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Submitted on 1 Jan 1988

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S2 analysis of cholesteric elasticity

F. Lequeux

To cite this version:

F. Lequeux. S2 analysis of cholesteric elasticity. Journal de Physique, 1988, 49 (6), pp.967-974.

�10.1051/jphys:01988004906096700�. �jpa-00210784�

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S2 analysis of cholesteric elasticity

F. Lequeux

Laboratoire de Physique des Solides, Bât. 510, Centre d’Orsay, 91405 Orsay Cedex, France (Reçu le 30 novembre 1987, accepté sous forme définitive le 8 fgvrier 1988)

Résumé. 2014 On montre que dans le cas d’une élasticité isotrope (K1 = K2

=

K3), les structures cholestériques à

une dimension ont un analogue mécanisme simple : elles sont représentées par le mouvement d’une charge glissant sans frottement en présence d’un champ magnétique uniforme sur la sphère image S2. Etendant cette approche à des structures à plusieurs dimensions et écrivant une règle de flux, nous présentons sommairement trois instabilités élastiques analysées sur S2.

Abstract.

2014

We show that, in the case of isotropic elasticity, the one dimensional cholesteric structures can be

simply integrated : on the image sphere S2, they can be pictured as the motion of a charge gliding without

friction in the presence of a constant magnetic field. We can write a flux law, even for a multidimensional cholesteric field. We present briefly how this representation gives an interesting approach of three elastic instabilities.

Classification

Physics Abstracts

61.30

1. Introduction.

Cholesteric liquid cristals are uniaxial liquid crystals

and can be described, from an elastical point of view, as a field n (r ) from the real space R3 to the space S2 which is the unit sphere of R3 (if one takes n I =1). The equivalence between n and - n can be taken into account by using P2 instead of S2. Since

we do not consider defects but only continuous media, we prefer to use S2.

The free energy of a cholesteric has been given by

Frank [1] :

(where q is the natural inverse pitch).

This energy is constituted by three terms which

measure splay (K1 ), twist (K2) and bend (K3 ) [2]. In

the special case where the three constants Kl, K2, K3 are equal, the energy is :

or

In this case, the energy becomes highly symmetric

and numerous studies have been done on this

isotropic elasticity, the latest developments being

studies of those systems in the curved space

S3 [3].

The classical representation of this energy is in terms of splay, twist and bend.

In the special case q

=

0 (i. e. nematic) Thurston [4] has proposed a representation of the energy. We extend his approach to cholesterics. We limit our-

selves to isotropic elasticity. Although it could easily

be extended to anisotropic elasticity, it would be

cumbersome and of no peculiar interest.

Let us explain the basis of our representation.

One can represent the field on the image space

S2 as follows : one can draw, on S2, the curve (n (r )) image of the R3-curve (r). In fact this appears to be interesting when we take, for the R3-curves (r), lines parallel to one of the three axes of a

classical reference frame Ox, y, z and we limit ourselves to this case.

We limit ourselves to the problem of a static

cholesteric in a rigid box with a strong anchoring, (i.e. where the field n is given on the faces of the

box), and without external fields. Consequently, we

will never take surface energy terms into account.

After explaining our method, we will show on some examples how this method gives (we hope) a

clear analysis of some elastical problems.

Article published online by EDP Sciences and available at http://dx.doi.org/10.1051/jphys:01988004906096700

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968

Our method gives only a visualization of the energy, which seems to us to be very useful. It allows

us to do some approximations or to guess some textures without a complete classical calculation.

This is important in this problem where there is in fact only one dimensionless parameter qL (where

L is the size of the box).

Our method gives neither a new method for minimizing the Frank energy nor a new mathematical formulation but only make visual the energy of some

textures.

We will see that this visualization of the energy

can give an interesting approach and discussion of

some simple problems. In part 2, 3, 4, 5, we explain

the basis of our method. In 5, we use it in some very

simple cases.

2. Method.

As said previously, we take Kl = K2 = K3.

Let us first take a one dimensional-field, i.e. a field depending only on z. We take the orthonormal frame (0, x, y, z) with the coordinates (x, y, z). On S2, a curve (n (z ) ) is defined with z as a parameter.

