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Permeative and hydroelastic flow in smectic A liquid crystals

R. Bartolino, Geoffroy Durand

To cite this version:

R. Bartolino, Geoffroy Durand. Permeative and hydroelastic flow in smectic A liquid crystals. Journal

de Physique, 1981, 42 (10), pp.1445-1451. �10.1051/jphys:0198100420100144500�. �jpa-00209336�

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Permeative and hydroelastic flow in smectic A liquid crystals

R. Bartolino (*) and G. Durand

Laboratoire de Physique des Solides, Bât. 510, Université de Paris-Sud, 91405 Orsay, France

(Reçu le 7 avril 1981, accepté le 9 juin 1981)

Résumé.

2014

Nous calculons l’écoulement et la déformation élastique d’une lame de smectique A idéal comprimée

sinusoidalement entre deux membranes parallèles

aux

couches. A basse fréquence, la perméation apparaît dans

les deux couches limites prévues précédemment. A haute fréquence la perméation disparaît. L’écoulement est

une

pure distorsion hydroélastique, où les couches smectiques sont gelées dans la matière. La partie élastique de l’impédance mécanique de la lame smectique subit une relaxation, augmentant de 20% par rapport

au

régime élastique de basse fréquence. Une tension de surface finie doit supprimer les couches limites de perméation à

basse fréquence.

Abstract.

2014

We compute the coupled flow and elastic distortion of

an

ideal smectic A liquid crystal normally squeezed between two oscillating plates parallel to the layers. At low frequency, permeation occurs within the boundary layers as already predicted. At high frequency, permeation vanishes. The flow is

a

pure hydroelastic distortion, with the smectic layers

«

frozen » inside the matter. The elastic part of the mechanical impedance of

the smectic slab undergoes

a

relaxation, increasing by 20 % above the purely elastic low frequency regime. Surface

tension will suppress the permeation boundary layers at low frequency.

Classification

Physics Abstracts

61.30

-

62.40

-

46.30M - 47.55M

Each layer of a smectic A liquid crystal [1] is a two

dimensional fluid. In defect-free samples, a flow nor-

mal to the layers is generally associated with layer

motion itself. For fixed layers, a weak permeative [2]

flow can be induced by a pressure gradient normal

to the layers. A D.C. squeezing flow has been pre-

viously described [3], for the case of a non ideal smectic

A containing so many defects that the layer number

is not a conserved quantity. An interesting prediction

of this model is the existence of a permeation boundary layer close to the boundary plates, across which the

pressure gradient necessary to induce permeation can

relax by inducing lateral flow. When the smectic slab is thicker than the boundary layer, the flow should be

permeation limited. Experimentally, to observe such

a behaviour, an oscillating squeezing flow [4] is much

easier to realize. In this paper, we have extended the D.C. model of reference [3] to the case of A.C. squeezing

oscillations. Assuming small amplitude oscillations we can keep the ideal (defect-free) model for the smectic A.

We compute first the flow and the layer distortions

versus frequency. We then derive the expression of the

transmitted force through the smectic layers, i.e. the quantity of interest for an experimentalist who can easily measure the mechanical impedance of a smectic

slab versus the frequency [5].

(*) On leave from Universita degli Studi di Calabria, Diparti-

mento di Fisica, Arcavacata di Rende, Cosenza, Italia.

Our model is the following : we consider a smectic

slab of thickness 2 d squeezed between two parallel

membranes of large size L > d (Fig. 1). The two

membranes vibrate along Oz, normal to the smectic

layers, with amplitudes + ô exp(iwt).cos qx x, with

qx

=

x/L. We restrict our analysis to an incompres-

sible two dimensional flow in the plane (x, z). Using

the same notations of reference [3], we call u the z displacement of the layers, Vz and Vx the components of the mass velocity, p the specific mass, p the excess

pressure, B the smectic layer compression elastic

constant, 1 an averaged viscosity, Â the permeation

constant. The edges of the smectic drop form a free

surface. We neglect the surface tension and take p

=

0 (and u

=

0) at the edges. We are interested in « thick

samples, where the thickness d is larger than the boun-

dary layer thickness 1

-

(mL )1/2 (m is a molecular

Fig. 1.

-

The cell geometry.

Article published online by EDP Sciences and available at http://dx.doi.org/10.1051/jphys:0198100420100144500

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1446

length). In this case we can neglect curvature elasticity compared to layer compression elasticity.

