Modélisation of fluid-fluid interfaces with material properties

Modélisation of fluid-fluid interfaces with material properties by. R. GA TIGNOL and P. SEPPECHER. Laboratoire de Mécanique Théorique, Associé au ...
1023KB taille 13 téléchargements 186 vues
Journal de Mécanique Théorique et Appliquée, Journal of Theoretical and Applied Mechanics, Numéro spécial, 1986, p. 225 à 247

Modélisation of fluid-fluid interfaces with material properties by

R. GATIGNOL and P. SEPPECHER Laboratoire de Mécanique Théorique, Associé au C.N.R.S.-U.A. n° 229, Université P.-et-M.-Curie, 4, place Jussieu, 75252 Paris Cedex 05 ABSTRACT The interfaces are seen as thin three-dimensional layers. The fluid inside these layers is a mixture the internal energy of which depends on the density gradient of each constituent. The internal strengths are described by a second gradient theory. The corresponding equation set is then integrated through the layer. So we obtain the evolution equations of the interfacial physical quantities in which there enter the parameters of the fluids on both sides of the interface. Then by an asymptotic proccess the interfacial layer may be considered as a carrier surface of material quantities. As a special case the balance laws are derived for an interface without mass but carrying a surfactant. At last using the linear thermodynamic of the irreversible proccesses we give the interfacial transport coefficients.

RESUME

Les interfaces sont assimiìées à des couches tridimensionneUes de faibìe épaisseur. Le fìuide contenu dans ces couches est un mé Lanqe dont l: 'énergie interne dépend des gradients des densités de chaque constituant. Les efforts intérieurs y sont décrits par une théorie du second gradient. Le système d'équations décrivant ì'évoìution du miìieu est intégré sur ì'épaisseur de ìa couche. On obtient ainsi des équations ìiant ì'évoìution des paramètres interfaciaux aux paramètres décrivant Lee deux fìuides de part et d'autre de l:' interface. Par un processus asymptotique ì'interface peut al.one être considérée COmme une surface porteuse de propriétés matérieììes. Les ìois de conservation sont en particuìier, expìicitées dans ìe cas d'une interface sans masse transportant un surfactant. En utiìisant ìa thermodynamique ìinéaire des processus irréversibìes on donne ìes coefficients de transport interfaciaux.

with it

l.

INTRODUCTION

The

interfacial

an is

internal

energy

important

properties increase

into

to

account.

In this paper,

variations

the (l).

connected

give

to

the

Such

two fluids to

the

interface

is

the

case

is

often

phenomenon a more with

regarded

of

surface

complex the

as

a discontinuity

tension.

structure

introduction

and

of

But

in

some problems

to take more

surface

surface

material

viscosities

which

the dissipation.

of interfacial

use the

region between

of

in order

balances, some

parameters

laws of continuum

definition

of

to give an understanding

we regard

the

Limiting oneself

the interface

are

much

mechanics;

internal to a layer

larger

as

is

Journal de Mécanique Théorique et Appliquéel Journal 0750-7240/1986/22523/$ 4.30/© Gauthier-Villars

Inside

power method

given by the

with a thickness

that

of

is

of the relevant

equations

layer

the space

transition

than outside.

by the virtual

strengths

to the derivation a thin

the

interfacial

for a class

so-called small

Theoretical

of virtual

"second gradient

compared to

and

in which

the

Applied

region

we

motions, theory"

radius of

Mechanics,

the

R. GATIGNOL

226 mean curvature of

the

interface, it

is

P.

'"

SEPPECHER

possible by asymptotic approximation, to

replace the

interfacial layer by a discontinuity surface carrying material properties. The surface quantities are defined by integration over the thickness of

the

layer. Then we can wri te down the laws

of interfacial balances as well as an expression for the interfacial entropy production. First we note that from a physical point of view the properties of the medium in the interfacial region are appreciably different from these of the two adjacent fluids. It is difficult to precise the thickness of the layer. But the experimental work of Palmer, as mentionned in

(2),

the book of Hirschfelder, Curtiss and Bird

allows to say that the thickness for a liquid-

vapor interface is larger and larger, when the critical point is approached. hundreds

of molecular

diameters.

More,

the volumic mass is observed

It may be several

to be a continuous

function

of position in the direction normal to the interface. Under conditions well away from the critical point, however, the a

few molecular diameters (~,

interface

is

an expression

explicitly

(4).

recognized

for the surface tension

layer thickness is only

Nevertheless the three-dimensional in

statistical

mechanical

character of the phase

calculations

in

order

to

obtain

(4). Let

us

consider

a thin

transition

region

with

a finite

thickness, located inside a layer limited by two surfaces " by

"+'

and

and dividing two continuous media denoted

the indices

may

occur

through media

or

generally

more

On

equilibrium the

+

the

interfacial

two

in

l).

are

stress

the

mass

A

transfer

layer. We

suppose

two Newtonian

mixtures

their

contrary

(Fig.

