Seyed Reza Seyednejad*a and
Miha Ravnikab
aFaculty of Mathematics and Physics, University of Ljubljana, Jadranska 19, 1000 Ljubljana, Slovenia. E-mail: seyed-reza.seyednejad@fmf.uni-lj.si
bDepartment of Condensed Matter Physics, Jožef Stefan Institute, Jamova 39, 1000 Ljubljana, Slovenia
First published on 6th January 2025
We demonstrate the generation of diverse material flow regimes in nematic liquid cells as driven by time-variable active surface anchoring, including no-net flow, oscillatory flow, steady flow, and pulsating flow. Specifically, we numerically simulate a passive nematic fluid inside a cell bounded with two flat solid boundaries at which the time-dependent anchoring is applied with the dynamically variable surface anchoring easy axis. We show that different flow regimes emerge as the result of different anchoring driving directions (i.e. co-rotating or counter-rotating) and relative phase of anchoring driving. The flow magnitude is tunable by cell thickness and anchoring driving frequency. More generally, this work aims towards possible applications of responsive time-variable surfaces, including photonics or synthetic active matter.
In addition to known mechanisms for pushing fluids out of equilibrium, such as electrophoresis,18 thermophoresis,19,20 electro-osmosis,21 electrowetting,22 optical fields,23 and acoustic waves,24 the dynamics and flow in nematic environments can be driven by internal activity, caused by chemical ingredients25,26 and biological agents.27,28 The inherently out-of-equilibrium liquid crystal systems are active nematics,29,30 which show peculiar topological and elastic properties of such tunable fluids,31–37 where the confinement geometry38 and the channel size39 are of basic importance.
In intrinsically passive NLCs, the flow can be a result of the constant entry of elastic distortions generated by a rotating external field.9 Elastic distortions can also be brought into the NLC bulk by remotely rotating a solid colloid inside the NLC that makes the colloid swim,40 or by oscillating hydrostatic pressure, making spherical bubbles pulsate and swim in the bulk.41 Moreover, flow in the micro-channel networks can be modulated and guided by using surface anchoring profiles, that are controlled by optical techniques.42
Our aim here is to drive flow in a passive NLC channel by generating elastic distortions through dynamic surface anchoring. NLC molecular alignments on the interfaces regularly are categorized as planar (parallel), homeotropic (perpendicular), or conical (tilted), which can be experimentally achieved by various physical and chemical techniques.43,44 Polymeric thin film surfaces and monolayer coverage of surfactants are used to guarantee the homeotropic or planar anchorings on different types of interfaces.45–47 Moreover, in recent years, the photo-patterning technique has made it possible to design every arbitrary patterns of in-plane surface anchorings by using electromagnetic polarized light beams on a layer of photosensitive dyes.48–50
Here we demonstrate the generation of different material flow regimes as controlled by rotating surface anchoring easy directions in nematic liquid crystal cells. We explore the role of co-rotating and counter-rotating anchoring at the two bounding surfaces, as well as the role of the relative phase. Different flow regimes are demonstrated, including no-net flow, oscillatory flow, steady flow, and pulsating flow.
Time evolution of the tensor order parameter and the flow field of the NLC are described using the Beris–Edwards approach,51,52
= ΓH + S, | (1) |
ρ[∂tvi + (vj∂j)vi] = ∂jσij, | (2) |
∂ivi = 0, | (3) |
We solve the Beris–Edwards equations using hybrid lattice Boltzmann algorithm.54,55 For that purpose, we consider a 100 × 20 × H grid box, with the the grid size Δx = 1.5ξN, where the cell height H varies between 50–200Δx. Periodic boundary conditions are considered in x and y directions.
As shown in Fig. 1, on the top and bottom cell surfaces, the surface anchoring easy axis 0(t) = (sinθ, 0, cosθ) is assumed to rotate in the xz plane from planar to homeotropic to planar and so on, with constant angular velocities ω1 and ω2 on the bottom and top walls, respectively.
