now see the difference with the

gravitationally

unstable situation.

Let us

study

the

Rayleigh-Taylor

behaviour

(x

= -I and 4l

=

0).

If we suppose that k < I

(let

us

point again

that this

hypothesis

is not

justified

in the electric case, since the unstable domain is around k

=

I)

we can write

equation (14)

as

1

sinh(ka) cosh(ka)

ka

s =

~

~

(16)

dk cosh

(ka)

+

(ka)~

which has a maximum for

k* m

2.121a

s* m

0.16/d

where the conditions of

validity

are now a » 2.12 and

0.16a~

<

d~,

so that

viscosity

effects

are more

important

than those of thickness.

Here we find a case where the

wavelength

is of the order of the thickness a, so that in the

Rayleigh-Taylor

case we can have a

wavelength

of the order of

lc, iv,

or a

depending

on

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