+

and

that the

the

and

of

such

tensors

transition

fluids,

fluids;

are

layer

at

spherical. we

have

for

the medium a preferential direction, so that the stress tensor is not spherical at the equilibrium. The

parameters

mass,

in

the

+

and

two media

(volumic

...)

coefficients,

viscosity

pressure,

are

different but they

smoothly connect one another through

the

specific,

Figure l layer.

surface S by

be

we

introduce

( the normal unit vector to to

four

fluid regions

give a across We

To

an

(Fig.

+

l).

pointing from fluid

S

The space is

R'

R_,

+

divided

On

and

possible profile for a

quantity

can

IjJ

emphasize

the

two

following

interfacial

"true"

integration

(1)

2,

into we

when we go

point. of

to the definition

those of

the

introduced

by

layer of

the

quantities.

interfacial along

view :

of the "true"

interfacial quantities and the second to "excess"

Figure 2

Fig.

the layer in the normal direction.

the first one is related

A

imaginary

inside the interfacial region and we denote

the

quantity thickness

is of

the

real physical quantity describing the medium

MODELISATION

OF FLUID-FLUID

227

INTERFACES

An "excess" interfacial quantity is defined by the following integral s

(2)

(I/!

I/!ex

where

I/!

I/!+)

(or

represents the value

the assumption that this medium the boundary

S

With the filling

were

in

excess,

and that I/!

(or

~

f

- I/! )d~ +

of the quantity

occupies all the I/! +)

- I/!+) d~

+ (I/! a

in

!JJ

region

,

the

introduction of the excess values, the media

the s tJ; ex'

whole is

R_ U

regions

concentrated

R'

and

R' +

the

geometric

surface

on

of

I/!

and

+

+) under limited by

in R_ (or R+). are seen as

respectively, S.

(R+ U R~)

(or

coincides with the true value

(or

medium

U R'

R

while

That is

the

if

they

quantity

corroborated by the

equality

where

X

and

X+

are two values taken by the variable

+.

or

in the media

The thickness of the interfacial layer is not well defined, but we can expect given expression for

I/!:x

does not depend on it.

depends on the precise localisation

of the

surface

S.

(5).

in excess has been first given by Gibbs (1928)

that the

On the other hand, this expression strongly This description with the quantities

A suitable

choice for the surface

S

is

the one for which the interfacial mass in excess, ps , is zero (then S is called equimolecular ex localisation surface). Lastly we can say that with the excess values, the equations on S between the two media

and +

are exactly

jump relations. With

the

introduction

of

the

"true"

interfécial

quanti ties we consider a different approach. of

magnitude

densities interface

the

ratio

of

component

the

gradients

inside

and

of

the

outside

the

by a small adimensional

is characterized

E.

microscopic

variation

is

the

each

region

parameter In

of

of

The order

of

a

described by a

figure

description

quantity

(it

is

I/!

(the

graph similar to possible

to

€l

order

along the normal

the

direction

that given on

have

for

a

the more

complicated function).

o

In

the

macroscopic

interfacial

S the variation of

Thereby two-dimensional

of

through the layer,

I/! on the surface we

can medium.

S (Fig.

consider Such

a

that

description, is

thickness. The value

Figure 3

the value

layer

seen

as

(the a

order

surface

of the quantity

I/!

S

l),

the

without

on the surface

is undefined a priori, but keeping the memory of we may affect the material

surfacic quantity

as

3). we

have

shematisation

is

two

three-dimensional

easy

to

if

understand

media we have

separated no

mass

by

a

transfer

between the interfacial medium and the adjacent media. In

the case where

same, we must belonging

distinguish

to the

the material particles of the interfacial between

two velocities

layer and the velocity

WS

the material

medium are not always the

velocity

of the geometric surface

VS S.

of the particles A discussion about

228

R.

this

difference

has been

The order

of

The value and

of

exact

magnitude

true

is

of

layer

Ishii

(12)

account

(9),

and

(Deemer

and

on the definition

Dumais

the

only

on which

the

Chung

Goodrich

and the calculus

choice

layer

of

the

and

Shaposhnikova

of the surface

et

tension

al.(13),

alone

is

(8),

Albano, and

for

those

the

rarely

except

(for

1:

of an interfacial

(13)

layer

by

values,

consequence.

"excess" quantities,

interfacial

Gogosov

defined.

true

Deemer and Slattery

Za Bin

(l'l),

the

is of slight

of

the

well limited

for

the existence

of

for

is

region

and,

strinked using

alone

the

given,

is

equations

description

(8),

interfacial layer

on the

and Goodrich (11)

Naletova,

Slattery

the

We only mention those

(la)

detailed

SEPPECHER

asymptotically

interfacial balance

Gogosov,

However

of

depends

is

S

P.

(7).

thickness

of many works.

and Vlieger

(6),

quantity

the

the

the concern

quantities.