θ1(t) = ω1t, θ2(t) = ω2t + ΔϕA, | (4) |
(5) |
Fig. 2 No net flow and oscillating flow regimes generated by co-rotating time-varying active surface anchorings. Snapshots of the director and flow fields when ω2 = ω1 = ω0, with anchoring phase differences ΔϕA = 0 in (a)–(c) (first row), and ΔϕA = π/2 in (e)–(g) (second row). Front and side views are displayed in the first and second columns. Anchoring angular velocity vectors ω1 and ω2 are shown with red arrows at the bottom and top surfaces. (c) and (g) Show the local flow field at the same time as in (a),(b), (e) and (f), respectively. (d) and (h) Show how the velocity field in the channel changes in one-period duration Tp; maximum Ericksen number is Er ≈ 0.2. (i) Flow flux through a plane cross-section perpendicular to the x axis in the middle of the system as a function of time. The gray box shows the steady state phase of the system, in which the time average of the flux is calculated. The non-zero Fourier coefficients are calculated as a2 = 0.70 and ϕ2 = −0.52π. The inset shows a close view of ΔϕA = 0 case where the fluctuations order of magnitude is 10−4. (see also Videos S1 and S2, ESI†). |
The director field mostly remains in the xz plane near the top and bottom surfaces and rotates around the y axis. By going farther into the bulk, the director field splays out of the plane, and then in the middle of the bulk, it shows a rotational motion on a cone around the y axis with an easy angle ψ, which is a function of z and has a minimum at z = H/2. The escape of the director field toward the y axis helps the system avoid the growth of elastic distortions due to director winding.
With ΔϕA = 0, the flow velocity field as shown in Fig. 2(a), is symmetric as well. Here the flow is in the opposite directions in the top and bottom halves of the cell, where the flow is mostly in the left direction at the upper part and it is in the right direction in the lower part of the cell. Therefore, the overall flow flux throughout any yz cross-section of the cell is always zero, as shown in Fig. 2(i). Despite no (time-averaged) net flow, the local flow velocity vector oscillates in time, between its minimum and maximum. Somewhat differently, for ΔϕA = π/2, the vector field shows spatially asymmetric shape, as the flow vector field locally oscillates at upper and lower parts with a π/2 phase difference, which gives rise to an instantaneously non-zero oscillating back and forth flow flux with zero time average, as shown in Fig. 2(i). The flow flux data follows an effective cosine function with angular velocity 2ω1; i.e. note, twice as fast as the director orientation near the walls, which is the result of nematic head-to-tail symmetry ( ≡ −). Namely, the nematic field close to the surfaces as the source of flow in the bulk returns to its initial orientation already after half a round rotation (θ → θ + π) and drives the bulk fluid the same way as before (see Videos S1 and S2, ESI†). As a result, the flow velocity field has a period of half a round of the surface anchoring rotation.
In order to observe the net flux, we choose different anchoring angular velocities on the top and bottom surfaces. In Fig. 3, we show an example where the director on the two boundaries rotate with the same angular velocity but in opposite directions, ω2 = −ω1. The director field behavior is mostly similar to the symmetric case of Fig. 2, except that it is mirror-symmetric as the bending directions are the same at the upper and lower halves of the cell. By using ΔϕA = 0, and counter-rotating anchoring angular velocities, as shown in Fig. 3(a)–(d), effectively, the same synchronized elastic distortions emerge and importantly, with the same direction of the backflow generated material flow driving. The local flow field oscillates all over the bulk, and the magnitude is always largest in the middle, which results a sinusoidal profile of the flow flux which is shown in Fig. 3(i). For ΔϕA = 0, the flow flux has the form of the second term of Fourier series with the angular velocity 2ω1 in accordance with Fig. 3(i). For ΔϕA ≠ 0 the flux time profile becomes more complicated as the fourth Fourier terms appear. The phase difference does not affect the frequency of the flow flux or its time average. But it does decrease the magnitude of the flow beats. Consequently, the phase difference between the time-variable surface anchorings can be used as a control parameter for tuning the flow smoothness and the overall profile.