We call velocity on the curve an , making an

az

analogy between z and time.

The curve on S2 is described with a velocity equal

to the gradient aznj.

Let us take S2 as the unit sphere of R3 with the

usual orthonormal frame ex, ey, ez. Of course, we take our frame (x, y, z) of the real space equal to our

frame (ex, ey, ez) of the space image, but we take

different notations for real and image space in order to avoid some confusions.

On S2, we can express splay, twist and bend of a one dimensional field n(i ).

Multidimensional field.

If the field depends on d coordinates, the image

on S2 is a mapping of a part of S2 constituted by

d sets of curves, each one being a one-dimensional

curve with the d-1 other coordinates as par- ameters. For example, for two-dimensional field

(x and z for instance) we have two sets of curves :

and

In this case the coupling between the two sets of

curves is complex because implicit (one set of curves

can be deduced of the other). Nevertheless, we shall

see that two dimensional structures can be interpre-

ted on S2.

3. Energy of a curve n (z).

The density of the energy of a structure can be written (after (1)) :

and can be understood as the sum of the energies

associated with the curves (in x, y or z). This

associated energy is :

(respectively x and y).

Let us consider the one-dimensional problem. The

energy is the sum of a kinetic energy, (the square of the velocity), and a kinetic moment of the moving point n about the axis ez. The trajectory can easily be integrated by minimizing the free energy F.

4. One dimensional problem, mechanical analogy.

A material point P of mass m and charge e, moving

without friction on S2, in the presence of a magnetic

field B, has a Lagrangian L equal to (6) :

We can make the analogy

And the Lagrangian of P is equivalent to the local

energy of the field n (z ). Equilibrium configuration is

a minimum of the integral of F, and consequently, a

minimum of the action of the point P ; the curve n(z) is the trajectory of a point (m, e ) moving on S2, without friction, in a magnetic field B = -2e,-A

with the relation qm

=

eA.

The velocity of the point P is constant in the

modulus (because the magnetic force does not work), so the value an is constant in the space.

az

We take n in spherical coordinates :

The kinetic energy is constant :

(4)

The Lagrangian is :

where

°

designates the z (or time) derivation.

.

Then the equations of motion are :

One derives :

where a is a constant.

The trajectory is restricted in a zone where 0 is such that

The integrals are

and

In the case where the trajectory goes through the point ez (or - ez), we have a

=

0 and simply :

which is an elliptic integral of the first kind.

5. Flux law.

It is well know, that the trajectory of a particle moving without friction on a surface is the path of a perfect elastic stretched over the same surface. In order to extend the analogy to our system, we just

have to add the magnetic term, which appears to be

a flux term.

So, we can build this other mechanical analogy :

The energy is equal to the energy of an elastic loop (with a vanishing length at rest) plus the flux of ez through the loop, with the adequate coefficients.

If f is the length of the loop

L, the reciprocal length in R3 and CP the flux of e, through the loop

the total free energy is :

This formula is valid for any closed loop n, and for

an open loop, the flux contains an arbitrary additive

constant.

Note that for any dimensional structure one has :

where S is the surface vector of the surface leaning

on n (i ).

Even if the velocity is not constant, the value of

the 2 qn . curl n term for a curve n (i ) is -4qOi, where 0 i is the flux of the vector ei through the

curve n (i ).

In general the velocity modulus is not constant

ðn ) 2

and one must integrate ( an ai 2 over all the

d set of curves.

The total energy is then

where the 0 i are the fluxes of ei through n(i ).

The coupling between the x, y and z directions is

implicit and in fact for 3 dimensional problems, it is quite difficult to minimize the energy of the field.

We will now discuss some particular cases. The boundary conditions are expressed by imposed points or curves at the extremities of the sets of the n curves.

Remark : The lowest energy situation, for an

infinite continuous medium, is the classical one- dimensional planar geometry :

described on S2 by the great circle n (z ) normal to the

direction Oz (the equator) swept many times, the velocity being equal to q, as one can easily verify :

on S2, it is the geometry which maximizes the

(negative) flux and the energy (given by Eq. (3)) imposes the velocity q.