Gouin

the

position of the surface

Bedeaux of

of

interfacial

The derivation of layer,

recently given,

The thickness

1:+.

the

a

GATIGNOL &

"true"

taken

into

in the many works

instance

(14) ,

Brenner

(15). In

many

presented

analogy

works

as

a

with

relative

to

two-dimensional

the

power,

us mention

and those

surface local

with

enclosing

material are

in

the

material

the

the

(16),

material

Delhaye

(20) to

lead

very

of

the

language

to

a

the

interfacial

by

introduced

are

then postulated (8).

the theorem of the virtual

interface

for

are

Deemer and Slattery

distributions.

nicely

the

(18),

interfaces

are

laws

who apply

where

these

quantities

(17),

Dirac

distribution

symmetry

structure,

The interfacial balance

connected

and they

and

which

and Mazur

quantities

surface

property

a

of Daher and Maugin (19)

Albano

written

a singular

on

continuum.

approach

Bedeaux,

laws

transversality

continuum

with

and Prud 'homme

the

of

the

balance

interfaces

three-dimensional

in an integral form (Barrère Lastly let

the

is

seen

as

In

this

last

a singular work

three-dimensional

interfacial

stress

balance

tensor

are

the

continuum

laws.

then

very

The easy

to obtain. In using

this

the

paper,

components.

S

in

the

second gradient The

without

section

III

thickness.

The balance IV and

Again

in

stress entropy give

its

are

for

of

the

of

true

the

mass,

and,

In

by

the

last

using

the

the

section

of

quantities

linear

interface spheric

at

The

the

thermodynamic

of

the

with a

n

surface

general

form



are

surface

detailed into

the

for

the

irreversible

in

account.

interfacial irreversible

processes,

we

coefficients.

interfacial

zone

In

this

is

considered

section

describe

can

equilibrium

appear and

as

we present

is well known that

cannot

presence

E

o

and entropy on

by

layer

of order

expression

THREE-DIMENSIONAL DESCRIPTION OF THE INTERFACIAL ZONE

It

a mixture

adopted.

the

2.

components.

interfacial region

of

symmetry property of

derive

transport

evolution.

is

a surfactant

and the we

the

case

interfacial

momentum, energy

appearance

transversality condition

discussed.

of

in the

when we only keep the terms

interfacial take

the

description of

theory

schematisation

view

given

how to

the

the

detailed this

the

fluid mixtures

is

IV,

production

The

more

laws

we give

we present

concerns

law is

we explain

section

tensor

;

The point

of an interfacial balance

section

section II, theory

the

the

scope

three-dimensional

and

the equations

phenomena as in

a

discuss

characteristic

set

of

of Newtonian fluids

capillarity. of

the

fluid

Indeed

Newtonian anisotropy

continuum

equations

of

which

or even these

no specific

fluids.

with

Moreover interfaces

does

or

describe

of Newtonian

energy the

one

due

stress not

to

the

tensor appear.

MODELISATION

So these

equations

are not

OF FLUID-FLUID

suitable for

the

229

INTERFACES

description

of

the

evolution

inside

the interfacial

zones. Then we are a

fluid

thermodynamic

think

the

to

in

be

1901,

intersticial flux

the

flux

way than

of

stress the

in

of

suggested

the

us

given

to

consider

and

the

such

classic

fluid

that

is

general

are

:

the

The interfacial

large.

of these

a function

fluid

end we apply

theory.

a consequence

a function

an important

energy

flux

for

difficulty second

the

is

It

large

of

natural

gradients.

its

added

law;

then

internal

: this

principle

have

balance

by

internal these

entropy,

(Gurtin

they

energy.

expression

an energy

for

(23).

of

precised

However

the energy In

flux term

have

balance

using

the

the case of

strengths

order

called what

the

of

to

"flux

possible

powers

(l).

one

description introduces

specified value.

virtual

(Germain

the medium has

classic

naturally

It

law with a well

principle theory

where

than

difficulties.

energy

by

second gradient

in

case

the remove

in the

the

(21) the

for to

obtained

V

an

This

in

the

method

component

only.

an This

class

has

been

Here

these

(25).

a mixture

isotropic

ve loci ty its

barycentric

laws for

medium which

E.

{l, ... .n },

velocity.

We

each component leads

í

s a mixture

We denote

n

with

First

let

us recall

the

virtual

the

virtual

v

class

continuous strengths

af

the power

power

is

an objective it

ai,

and

Bi

to

the

power

the

d

form on

:

motions

is

V

in a Galilean of

forces

for

the space

(second gradient (an objective

no chemical

of

volumic

of the mixture

reaction.