The flow in the smectic slab is described by the

Navier-Stokes equations :

where g

=

B ô2u/ôz2 is the elastic force density asso-

ciated with layer compression. We describe the viscous

coupling between flow and layer distortion with the

permeation equation :

The boundary conditions on the upper and lower mem-

branes are :

(sticking condition for the flow) and

and

(no permeation through the membranes).

1. The simplified low frequency model. - We, first study the non inertial regime, assuming co «n/pd2

(~ 103 to 105 Hz) so that we can drop the acceleration terms. The incompressibility condition div V

=

0 results in

which allows the pressure to be eliminated. Using (1), (3) and (5), and the thickness condition L > d,

one obtains an equation for u

which on integration becomes,

where we call m2 = À YI and ÂB = m2 BI YI

=

m2/i.

m is a molecular length. Because of the symmetry of the problem, /3s

=

0. The solution of (7) is the super-

position of the particular solution u

=

oc(x, t) z and

the general solution of the equation,

which becomes after a Fourier transform :

In order to simplify the following, we drop the obvious

x and t dependence on u and V. To obtain (6), we have

used the low frequency approximation wT 1, and 1 qz 1 > qx. With B - 10’ and il

=

0.1 cgs, one finds

’t ~ 10- 8 S so that the low frequency approximation

allows a wide range of frequencies to be considered.

We shall discuss later the thickness condition.

For a given frequency Wt, solution of the dispersion relationship (8b) gives two purely imaginary (diffusion like) roots :

and the general solution of (8a) is, because of the ± z symmetry :

At low frequencies (Wt mqx), the two roots of (8b)

have the same modulus 1 qz 12 = 1 q’ z 2

=

qxlm, which

is the inverse squared thickness of the permeation boundary layer [3]. At. high frequencies (cor > mqx)’

the two roots are :

qZ is related to the diffusive motion of the smectic

layers, under the elastic restoring force proportional

to the curvature qX, in the absence of permeation.

We shall call this motion the « hydroelastic » mode.

qz is related to the diffusive motion of the smectic

layers due to the pure permeation mechanism, in the

absence of flow. It is the « permeation » mode. In

contrast with the low frequency regime, at high fre- quencies, the permeative and hydroelastic modes are decoupled. For wT~‘ 1, their spatial extension along z

is comparable with L (hydroelastic mode) or m (per-

meation mode). As we have assumed cvi « 1, the

condition ( qZ I > qx is satisfied even for the long wave- length hydroelastic mode.

1.1 CALCULATION OF THE DISTORTION.

-

We can now compute explicitly the distortion u versus cor,

using the three boundary conditions on the membra-

nes. (4a) becomes :

(4)

This can be transformed, using the dispersion rela- tionship (8b) to :

iwTa+

(4b) and (4c) give :

The solution of I

where

So that the distortion u can be written as :

1.2 CALCULATION OF THE VELOCITY FIELD.

-

V’ z

=

V z(Z) cos qx x is obtained directly from the permeation equation (3)

We derive Vx

=

Yx(z) sin qx x from the incompres- sibility condition

1.3 REACTION OF THE SMECTIC SLAB ON THE MEM- BRANES.

-

The normal stress exerted by a smectic layer on a lower z layer is

On the lower plate, because of the boundary condi-

tion (4a),

To compute p

=

p(z) cos qx x, we use the Navier- Stokes equation (2) and the previously computed Vx(z) and Vz(z) (Eqs. (19) and (17)). We obtain :

and using (8a), the reduced normal stress is simply :

1.4 DISCUSSION.

-

Contrary to reference [3], we

have assumed no permeation on the membranes. The first point to consider is why there should be any

permeation at all close to the membranes. This follows

directly from the boundary conditions. On the mem-

branes, Ù V- (4c). We also have avz/az

=

0 (4a),

but êulêz is non vanishing, because of the mechanical

reaction of the smectic spring to the externally forced displacement b. This results in

close to the membranes and permeation must occur.

In discussing the properties of the squeezed smectic

slab the most relevant parameter is the ratio of the

sample thickness to the boundary layer thickness.

Of secondary interest is the reduced frequency (DT.

Let us discuss here the case of thick samples

For zero frequency, V and û vanish. u obeys the

standard equilibrium equation

Apart from the cos qx x dependence,

u

is the simple homogeneous distortion :

The transmitted normal stress on the lower plate is :

The mechanical reduced « impedance » of the

smectic slab is

In principle, it is then possible, for an ideal sample, to

deduce the unidimensional elastic modulus B in a D.C.