Fig. 3 Steady flow regimes driven by counter-rotating time-varying active anchoring rotations. Snapshots of the director and flow fields for ω2 = −ω1 = −ω0, with anchoring phase differences ΔϕA = 0 in (a)–(c) (first row), and ΔϕA = π/2 in (e)–(g) (second row). Anchoring angular velocity vectors ω1 and ω2 are shown with red arrows at the bottom and top surfaces. (c) and (g) Show the local flow field at the same time as in (a), (b), (e) and (f), respectively. (d) and (h) Show how the velocity field in the channel changes in one-period duration Tp, where the maximum Ericksen number is Er ≈ 0.3. (i) Flow flux through a yz plane cross-section as a function of time. The non-zero Fourier coefficients calculated as a0 = 1.00, a2 = 0.68, ϕ2 = 0.53π, a4 = 0.04 and ϕ4 = 0.47π for ΔϕA = 0, and a0 = 1.00, a2 = 0.03, ϕ2 = −0.68π, a4 = 0.03 and ϕ4 = 0.50π for ΔϕA = π/2. (see also Videos S3 and S4, ESI†). |
Fig. 4 shows the adjustment of the flow profiles and the flow magnitude taking different (counter-rotating) angular velocities of the surface anchoring easy axes on the two surfaces. Fig. 4(a)–(d) show that the flow velocity oscillates with a larger magnitude near the top surface, where the anchoring rotation is faster, which notably, also allows the flow to steer to the top or bottom of the channel. Moreover, by increasing ω2 the flow amplitude and also the flux average increases, as shown in Fig. 4(e)–(h). The overall period of the system is still determined by the slower surface anchoring on the bottom, whereas the faster rotation at the top leads to the flux time behavior as higher order terms in the Fourier series, with exact values of the coefficients determined by the anchoring phase difference ΔϕA.
In Fig. 5 we have studied the case of static surface anchoring on the top surface, ω2 = 0, while we kept the dynamic anchoring on the bottom, ω1 = ω0. Specifically, the standard homeotropic and planar anchorings are considered at the static top surface. Fig. 5(d) and (h)–(j) show that this static-dynamic time-variable anchoring creates a pulsating flow, where the flux periodically stops or even draws a little bit back at specific moments and then drives on again. The next significant difference here appears in the leading frequency of the flow (and flow flux), which is found to be the same as the anchoring frequency ω1 (and not 2ω1 as before with two dynamic surfaces). The fixed anchoring in both homeotropic and planar conditions does not allow the system to recover its initial state when the anchoring direction rotates by only half a turn (i.e. by π). See Videos S5 and S6 (ESI†). Therefore, after a π rotation of the director on the bottom surface, the director field undergoes different configurations, resulting in different backflow coupling and thus different material flow. We note that the 2ω1 frequency is still present in the Fourier series of the flow flux as the second-order term. The time average of the flux is expectedly different in homeotropic and planar anchorings due to the different bulk distortions and different backflow effects.
Fig. 5 Pulsating flow regimes driven by single-surface time-variable active anchoring. Snapshots of the director and flow field when the anchoring is fixed on the top surface ω2 = 0 and ω1 = ω0 on the bottom. For the static top surface, homeotropic (a)–(d) and non-degenerate planar (e)–(h) is assumed; corresponding flow profiles are shown in (d) and (h) respectively as functions of time, where the maximum Ericksen number is Er ≈ 0.3. Flow flux as a function of time when homeotropic (i) and planar (j) anchorings on the static surface with Fourier coefficients a0 = 0.39, a1 = 0.18, ϕ1 = −0.28π, a2 = 0.33, ϕ2 = −0.48π, a3 = 0.07, ϕ3 = −0.20π, a4 = 0.03, ϕ4 = 0.28π for (i), and a0 = 0.50, a1 = 0.18, ϕ1 = 0.40π, a2 = 0.30, ϕ2 = −0.50π, a3 = 0.06, ϕ3 = −0.82π, a4 = 0.02, ϕ4 = 0.70π for (j). (see also videos S5 and S6, ESI†). |
Fig. 6(a) and (b) show the flow flux as dependent on the cell thickness H and the magnitude of anchoring angular velocity when ω2 = −ω1. The net flux increases with the anchoring angular speed for small ω1. For large ω1, the backflow effect becomes less efficient since the high speed of the anchoring overcomes the relaxation time of the nematic fluid, and as a result, the net flux approaches a saturated level. The net flux also increases by the cell thickness H, as shown in Fig. 6(a). The inset in Fig. 6(a) shows that the cell thickness has some effect on the average flow velocity across the channel bulk, calculated as 〈vx〉 = a0/A, where a0 is the zero-order Fourier flow flux coefficient or the time average of the flow flux and A is defined as the area of the cell cross-section. Here, note that although the flow flux magnitude increases with the cell thickness, its qualitative behavior does not change much, and even the average flow velocity in the inset of Fig. 6(a) varies only weakly with the width of the channel. This can be a result of the fact that the considered nematic orientational profiles are effectively scalable as only conditioned by the director's elasticity and not nematic scalar order parameter.