The mass

__1_+VV 3t .

quantities

and external

components volumic

o

dt

principle

acceleration

internal

derivatives

of

theory).

quantity

frame

and for

V

a system each

fields

is

considered of

n

The virtual

an absolute equal

to

the

virtual motion. vectors

Vi

power of the

is a quantity which

with

internal

does not

depend

is expressed). pint

(4)

respect

of

cons ide red virtual

second partial

on the frame where

of

virtual

n mass

equations

V. Ji

and

chronology

the

we have

following

i +p i V.V+

with

by

assume that

to the

dP d"t

(3)

where

the

To this

Application of the virtual power principle

Let

with

the

thermodynamic

allows

is

and Gouin

extended

2.1

The

is

a more

(21).

density gradients

energy

description tensor

mechanic

motions

are

sum of

describing

and Gouin

on the interfaces

(2~

with

working"

for

virtual

by

equations

Dunn and Serrin 1984 (24),

appropriated

used by Casal

and

limitative

internal

Korteweg

appropriated description

balance

of

(Casal

could take.

a unique

results

set

by the presence

that

difficulty

A more

of

less

of energy

incompatible

this

form this

extra

a

of such materials encountered

overcome

with

the

capillarity"

mass of each component and of the gradients of these volumic mass.

Already the study

in

excess

we assume

the volumic

of

construct

characterized

that

Therefore

seems

to

principles

regions are to

going

"endowed with internal

Ci first

- Iv are

tensors

of

two indices,

order so

the

l,

2 and 3. way to

The tensors

write

the

V V Vi

expression

(4)

are is

symmetrical not

unique.

230

It

R. GATIGNOL

becomes unique if we lay down conditions

with respect to the first two indices

(25).

P.

&.

SEPPECHER

to the tensors

The objectivity

Ci

that is to say the

property of

pint

symmetry

has the following

consequences n ¡;

(5)

a

i

a

i=l For simplicity,

is a symmetric

the virtual power of the external pext

(6)

text.V dv +

JV n

where

V

z

(l/p)

forces is supposed of the form

Fext.V

Lav

with

z

p

i=l The external

forces

ds

n

i Vi

p

tensor.

p

i

i=l

are of simple

form and

they

act in a similar

wayan

each constituent

of the mixture. The virtual

power of the

acceleration

quantities

pace

where

with

is the acceleration

vector of the

pace

(7)

fv

p

r.v

It amounts to the same to suppose components playa

are

is a priori

very

near

each

other

i

dv

r

v

~ {l,

order

i that

We assume

--ª-at

with

ri ~ r, in

component.

...

V

,n}.

we could

+

V. V V.

The velocities of the different assume

that

the

inertial

forces

weak part in the diffusion phenomena (25).

From

the virtual

power principle,

for each system

V

and

for each virtual

motion of

iì,

we have

fav

(8)

By integrating by part the terms by taking virtual obtain

velocities

Ili

last

once and the terms a neighbour

of the

Ci

twice,

boundary

aV

of

and

V

we

:

v.ië +

(9)

where

: V Vi

which are zero on

Fext.V ds

¡¡i

and

indices

:

?

are the tensors deduced

from

lBi

"2aßy We obtain the following

local

(la)

p

r

equations

with

a

V V

and

Ci

by permuting the first and the

MODELISATION

(11)

a

OF FLUID-FLUID

INTERFACES

i

i

q;i+~V."C.

V.Bi + V V

O

p

The equation (lO) is the equation (11)

231

i

l, ...

obtained by taking all the virtual

,n

.

velocities

as

equal,

and

by taking all the velocities

equal to zero except one of them. The equation (lO) is the classical balance law for the momentum that we can also write d

(12)

dt g + g V.V

the tensor ~

2.2

- V.~

with

of order 2 is symmetrical and is called

Application of the first

g

p V

the stress tensor ..

and second principles of the thermodynamic

At every time the material derivative of the energy of a system is the sum of the power

Q.

of the external forces and of the rate of the received heat

Denoting by

U

the internal

V and using the kinetic energy theorem (obtained from the virtual power

energy of the system

principle by taking the real velocities), this first principle can be written

(dU/dt) =

Q_

pint.

In a local form it becomes:

du + V V dt u .

( 13)

Here

u

denotes

the

internal

unit of volume and

q

energy

per

unit

of

volume,

r

the

rate

of

the heat current. By using the equation set (11),

energy

source

per

the equation (13)

becomes

(14)

~+ dt

n

(15)

r - V .. q + il:

u V.V

E

(V

1:

i=l

V V + V.E

ci +~ l (iSi - V pl

Vi

.ci)

.Ji)

We emphasize that in the energy equation (14), there appears an extra energy current denoted by

E. To distinguish this extra energy current from the heat current

q

is absolutely

necessary

before defining the entropy current and before using the second principle of the thermodynamic. Indeed we adopt for the entropy current the expression only; here, in a classic

as usual, form :

T

(16)

~~ + s V. V + V. (~) -

where

is the massic entropy and

cr

pi

( 17)

and their gradients

du

1:

ij The

coefficients

~

i

are

¡.j i

u

q

f

cr i: O

cr

is an objective function depending on the entropy

Vpi.

n T ds +

i=l with

related to the current

the entropy production per unit of volume.