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1448

squeezing experiment, by measuring the normal stress

S, versus the applied strain ôld, in the zero frequency

limit.

It is interesting to look at the velocity field for vanishing Wt, to make a comparison with the distor- tion profile. Vz and Vx are of the order of iw03B4 and

irobldqx’ We have then plotted on figures 2 and 3 the

normalized thickness profiles of Vz(z)/(irob) and Vx(z) dqxlirob for 03C9T

=

0. One sees clearly that the boundary layer region is the only one where a standard hydrodynamical flow occurs, with an exchange bet- ween Vz and Vx. The maximum on the Vx profile corresponds to the largest slope of VZ, where the VZ profile joins back to the linear profile of u(z). In bet-

ween the two boundary layers, we observe a region

of uniform distortion along both x and z directions, where Vz - ù and no permeation occurs. This region corresponds to that part of the smectic slab which

undergoes a solid-like « hydroelastic » distortion.

Fig. 2.

-

Normalized velocity profiles Re (Vz/iwb) for

mi =

0

and

mi - oo.

The linear dotted line gives for comparison the

zero

frequency normalized distortion u/b. 1 is the permeation boundary layer thickness for

mi =

0. Only

one

half of the profile 0

z

d

is represented, the other part ( - d

z

0) is symmetrical.

Fig. 3.

-

Normalized velocity profiles Re (Vx dqx/irot) for

wT =

0

and

mi - oo.

1 ils the permeation boundary layer thickness. The onset of surface tension will force

a

constant curvature at

zero

frequency and suppress the permeation boundary layer.

Increasing the frequency, one finds a regime where

the amplitude of the permeation flow is a maximum.

2

2

This occurs when ù _ M2 ô2U T TZ2

1

i.e. for (WT)p ~

p

mqx. qx At this frequency the distortion profile is already

Fig. 4.

-

Normalized profiles for the

mass

velocity V and the layer velocity û, for

mi -

mqx when permeation is at

a

maximum.

The permeation boundary layer thickness is larger than 1.

distorted from the elastic profile (25), as shown in figure 4. Increasing further the frequency, the per- meation amplitude decreases roughly as mqxlwt, which

means that icou and Vz have the same thickness profile.

The smectic layers are « frozen » in the smectic mate-

rial, since Ù - Vz. The flow is purely hydroelastic.

Another important frequency is that where the z

extension of the hydroelastic mode is comparable with

the thickness. From (11a), this occurs for (wT)H ~ qx d 2.

Of course, (Wt)H is larger than (wt)p, because we are considering the thick sample case (qxlm) d 2 > 1.

Above (wt)H’ where the viscous forces dominate the elastic forces, the flow must be the same as in a simple

viscous fluid. One can derive the velocity profile from

the limit of (17) and (19) at large wT. It is simpler to

recalculate it from the high frequency limit of the

equations of motion. For high frequency, ù

=

Vz,

from (3). (6) gives 84ul8z4

=

a4 vZ/az4 - 0. From (23)

we see that p is independent of z, which leads to a

standard Poiseuille flow for Yx. The solution is simply :

and

This high frequency Poiseuille profile is shown in

figures 2 and 3.

1. S MECHANICAL IMPEDANCE OF THE SMECTIC SLAB.

-

For our practical problem, it is interesting to consi-

der the frequency dependence of the normalized impe-

dance Z of the smectic slab, previously defined in

equations (27) and (23). For Wt well below (Wt)p, one

obtains the following expansion :

where J1 is the dimensionless thickness

(6)

We are now considering the case of large J1 so that (30)

reduces simply to :

In addition to the elastic contribution 1, we should observe a viscous contribution proportional to the

membrane velocity icvô. In the case of a simple viscous fluid, one should have (see later) :

(31) shows that in presence of permeation, the smec-

tic slab behaves mechanically as a spring in series with

a simple viscous fluid squeezed between the same two

membranes, the thickness of which is (ld)1/2, the square root of the product of the sample thickness d by the permeation boundary layer thickness l= (mlqx)1/2.

For wt larger than (wt)H’ the normalized impedance

is as follows,

Using the high frequency limit (11a) for qz, one obtains the expression :

the imaginary part of Z diverges ; since for large fre-

quency the viscous forces dominate the elastic forces,

this imaginary part must be the normalized impe-

dance of a simple viscous fluid slab, in the same geome-

try. This can be checked directly by solving the con-

ventional « thrust bearing » problem in our geometry.