In conclusion, we demonstrate the generation of material flow in flat cell geometry of nematic complex fluids as driven by time-variable active surface anchoring. Our results show that the co-rotating or counter-rotating anchorings lead to different flow regimes. If we look at the results shown in Fig. 2–5, effectively, we notice that the local flow direction is always roughly determined by the angular velocity vector of the nearby surface anchoring through the right-hand law. As a result, for co-rotating anchorings where the angular velocity has the same magnitude and direction, the top and bottom surfaces effectively cancel out each other's effect and result in a zero time-averaged net flux, while non-zero oscillating flux (with zero time-average) can emerge by imposing a phase shift between the angles of rotation of the two surfaces. Differently, for counter-rotating time-variable active surface anchoring, when the anchorings on the top and bottom rotate with the same angular velocity but in opposite directions, effectively, both active surfaces work up together which leads to a directional net material flow. Moreover, by choosing different rotation speeds at the top and bottom, the flow profile can be steered towards the top or bottom surface as a larger flow is realized near the wall with faster anchoring rotation, which can be a control parameter for flow steering. In parallel, we show that the phase shift ΔϕA can be used to tune the flow profiles as well as the exact flow flux time dependence. Fourier analysis of the flow flux of co-rotating and counter-rotating surface anchorings shows that only even Fourier terms contribute to the flow flux, and as a result, the overall frequency of the flow flux is twice as large as the smallest anchoring frequency. This constraint changes when one of the surfaces is fixed and the other is rotating, where both odd and even terms emerge in the flow flux. Pulsating flow flux is a characteristic behavior of this static-dynamic time-variable surface anchoring regime, where the dynamic surface anchoring is applied only on one side. In our simulations, the Ericksen number varies between less than 0.1 for thin layers with small rotation angular velocities and 0.6 for thicker layers with faster anchoring rotations. This number is comparable to a typical maximum velocity of v = 6 μm s−1 in experiment69 and a typical cell thickness of H = 10 μm, with the same rotational viscosity and elastic constant used in this article (see Section 2). We do not see any topological defects in our simulations in the steady state as shown in Fig. 2–5. We believe there are two reasons for the absence of the defects here: (i) simple 2D-infinite plane geometry for the boundaries and (ii) uniform anchoring rotation with no dependency on position. Of course, by choosing more complicated geometries or scenarios for the dynamic surface anchoring driving, the emergence of topological defects and consequently, more complicated flow fields is expected.
In this work, we focused on the ability and possible modalities of the surfaces to drive and control the microfluidic flow of complex nematic fluids which would broaden the options of pumping NLC flow in the experiment as a complement to other propositions for driving NLC flow in the bulk for example by using electric or optical fields.9 For example, the distinct difference of this work is that the flow driving does not depend on any material dielectric properties (e.g. refractive indices, dielectric constant, etc.) and could be applied also to zero-birefringence nematic fluids. Secondly, the concept of flow driving through time-variable surface anchoring could – by using different surface anchoring driving mechanisms – be transferable to other nematic material length scales such as colloidal liquid crystals which could be much more challenging with optical (size) or electric field effect (homogeneity of the field). Finally, the effectively surface-imposed dynamic control could also be transferred to different – for example, active-materials (i.e. beyond molecular liquid crystals) where bulk control of the materials is currently much less established or available. More generally, this work contributes to the development of novel material driving routes in topological soft matter and synthetic active materials.
Footnote |
† Electronic supplementary information (ESI) available. See DOI: https://doi.org/10.1039/d4sm00924j |
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