Now we aSSume that the internal energy s, the densities

q/T

is the absolute temperature of the medium. We use the entropy balance

u

i

dp

Then we have i

n +

n

1:

i=l V i,j

€o

z

¡.ij Vp j. d (Vp i)

j=l {l, ...

,n}

called chemical potentials. The coefficients

/j

might be

232

R.

called

s

GATIGNOL

"cocapillarity coefficients" ; in the

coefficient (21).

The

coefficients

P. SEPPECHER

case of one component only

are determined in

À ij

n

at most.

n

For

2.3

larger than 3,

only

the quantities

Àij

jgl

À 11

is the capillarity

a unique manner vjp

only

are uniquely

if

n

is

3

determined.

Expression of the entropy production

Let us remark that

the equations (3) imply

n ¿

(l8)

Àij Vp

i

n

~i a

with

Ai V vi + C

Ai

~i _j_(V i) = a .Ji dt p

j=l

+ Il

V V vi

i Àij vpj. V Vp

¿

j=l n

Ai Il

z

n

Ai

¿

C

[2

where

+ Vp i. Vp j [2)

p

Àij

i

Vp j

®

[2

j=l

denotes the unit tensor of order 2.

We assume that equation (17) dissipation

vpj

Àij(Vpi®

j=l

and

the

equation

(l7)

the equations (3),

is

always

(13)

valid

and (16)

(Axiom of the

we obtain

_ .9T

V T + (Ts - u + n

- pint -

n

z

n

By using (18)

.9T

V T + (Ts - u + i

n

+ igl ( a n

+

-

~i a

the

¿

d dt

+

V V

Bi)

V V

i )J

i

êi)

assumptions.

not depend on the

in

theory VJi

of the and

Ji.

V.Ji

We restrict

fluid mixtures.

V V Vi.

study

to a simple

of the

The first of these assumptions

Therefore

Since the quantities

are related by the relation

our

second gradient

in the case of one component only

O

The quantities

Ji

V V Vi

sed

in

.

)

V Ji

[2

1

nor on the first gradient of the mass currents

occur from the terms

i

Vp

P

stresses do

paper of Casal and Gouin

i=l

(p i)2

we make some simplifying

viscous

Bi)

(Ili

¿

/)V.V +

-

(Ili

Vi

usual

- Bj)

(Vp i)

n

i

p

(--.-+

¿

i=l n

In order to go on,

n i=l

i p Il i _ Bi

+ ih(C

tion is

(Ilj

j=l

we arrive to

To

in which

¿

)Jj)V. v +

Àij Vp j

¿

¿

n

pj

j=l

i=l j=l

the

state). From the expression for the

Ta: To

model

local

the following

E {l,

we assume V V Vi

that

; the

E {l,

o ; ...

no dissipation

so we have

,n}

is propo-

second a s sump-

are independent,

... ,n}

i~l V.Ji

v

(21)

velocities

we have

may

233

MODELISATION OF FLUID-FLUID INTERFACES

where

OC

is

a tensor

which does not

depend

on the

index

i.

n jh

V. (Àij

V'p j)

u +

n 1: i=l

Let us denote ,i

i

W

W

P

Ts

~N

- P

D

The dissipation expressions

and the

the

the

limits

considered

terso

of

expression

intricated

to

A complete

the

a mixture. term

stress In the

set

entropy

the

to

the

obtained

classic

current

is

the

-

Vp i ® Vp j

in the

equation

of

the

the to

a::D i

(26),

study

V.V)Vpj

irreversible specify

objectivity

processes

a set

of

principle V'p

i

results

.E.

l,

among the

gradients

i P

P

different

lj(v.Ji

]

term

dissipation

small

is

(20)

term

energy

without

introduced

from

of

laws

for

Curie)

is

thermostatic

the

+pi V.V)Vjp

parame-

n 1: i=l

Ts - u +

E

n 1: i=l

equation energy

set

current

(24). Moreover

spherical.

Wi pi

Wi Ji

for

n

following heat

conventional

current,

only we have

P

Ts - u+pV.(Àll

eN

- p 12

E

Àll

_ À 11

Vp)

Vp ® Vp

p(V.V)Vp

(21)

the

we have

[2

and Gouin

classic in

by Dunn and Serrin

phenomenon is no longer

a mixture with the l,i Ji is called = q + ih " (l/TXq' - 1: wi Ji).

of Casal

the

constitutive

(principle

i

the

follo-

V V'

+ p

parameters

(l6),

the

-

Àij(V.Ji

leads

In the case of a continuum with one constituent

We find

(14) have the

(25).

extra

W

Ji +

n 1: j=l

vector

(l4),

equations

q' quantity

n 1: i=l

of

the

we have

of a medium with

quantity

Ji

in Ref.

r io i ,

hand

~N

case

given

(3),

corresponds

of

-eN

the

Àij

involved

V T - V(w,i)

The application

is

On one

tensor

We find

current

dissipation

\..l,i

usually

n 1: j=l

i

~N

thermodynamic

the

appearance

study

u,i

linear

for

mixture.

due

E ; this

the

(20)

The equation

the

n 1: i=l

E

In

for

..9. T

Ta

(21)

the

energy

p

:

(20)

of

extra

)..l,i

n 1: i=l

-

[2

-z:

-z:

wing

-

and Dunn and Serrin

(24).

and

difference

consequent

ly

: the

234

R.