It is interesting to understand the 20 % increase in the elastic part of Z. This high frequency strengthening

is simply related to the fact that the smectic layers

are « frozen » in the material. The high frequency

distortion profile u(z) does not minimize the elastic

Fig. 5.

-

Normalized impedance of the smectic slab

versus

the

frequency. Above the maximum permeation frequency (Wt)p ’" mqx,

the friction decreases and the apparent elastic modulus increases

by 20 % (see text).

free energy anymore. The apparent reduced elastic constant can be estimated in the following way,

using for u equation (28), one readily finds Z = 5

=

1.2.

The frequency dependence of Z is shown in figure 5,

which demonstrates the relaxation of the apparent elastic constant above (wT)H’ from 1 to 1.2.

2. Discussion.

-

2.1 THE INERTIAL REGIME.

-

In the previous calculation, we have neglected inertia

terms. The results represent the wT

-+

0 limit of the

more general solution. It is useful to understand what

happens when inertia is taken into account. As usual, dealing with small amplitude oscillations, we can

linearize the Navier-Stokes equations (1) and (2), writing :

We now introduce the maximum second sound

velocity c by

In addition to the low frequency and thickness condi- tions wT 1 and qz > qx, we introduce the additional condition :

which means that, for the molecular frequency T - 1,

the second sound wavelength is much larger than the

molecular length m. We finally obtain the new dis-

persion relationship :

The second sound velocity, for a distortion of wave

number q(qx, qz), is c qx qz With our assumption of a

q2

thin sample, we must have q - qz. The frequency

ws

=

cqx is just the frequency of the second sound wave associated with the layer distortion. As long as úJ ws, the previous discussion remains valid. Close to w

=

ws, the membrane vibrations will excite, at resonance, second sound waves. In practice, úJs is of the order of 104 Hz. The resonant excitation of second sound

waves at úJs has not yet been observed, although it

could correspond to the unexplained low frequency

mode found in Rayleigh scattering [6].

We can try to estimate the influence of inertia on Z,

when increasing the frequency, well below ws Resum-

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1450

ing the calculation of the pressure (Eq. (22)), we find

for the reduced normal stress :

instead of a (Eq. (23)). The detailed expression of Sz

is clumsy. Note only that inertia introduces W2 terms in the mechanical impedance of the slab.

2.2 THE ASYMMETRIC CELL.

-

To measure

the mechanical impedance Z, experimentally it would

be more convenient to excite the vibrations of only

one (the upper) membrane, and to deduce Z from the

transmitted force exerted on the other static (the lower)

membrane. One can find the solution of this non

symmetric problem by superposition of the previous

« symmetric » solution with that of the « antisym-

metric » problem, where the two membranes are

assumed to vibrate in phase as :

The superposition of the two solutions gives the boundary conditions of a vibrating upper plate, with amplitude 2 03B4, and of a static lower plate with zero amplitude.

So long as we remain in the non inertial approxi- mation, the

«

antisymmetric » solution is the uniform distortion u(z)

=

u(d), Vz

=

iwô, V x

=

0. The trans-

mitted force across the smectic slab remains the same.

In the non inertial regime, we must also take into account the inertial force associated with the oscil- lation of the centre of mass. This results in an addi- tional pressure term :

i.e. to an additional term in the mechanical reduced

impedance :

For the second sound resonance ws, this remains a

weak correction - q’ d 2 1, because the sample

is thin.

2. 3 SURFACE EFFECTS.

-

In our model, we have neglected the surface tension at the free edges of the

smectic slab. This can be justified physically if we use a surfactant, for example, or if the free edges break into steps to allow the smectic layers to glide across the

side surface of the sample. It is interesting to estimate

what happens in the presence of a smooth curved edge

surface with surface tension.

Assume as previously that the free edges are vertical

in the absence of membrane deformation. At low

frequencies, the velocity profile Vx is shown in figure 3.

The lateral displacement of the edge is :

The Laplace pressure due to surface tension is

since we restrict our model to two dimensions.

V, is the superposition of the hydroelastic part

i03C903B4 Z/d and of a Poiseuille-like flow within the per- d

meation boundary layer of thickness

This Poiseuille flow has an amplitude v., - p

Z

iwô 1 d

Writing the incompressibility condition across the boundary layer, one finds a contribution to the lateral

displacement of the order : y - Lô/d and a Laplace

~

y ô

pressure P1 ~y. Note now that, because m is a

p m d

molecular dimension, y/m is of the order of B, the smectic layers compression modulus, so that :

The physical meaning of equation (46) is important.