6. Study of some simple configurations.

We now present some examples where our analysis

raises an interesting discussion.

6.1 TRANSITION CONSTANT FIELD/ONE DIMENSION- AL FIELD IN A HOMEOTROPIC GEOMETRY (OR TRANSLATIONAL INVARIANT CHOLESTERIC OR

TIC).

-

Let a cholesteric sample be located between two parallel planes (in z

=

0 and z

=

d) where the boundary condition is n

=

ez, (homeotropic anchor- ing). One can observe [7], by decreasing the natural

pitch 2 7r/q (by heating for example) that the initial

situation n

=

ez, at a certain threshold begins to

modulate along the Oz axis. On S2, the trajectory

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970

n(z), initially reduced to the point ez then is described by the relation (Eq. (2)). n(z) is then a

lobe closed on the point ez of S2 (see Fig. 1).

Fig. 1.

-

One dimensional structure between two parallel planes with n normal to the planes on the boundary. The

structure is a point on S2 for large pitch (n is constant) and develops into a lobe (while q increases) increasing its flux

about e.. On the bottom the classical representation of the

initial and the TIC structures.

We will first describe what happens at the

threshold between n constant field and n (z) rep- resented by a lobe on S2.

In order to get the smaller order (in size of the

lobe) terms in energy, we will approximate the sphere near ez by its tangent plane (z = 1 in the image space). In this case, it is evident that the n(z) are circles passing through ez (on the plane,

circles have a maximum ratio flux/perimeter). The

energy is then, (using Eq. (3)) :

where r is the radius of the circle n (z ).

For - ; , F is minimum for r = 0 and for

q >- ; , F is minimum for r - oo.

The threshold is then q - ’T d

We can verify that this gives the good r2 term for

F, and that when Eo - 0, equation 2 becomes :

The angle between ez and the circle gives an r4 contribution to the flux.

It is evident that the curvature of S2 (which

decreases the flux about the plane z = 1) stabilises

the lobes n(z ). The r4 terms in F are negative

because flux and the ratio flux/perimeter are both energetically unfavourable on S2 (about on z = 1).

Consequently we have on S2

We have a second order i la Landau transition : i. e, the lobe develops while increasing q for

q >- -i . The classical representation of n on the real

space is drawn in figure 1.

6.2 MODULATION OF THIS STRUCTURE ALONG Ox

(DOUBLE TWISTED OR DT).

-

The latter structure (the TIC), at a certain amplitude, presents another modulation along the Ox axis. Without taking details

into account, we can just explain it.

The initial lobe no(z), previously described (Eq. (2)), reaches (by increasing q) a zone near the equator and then develops into a two dimensional

configuration, the structure increasing its flux about the Ox direction.

Let us explain how it develops.

Curves at z

=

cst. are initially points, and spread

out in some small loops centered on their initial position, in order to increase their flux about Ox.

The more the loops are normal to Ox, the bigger they become, and their size vanishes for z

=

0 and

z

=

d (i.e. at the point ez) in order to satisfy the boundary conditions.

The curves for x constant can be deduced and are

similar to the initial lobe (see Fig. 2).

This complex situation exhibits a double-twist : there is twist about Oz and about Ox. We limit ourselves to this simple approach, but will develop a

more precise analysis in a future publication. We only present a picture of the two instabilities in

figure 3 (courtesy of P. Oswald).

6.3 ZERO LAYER CHOLESTERIC DILATION INSTA- BILITY.

-

Let us now consider a cholesteric between two parallel planes z

=

0 and z

=

d, with n on each plane equal to ex. (This planar anchoring, like the homeotropic anchoring, can be imposed by adequate treatments on glasses).

For small q (i.e. large pitches), n is constant

between the plane and is represented by the point

ex on S2.

Let us now try to estimate what happens while

increasing q.

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Fig. 2.

-

The previous lobe n(z) develops in a 2-

dimensional structure, creating small loops with flux about Ox (on the bottom the R3 representation).

In order to minimize its energy, the system will increase its flux. Near ex, the only flux a lobe can get is a flux about ex (the surface at ex contains

ey and ez). Hence the structure will develop n (x )

lobes.