Let of

us assume that

the linear

the viscous

the

thermic

thermodynamic

stress

of

and

the

intrinsic

o With five transport

must verify

dissipations

.!.(V

us

(21).

this

Lastly

define

a

last

an

of

interfacial

to be straight

be

expression the

is more complete

inequalities

the

gradients

the

~o.

to

is

well

to

WS

than

these

the

five

expression

coefficients

the

the

has

is

small

where

of in

such a

a small

of

we

some

¡;

have

a

O

region,

thickness

with

in

with

are

of

these

components.

TI

very

addition

The lines

1;.

in this

have

mixture

components

the directions

direction

we then

the space

much

large the

larger

than

gradients.

property

ç

of the field

We

that are

all

assumed

layer. direction. In the case

a contact

layer.

layer

small

and

¿

surfaces

But

for

S.

l).

Let

normal

surfaces

such as

line

or

a

contact

where

the

large

point

the

study

Let

presentation

layer us

of

is

be

I;

the the

are

I;

to

parallel

the distance

rate

of

volumic

masses

common direction surfaces

of

between

convenience

a motion

¿

and

¿

and

S,

that

surfaces

equal

of

the

densi ty

only which

of

will S

WS

by

the normal

(Fig.

+

of

l)

order

the normal

= O,

and

F,

the displacement

component

appear

on itself.

¿+

is

by F,

We denote

and ¿

the layer. We denote

in motion.

remark

which defines

LO, of

¿.

located inside

equations

interfacial

some

component

the

and

by two extreme

surface

.

«

(E

surfaces

as parallel

interfacial are

The

Öo

scales,

respectively

the

problem the

a tangential

region

masses

the normals to the interfacial

moving surface

defined.

- (ß + v)2

LAYER

being

be an isodensity

In,a dynamic of

as

and appear

gradients S

region

layer

inside

the

Let

co-ordinate

velocity

that

O

¡;

+ ~ - 2ß)

À(y

volumic

directions

ratio

each constituent,

=

for

(25).

inside and outside

ÖO

layer

the

We delimit

O

have a preferential

different

in Ref.

Let

on which

this

and to define

have

of which. is

the

layer

The interfacial gradients

¡;

three-dimensional

gradients

the considered gradients

for

+ Y + ~ + 2v

We assume that

density

theory

results

TVPT

we give

OF THE INTERFACIAL

consider

the

it

outside.

Then the

following

:

MODELISATION

Let

the

Vp

+ Vv)

V

2

coefficients

and Gouin

À

Inside

uncoupled.

to

® I; + I; ® 1;.0)

À

3.

are leads

tensor

where

by Casal

SEPPECHER

irreversible proccesses

ß(O.I;

chosen

P.

GATIGNOL &.

later

W':_ on,

of we

WS give

MODELISATIONOF FLUID-FLUID

To each

physical



quantities

quantity

and

f defined

in the interfacial layer,

~+

f~

We define

the

particles

interface

ps

per by

p

down the

(25)

ò

J

is

the unit

current of

fV

t

of

W dv

In

and

law for

a quantity

form for

a volume

W + W V.W + v. (W(V -

t;

area

W V

with

equation

the

field

f

V

is

W

which

which

is

Let

A

Ws,

and

be a piece limi ted

denote

by

v

normal

to

C, the

T

= I; A v

generated

of

equal

V

(w(V

- W) + J).I;

ds +

fA

the

on

S

the the

S

outward

and

pointed vector

the velocity

of

introduce to

the the

on

lateral

and as

surface

C,

and

the

the

S,

A,

surfaces the

surfaces

A~.

surface

for

C we to

such

C

leaning on

(24)

+ W.V).

a/at

Along

to

cut ted

the

asso-

tangent

normals

and

space Annex).

uni t normal

outside

thin

We

volume

A~, A

by the boundaries

J).n

C.

vector

We also

by

=

(IS/1St

curve

unit

the

whole (cf.

moving with

the

tangent

source

velocity

time derivative

W

and

- W) +

(w(V

aV :

of

the

in

the

equation

rate

with

WS

n

densities

limited

the

to

of

by

A the

(w(V

~

firstly

surface

defined

by

(Fig. 4).