Let us recall an argument from de Gennes [1]. The permeation boundary layer appears because the pressure gradient normal to the layers can be relaxed by a lateral flow at distance 1 from the membranes.

The lateral drop of pressure is primarily due to the

viscous drag. The Laplace pressure (46) is of the order of the normal elastic stress across the smectic

layers. From equation (31), we know that in the low

frequency limit the pressure gradient - B au g ~z is much

weaker than the elastic stress. The permeation boun- dary layer thickness must increase.

To understand qualitatively how this occurs let us

consider the Navier-Stokes equation (2). Including

the Laplace surface term, the pressure is now :

Using the permeation condition equation Vz ~ À P/1

and the incompressibility, we obtain :

to be compared with Lm in the absence of surface tension. For zero frequency, 1 becomes infinite. This is obvious because hydrostatic equilibrium in the

presence of Laplace pressure implies a constant cur-

vature for the edge of the squeezed smectic slab, so

that the profile of figure 3 is not an equilibrium profile.

For frequencies larger than ylr¡L (_ 102-103 Hz)

i.e. for

(8)

the model without surface tension remains valid.

There should be a critical frequency (COr)d smaller

than (wt)p for which 1 - d, i.e. for thick samples,

The permeation boundary layer should exist for

frequencies between (Wt)d and but must disap-

pear at low frequencies. Remember that from our

previous analysis, it disappears also above (W’t)H’ Of

course, a correct description of what happens between (Wt)d and (cor), must take into account the Vz flow

induced by the non uniform Laplace pressure. This results in capillary surface wave emission. The pro-

pagation of capillary surface waves on a smectic A has already been discussed for an unconfined geometry

by D. Langevin [7]. The problem of their propagation

and resonances in the confined geometry of the smectic slab appears to be more complicated. As we do not

know much [8] about the real state of smectic free edges,

we shall not try to discuss this question here.

The conclusion of this section is that, in the presence of surface tension, the permeation boundary layers

must disappear at low frequencies. For thick samples they could be observable around the low frequency y/ ilL (i.e. close to the maximum permeation frequency),

and lead to the excitation of capillary surface waves.

This result demonstrates the important effect of surface

properties on the three dimensional permeative flow

inside a smectic A liquid crystal.

2.4 CURVATURE ELASTICITY.

-

In the simplified model, we have neglected nematic-like curvature

elasticity. Is this assumption correct ? In the absence of surface tension the largest curvature appears at the

edges of the permeation boundary layers. The ampli-

tude of the layer displacement u which is curved is

u - bl/d, so that the maximum curvature energy

density is of the order of :

We have used the relationship K - Bm2 for the

Frank curvature elastic constant K. The nematic curvature energy is always negligible. The same result obviously applies in the presence of surface tension,

since the edge curvature decreases.

3. Conclusion.

-

We have computed the flow and distortion profiles inside a « thick » ideal smectic A

slab, submitted to a small periodic layer compression.

In the absence of surface tension, permeation occurs

at low frequencies in the two boundary layers as already predicted. At high frequencies, the smectic

layers are frozen into the material. The flow is Poi- seuille-like. The elastic part of the mechanical impe-

dance undergoes a relaxation, increasing by 20 %.

The inertial regime at higher frequencies should lead to a resonant second sound excitation. In the presence of surface tension, the permeation boundary layers are suppressed at low frequencies. At intermediate fre-

quencies, they should lead to excitation of surface

capillary waves. Systematic observations of the free surface and measurements of the surface tension of a

smectic A are required to check which model should

apply.

Acknowledgments.

-

We have benefited from dis- cussions with M. Kléman, Ph. Martinot-Lagarde and

J. Friedel.

References

[1] See for instance :

DE

GENNES, P. G., The Physics of Liquid Crystals (Clarendon, Oxford) 1975.

[2] HELFRICH, W., Phys. Rev. Lett. 23 (1969) 372.

[3] ORSAY GROUP

ON

LIQUID CRYSTALS, J. Phys. C 1 (1975) 305.

[4] BARTOLINO, R., DURAND, G., Phys. Rev. Lett. 39 (1977) 1346.

[5] DURAND, G., BARTOLINO, R., CAGNON, M., in Liquid Crystals of

one

and two Dimensional order (Springer Verlag, Berlin) 1980.

[6] RICARD, L., PROST, J., J. Physique Colloq. 40 (1979) C3-83.

[7] LANGEVIN, D., J. Physique 37 (1976) 737.

[8] LANGEVIN, D., J. Physique 37 (1976) 755.

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