For z

=

0 and z

=

d, the n (x ) lobes must be the point ex itself.

We can take n (x ) as circles centered on ex and of a

radius r(z ) with r(z

=

0)

=

r(z

=

d )

=

0 in order to

respect the anchoring.

Near the threshold, we can approximate (as in 6.1) S2 by the plane x = 1, and we take

r = ro sin 7 . In this case it is easy to prove that this is the lowest energy situation.

The field on S2 and on R3 is represented in figure 4. If the field is written n

=

cos cpex + sin cp sin Oey + cos Oez, we have :

and

The energy is written (in mean density using Eq. (3))

where 2 7T / k is the length in the real space along Ox

to sweep one time the n (x ) circles. (k is the wave

vector on R3).

As shown in figure 4, the n (z ) curves are arcs of great circles swept from ex and back to ex.

The structure can develop for a 2 F a2F ar2 0 i.e.

which gives the threshold (for a free value of k)

Remark : k has a definit sign, i.e., the n (x ) are swept

in the right direction. This will be developed in the

Fig. 3.

-

Picture of the TIC and DT instabilities : the black zone (on the left) is the n

=

constant zone ; the white zone

(on the middle) is the TIC zone ; the modulated zone is the DT zone. Optical microscopy, crossed polarizers, courtesy of

P.. Oswald.

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972

Fig. 4.

-

Dilation instability of a zero layer cholesteric.

Above the representation and on the bottom the classical

representation. The initial situation is n

=

ex everywhere.

case of a many-layer dilation instability. One can verify using Euler’s equations, that at the threshold,

our model is good. Experiments are in agreement and will be discussed in another publication.

6.4 ANALYSIS OF THE UNDULATION DILATION OF A PLANAR CHOLESTERIC.

-

Let us now consider a

cholesteric laying between two parallel planes

z

=

0 and z = d with n, on each plane, constant and

contained in the plane (planar anchoring). The

initial situation is the natural helical situation of

cholesterics, with nc layers :

This is pictured on S2 by the equator swept in n,, times.

When one dilates this system (or decreases the pitch 2 7T /q), one observes an undulation of the

layers [8]. Usually the analysis uses an approximate layered energy, known as coarse-grained energy [9].

We now present another analysis, based on S2 configurations.

Let the system develop into a two dimensional structure n (x, z ). One can easily prove that in dilation the n (x = cst., z ) curves cannot decrease (with a small perturbation Sn(z)) their energy around their initial equatorial configuration no (z )

because their (negative) fluxes are maxima (for

instance one can verify that

for any 5 n, with Fz equal to the energy of the

n(z) at x

=

xo curves).

Thus the only term which can decrease is the flux term about ex.

We choose Ox to be parallel to n(z

=

d/2) (for

symmetry reasons), and look for the simplest struc-

ture decreasing the energy. We call no the initial one

dimensional structure.

We must create a flux about Ox i.e. little loops n (x, z

=

zo ) near the points of S2, ex and - ex. The

loops have the symmetry of the system. They must

be ellipses of axes ez and erp

=

no A ez. Let a and f3 be the radii of the ellipses along erp and ez. The flux must have the same sign around

ex and - ex, i.e., the orientation of the n(x) must be

the same near ex and - ex. But since efP

=

ey at

ex, and efP = - ey at - ex, we must change the sign of

« or B. The symmetry n, - n of the cholesteric

implies that we take « and - f3 in - ex for

« and f3 in ex.

This imposes that /3 must be modulated by the

cosine ex. no.

Moreover, a and B must vanish for z

=

0 and

z

=

d (in order to satisfy the anchoring), and we can

write that :

,

and

The only approximation of this construction is that in reality the cos 7rz/d and the no - ex modulations

are coupled and resonate (as a more precise analysis

will show in a forthcoming publication, but for a many-layer system, this effect is not important). The

modulation is given by the perturbation vector

Bn ;

and is drawn in figure 5.

The energy can be calculated directly on S2 by (Eq. (4)), or by the classical Frank energy (Eq. (1))

without forgetting the condition n + Sn I = 1 at the

second order in a and 8.

