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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�
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.
2014Nous calculons l’écoulement et la déformation élastique d’une lame de smectique A idéal comprimée
sinusoidalement entre deux membranes parallèles
auxcouches. A basse fréquence, la perméation apparaît dans
les deux couches limites prévues précédemment. A haute fréquence la perméation disparaît. L’écoulement est
unepure 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
aurégime élastique de basse fréquence. Une tension de surface finie doit supprimer les couches limites de perméation à
basse fréquence.
Abstract.
2014We compute the coupled flow and elastic distortion of
anideal 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
apure hydroelastic distortion, with the smectic layers
«frozen » inside the matter. The elastic part of the mechanical impedance of
the smectic slab undergoes
arelaxation, 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
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 :
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,
uis 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.
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
zerofrequency normalized distortion u/b. 1 is the permeation boundary layer thickness for
mi =0. Only
onehalf of the profile 0
zd
is represented, the other part ( - d
z0) 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
aconstant curvature at
zerofrequency 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
1i.e. for (WT)p ~
pmqx. qx At this frequency the distortion profile is already
Fig. 4.
-Normalized profiles for the
massvelocity V and the layer velocity û, for
mi -mqx when permeation is at
amaximum.
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
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
versusthe
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-
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
Ziwô 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
~