A~

4

of volume,

¢l

with the velocity

and

fA

is

equal

o/1St

write

+

and

by

pieces

wdv

W,

denoted

T

unit

a volume moving

and by

by

IV

of

VS

dv



V

av,

ciated

1St

per

We have to

(26)

velocity

limited by the

quantity

(24),

and

Figure

material

+ J)

W)

+ f aV (w(V - W) + J) .n ds

the

the



density associated

volume.

unit



classical conservation

ò

density per

s

and secondly in an integral

(24)

where

two interfacial

( f)

d~

(Ishii (12)

(23)

We write

f

interfacial mass

on the

in a local form,

we associate

(f)

(22)

the

235

INTERFACES

ds

- W) + J).I;

fv

ds



dv

+ In

order

the

to

introduce

integral

denote

by

expressions H

form

(cf.

mean

curvature

the

Annex),

the

interfacial quantities

appearing

in

three-dimensional and

of order

H

the LO

this

last

tensor

of

mean curvature. (or of order

de f í.ned in equation. order

(22), each

2 associated

We shall

larger

In

than

limit LO

our

we are point

of

with

the

study to

in order

going the

to

transform

surface

second

interfaces

to consider

S

we

fundamental

plane

with

a

inter-

236

R. GATIGNOL &

faces).

Let

us

remark

On these conditions

that

~/L

we have

P. SEPPECHER

O(E)

at

each

point

inside the

interfacial

layer.

we have

fv

f dv

(27)

(fA

fA

f

(Cf

C

fCf.(1l2

d~

~

i

(28)

~+

f

ds

f.n

+ O(E»

- .~).

and in

We

is

P.

&

source

entropy

at lj;

one

densities.

and

a

and

represents

This

priori

the

the

same

the

inside

mass,

assumption

partial

time

total

is

volumic

the

and

momen-

released masses

if of

ljJ

each

constituent.

4.1.

Balance

From tuent

the

law of masses

equation

(3)

and

by

using

the

formalism

of

section

III

we obtain

(36)

p

By adding

i-consti-

the

is

(36)

equations

and

by using

the

definition

W//:

of

»//

_ Ws



by

the




O,

S

divides

normal (II

is

to

S

nega-

and positive

of

expression

in

the

are

the

the curvature

orthonormal

tensor associated

frame defined

by the

with the second fundamental

principal

directions

of

S,

is

following

where

and

tensor

as being

H

two principal

the tensor

with the

curvature

radii.

O

O

O

O

the

orthonormal

frame

We construct a three-dimensional

components

O

in

F

equation The

case).

In each point

the

>

F

region

when the surface

in the opposite

form

E

in

two regions

defined by the

O

O

two principal

directions

of

S

and the normal vector

f;.

Surface

e. of

divergence theorem

Let

B

Along

C

A,

be

a vector

we denote

and by

the

T

field by

one uses

{V Il (f; Il B)l.f;,

is

unit to

E. Let

vector C

A

be a part

tangent

such that

T

to

= f;

S,

of

normal

Il v (Fig.

S to 4).

limited C

and

by the

curve

pointing

We have:

JeB.hllf;)di

the classical it

defined in the

tangent vector

Je B.v di

where

v

easy

theorem to verify

of

Stokes.

that:

If

L

represents the operator

such

that

L(B)

out

MODELISATION

L(B) where

~2

OF FLUID-FLUID

INTERFACES

245

(12 - ( () : V B - (V.()(B.()

is the unit tensor of order two. Let us remark that the operator

X

denoted by

in Barrère and Prud'homme

L

is the operator

(16).

We introduce the following notation P = ~2

-

A//

(

(

projection operator on S (p = ~ = ~2)

A.~

=

s

B// = ~.B

A

is a tensor

where

~

V .B s V

with

f

V B IP.V

= B.P

BJo =(B.(l(,

or order 2 or more,

surface divergence

f

,

surface

of

gradient of

B f

So we have L( BJ.)

'1.(

O

L(B)

With the introduced notations the surface divergence is written

J Surface transport

S

We define the velocity the point Let book of

P us

W

and

M

recall

the

(29)

transport

theorem

us denote by

WS

E

of

is the orthogonal projection of

Germain

M

JA

B. ( dA =

öB JA 16T

t

as is

it

is

given,

used

to

mention

+ B V. W-B. V

wl. (

dA

it is easy to obtain

ò

t

J A fdA

or ò

t

JA

J A l if' +f öt f dA

V.W

Ws. ( =-(aF/at)/ l'IF I. -+

-+

OM = OP + PM ( where

S.

WS

t

its displacement veloci-

by using the relation

on surface

s s /ö

WS

satisfies the relation

on a surface

and where the notation

ö

f (

in motion and let

F(x, t) = O

in each point

ó

B

S

is now

is moving with the velocity

With

B. v di

theorem

Let us suppose the surface ty. The equation of

C

- f (.('1 W).() dA

for that

instance, the

in

the

surface

S

R. GATIGNOL

246

P.

&

SEPPECHER

REFERENCES

(l)

P. GERMAIN La méthode des puissances 12, p , 235-274 (1973).

ui rt.uel.l.ee en mécanique des milieux

continus.

(2) J.O. HIRSCHFELDER, C.F. CURTISS and R. B. BIRD Molecular Theory of Gases and Liquids. John Wiley & Sons, INC, New York, (3) V.G. LEVICH Physico-chemical Hydrodynamics. Englewood Cliffs N.J. Prentice-Hall,

J. Méca., vol.

(1954).