One easily finds that the variation of energy due to Sn is :

2 7T

where t

=

n, - 2 7r is the twist of the initial planar

structure.

Minimizing this quadratic form in a and f3 (we

can for instance write that the determinant of the

quadratic form 6F (a, B ) vanishes at the threshold),

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Fig. 5.

-

Dilation undulation representation on S2 : initially, the situation is described by the equator. Little ellipses develop near ex and - ex with the same sign about

Ox. This picture must be modulated in amplitude from

z

=

0 to z = d in order to respect the boundary conditions.

one gets for the threshold :

This analysis is more precise than the coarse grain

calculation. It gives the second order for k2 in

7T/d:

and the first order term which is in general given

with the wrong coefficient in the classical analysis. In addition, we show that the ellipses, when q = t, are incompatible with the layer conservation hypothesis

« = t/k which is the basic concept of the layered energy (as d becomes very large, q - t -+ 0

and f- t/k ; for many layered systems the 18

hypothesis of layer conservation is valid).

Here we do not present the complete analysis of

the dilation instability, because it is not our present aim, but we will discuss it later in a forthcoming publication. This approach, which is not a complete

solution of the problem, is nevertheless interesting

and more precise than the existing analysis.

7. Conclusion.

We have shown that the cholesteric structure with an

isotropic elasticity, when considered as a mapping of S2, can be simply interpreted from an energetic point

of view.

Each image of a straight line of the flat space is a

curve on S2. We can associate to each curve an

energy which is the sum of a kinetic energy and a flux.

We hope that our S2 method of energy analysis

can help to get a better understanding of the

cholesteric elasticity.

We are fully aware of the limits of our method,

and in particular of the fact that this method does not clearly bring new mathematical resolutions of the cholesteric elasticity, but we are convinced that it

can be simple and useful for a priori approaches, and approximations.

The anisotropic energy is cumbersome because the surface and the magnetic field of the mechanical

analogous are very complex, but it is quite simple to transpose isotropic results in an anisotropic analysis.

We hope too that we will be able to initiate new

interest in cholesteric elastical instability.

Acknowledgments.

We are greatly indebted to M. Kleman who has

suggested and discussed this work and we thank P.

Oswald for discussions about the T.I.C. and D.T.

experimental observations.

References

[1] FRANK, F. C., Discuss. Faraday Soc. 25 (1958) 19 ; NERHING, J., SAUPE, A., J. Chem. Phys. 54-1 (1971)

337.

[2] See for example DE GENNES, P. G., The physics of liquid crystals (Clarendon Press, Oxford) 1974.

[3] From SETHNA, J. P., WRIGHT, C. D., MERMIN, N. D., Phys. Rev. Lett. 51 (1983) 467 to PANSU, B., DANDOLOFF, R., DUBOIS-VIOLETTE, E., J.

Phys. France 48 (1987) 297.

[4] THURSTON, R. N., ALMGREN, F. J., J. Phys. France

42 (1981) 413 ;

THURSTON, R. N., J. Phys. France 42 (1981) 418.

[5] In the case of anisotropic energy, one must separate the three components (in K1, K2 and K3) of the gradient and multiply them by the convenient coefficient. This can be solved by taking a complex surface 03B6 instead of S2 in order to have

(~z)03B6 ~ F - 2 qn · curl n (see [4]).

[6] LANDAU, L., LIFSHITZ, I., Field Theory (Mir Mos- cow).

[7] OSWALD, P., BECHHOEFER, J., LIBCHABER, A., LEQUEUX, F., Phys. Rev. A 36 12 (1987) 5832 ; LEQUEUX, F., OSWALD, P., to be published.

PRESS, M. J., ARROTT, A. S., J. Phys. France 37

(1976) 387.

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974

[8] CLARK, N. A., MEYER, R. B., Appl. Phys. Lett. 22 (1973) 473 ;

DELAYE, M., RIBOTTA, R., DURAND, G., Phys.

Lett. A 44 (1973) 139.

[9] DE GENNES, P. G., The physics of liquid crystals (Clarendon Press, Oxford) chapitre 6, p. 245

(1974) ; (see also LUBENSKI, T. S., Phys. Rev. A

6 (1972) 452).

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