INC.

(1962)

(4) Y. ROCARD Thermodynamique. Masson, (5)

Paris

J.W. GIBBS The Scientific Papers of J. p. 219-274 (1961).

(1952). wiUard

Gibbs.

(6)

R. GATIGNOL Conditions de saut à travers une interface de Mécanique. p. 318-319 (1985).

(7)

R. GATIGNOL Liquid-Vapor interface

(8)

conditions

Dover

Publications,

fluide-fluide.

Actes

A.R. DEEMER and J.C. SLATTERY Balance equations and structural vo l . 4, p , 171-192 (1978)

models for

phase interfaces.

ALBANO, D. BEDEAUX and J. VLIEGER On the description of interfacial properties using singular a dividing surface. Physica, vol. 99A, p. 293-304 (1979).

(ID)

J.F. DUMAIS Two and three-dimensional

interfacial

(11)

F.C. GOODRICH The theory of capiUary (1981).

excess

(13)

(14)

M. ISHII Thermo-fluid

du 7ème

vol. l,

Congrès

Français

(To be appeared).

(9) A.M.

(12)

INC. New York,

Int.

densities

dynamics. Physica, vol. 104A,

viscosities.

Proc.

R.

dynamic theory of two phase flow. Eyrolles,

Soc.

J. Multiphase Flow,

p,

Lond.,

and currents

143-180 (1980). vol. A374,

p,

341-370

Paris (1975).

V.V. GOGOSOV, V.A. NALETOVA, CHUNG ZA BIN and G.A. SHAPOSHNIKOVA Conservation laws for the mass, momentum, and energy on a phase interface excess surface parameters. Fluid Dynamics. Vol. 6, p. 923-930 (1983). H. BRENNER Micromechanical derivation of the differential Interface Sci. 68, nO 3 p. 422-439 (1979).

at

equation

of interfacial

for

static.

true and

J.

Coll.

(15)

H. GOUIN Tension superficielle dynamique et effet Marangoni pour les interfaces liquide vapeur en théorie de La capiUarité interne. C. R. Acad. Sc. Paris, t. 303, série Il, n? l, p , 5-8 (1986).

(16)

M. BARRERE et R. PRUD'HOMME Equations fondamentales de l'aérothermochimie.

Masson, Paris (1973).

(17)

J.M. DELHAYE Jump Conditions and Entropy Sources l: p. 395-409 (1974).

(18)

J.M. DELHAYE Local Instantaneous Equations. In : Thermohudraul-ice of two-phase systems for industrial design and nuclear engineering. Edited by J.M. Delhaye, M. Giot and M.L. Riethmuller, Hemisphère Publishing Corperatio~ Washington, p. 95-115 (1981).

in

two-phase

systems.

Int. J.

Multiphase

Flow, vol.

MODELISATION

OF FLUID-FLUID

INTERFACES

247

(19)

N. DAHER and G.A. MAUGIN The Method of Virtual Power in Continuum Mechanics. Application to Media Presenting Singular Surfaces on Interfaces. Acta Mechanica, vol. 60, p. 217-240 (1986).

(20)

D. BEDEAUX, A.M. ALBANO and P. MAZUR Boundary conditions and non-equilibrium (1976).

(21)

thermodynamics.

Physica, vol.

82A,

p.

438-462

P. CASAL et H. GOUIN Relation entre l 'équation de l 'énergie et l 'équation de mouuement: en théorie de Korteweg de la capillarité. C. R. Acad. Sc. Paris, t. 300, série II, nO 7, p. 231-234 (1985).

(22) D.J. KORTEWEG Archives Néerlandaises, Vol. II, 6, p.

1-24 (1901).

(23) M.E. GURTIN Thermodynamics and the possibility of spatial Rational Mech. Anal., vol. 19, p. 339-352 (1965). (24) J.E. DUNN et J. SERRIN On the Thermomechanics p , 95-133 (1985).

of Interstitial

Working.

interaction

Arch.

in elastic

Rational

Mech.

materials.

Anal.,

vol.

Arch.

88,

(25) P. SEPPECHER Modélisation des zones capillaires. Mémoire de thèse, Université Paris VI (1987). (26)

S.R. de GROOT and P. MAZUR Non-equilibrium thermodynamics.

North-Holland Publishing Company, Amsterdam (1962).

(27)

B.J.A. ZIELINSKA and D. BEDEAUX A hydrodynamic theory for fluctuations around equilibrium of a liquid vapour interface. Physica, vol. l12A, p. 265-286 (1981).

(28)

S. CHAPMAN and T.G. COWLING The Mathematical Theory of Non-uniform Gases.

(29) P. GERMAIN Cours de Mécanique dee Milieux Continus, (1973).

University Press, Cambridge, (1960).

Tome 1,

Théorie Générale.

Masson et Cie, Paris