Microchannel flow of a shear-banding fluid: enhanced confinement effect and interfacial instability

Microchannel flow of a shear-banding fluid: enhanced confinement effect and interfacial instability

P. Nghe, S. M. Fielding, P. Tabeling, A. Ajdari Laboratoire Microfluidique, MEMS et Nanostructures, UMR Gulliver CNRS-ESPCI 7083 Department of Physics, University of Durham, Science Laboratories, South Road, Durham. DH1 3LE Laboratoire Physico-Chimie Theorique, UMR Gulliver CNRS-ESPCI 7083
July 26, 2019
Abstract

Using a micro particle imaging velocity technique, we resolve for the first time the three dimensionnal structure of wormlike shear banding flows in straight microchannels. The study revealed two effects, which should be generic for shear banding flows: the first is a strong amplification of the confinement induced by the edge of the channel, the second is an instability of the interface between the shear bands. A detailed quantitative comparison of our experimental measurements with a theoretical study of the diffusive Johnson Segalman model leads to excellent agreement. Our study clarifies the nature of shear banding flow instabilities, and shows that, despite the challenging complexity of the situation and the uncertainty regarding their molecular structure, shear banding flows in confined geometries are amenable to quantitative modelling, a feature that opens pathways to their practical utilization.

pacs:

In many complex fluids, a strongly nonlinear coupling between flow and microstructure can trigger the onset of flow instabilities, leading to the formation of coexisting “shear bands” that support differing shear rates at a common shear stress. This model situation for out-of-equilibrium phase separation has been the focus of intense research in recent years Olmsted2008 (), with wormlike micellar surfactants the most widely studied systems Cates2006 (), both as model materials and for their widespread application in, e.g., oil recovery and personal care products. Significant progress has been achieved by imaging experimentally the local flow profile, first by NMR Britton1997 () and later by DLS Salmon2003a (), ultrasound Manneville2004 () or particle image velocimetry Masselon2008 (). In this Letter we report a significant advance in such efforts, with the first full three dimensional (3D) velocity imaging of a shear-banding fluid. We perform this in the context of pressure driven flow in a rectilinear microchannel of rectangular cross section.

Using this imaging, we report two flow phenomena. The first is a strongly enhanced confinement effect induced by the edges, that we believe may prove generic in a broad class of heterogeneous confined flows. The second is an instability of the interface between the shear bands, characterized by a downstream evolution from (near the inlet) a smoothly bowed interface between the bands, to (far downstream) a modulated interface with wavevector in the vorticity direction. Throughout, we compare our data with a theoretical study of the diffusive Johnson-Segalman (DJS) model in the same geometry. The excellent quantitative agreement we find without fitting assesses the robustness of our observations in the general context of shear-banded flows. It also suggests that the behavior of wormlike micelles in complex geometries is amenable to theoretical description at a quantitative level.

In particular, the interfacial instability we observe relates to a growing body of experiments showing complex spatio-temporal patterns in shear-banded flow, most of which have been to date in curved Couette geometry. While observations of instabilities are now quite widespread in that geometry via 1D measurements, the only previous explicit observation of a 2D modulation of the interface is in Ref.Lerouge2006 (). The theoretical understanding of this instability remains preliminary Cates2006 (), but suggestions about its origin include (i) a bulk viscoelastic Taylor-Couette-like instability originating in the strongly sheared band LARSON1990 (); and (ii) an interfacial instability triggered by the normal stress jump between the bands HINCH1992 (); Fielding2005 (). An important additional contribution of this Letter is to give evidence favouring (ii), by eliminating the cell curvature needed for (i).

Figure 1: Squares: experimental steady state flow curve Nghe2008 (). Line: theoretical curve with the DJS model for . Both are renormalized by the shear rate at the onset of shear banding, and by the value of the stress plateau . Correspondence is not expected at high shear rates (see main). Inset: sketch of the basic (1D) shear-banded flow, with the coordinate system used throughout the paper.

Experimental — The sample comprises CTAB 0.3M, NaNO 0.405M (Acros organics), which forms a semi-dilute solution of wormlike micelles. Its basic rheology was characterized in Ref. Nghe2008 (), with a stress plateau of beginning at , corresponding to a pressure gradient for the onset of shear-banding of . Our experimental setup comprises pressure driven flow in a microchannel of rectangular cross section, with dimensions with the axes of Fig. 1. The photocurable glue used in the fabrication permits high aspect ratio channels that do not deform even under pressures far in excess of those in this study Bartolo2008 (). In this work, the setup of Nghe2008 () has been substantially modified to allow full 3D velocity imaging, as follows. Fluorescent tracers of diameter are tracked at 50 Hz with a charged coupled device camera (Allied) through a 100x oil immersion objective mounted on a piezo, giving a thick focal plane that can be displaced in with resolution. Images comprise windows, the position of which is determined using a moving table (Marzhauser). These images can be divided into subimages along , resulting in correlations between images of size for . As a whole, then, velocity is mapped over the sample with spatio-temporal resolution .

Theoretical — We compare all our data with the predictions of the diffusive Johnson Segalman (DJS) model JOHNSON1977 (). This is not intended to give a microscopically faithful description of our particular fluid, but is instead the minimal phenomenological tensorial model to capture the constitutive non-monotonicity needed for banding. Its parameters are: solvent viscosity ; slip parameter ; linear modulus ; relaxation time ; and interfacial thickness normalized by the height . Values for these are guided by previous linear and nonlinear bulk rheological measurements on this system, independent of the confinement effect or instability studied here. Specifically, the non-linear flow curve of Fig. 1 suggests a ratio of high and low shear phase viscosities. Perfect correspondence is impossible because the DJS model is oversimplified in having a Newtonian high shear branch, compared to the sublinear experimental trend. For pressure drops quite close to the onset of banding, as here, we do not expect this limitation to be severe. We set , though our results are robust to variations in this quantity. We estimate , based on linear rheology. The experimental aspect ratio is ; numerically we explore . Numerical calculations are peformed initially in units in which , , , but results are usually presented by scaling stresses (or pressure drops) and shear rates by their values at the onset of banding, as in Fig. 1. Below we will demonstrate excellent quantitative agreement between theory and experiment for both the confinement effect and the interfacial instability, without any fitting specific to these phenomena.

Our numerical study considers flow driven along a channel by a constant pressure drop , assuming translational invariance of the velocity field in the main flow direction . It comprises two separate parts, to allow a cleaner understanding of the two flow phenomena seen experimentally. First we study the enhanced confinement effect by simulating channels of high aspect ratio with closed walls in and . In order to isolate this confinement effect from the interfacial instability, in this part of the study we disallow any secondary flows in the channel cross section, thus artificially switching off the instability. Our aim is thereby to capture the “basic state” seen experimentally close to the inlet, before the instability sets in downstream. The second part of our study focuses on the interfacial instability, which we now isolate from the confinement effect by switching off the latter via the use of periodic boundaries in . This work is thereby intended to approximate the flow seen experimentally in the central region of , well away from the lateral walls. In each run we evolve the code to steady state with the aim of capturing the flow pattern far downstream from the inlet , assuming that these limits correspond to each other. A stringent check of our code, adapted from a former study Fielding2007 (), is provided by comparing against a true linear stability analysis its linear regime growth dynamics of tiny amplitude perturbations to an initially flat interface.

Figure 2: (a) Experimental velocity profiles across the centreline of the cell cross section in the zone near the inlet (a typical error bar of 5% is not shown for clarity). Pressure drop (solid, dotted, dashed and dot-dashed lines) with ; (b) corresponding numerical results for the same scaled pressure drops with , , . (c) Experimental (circles) and theoretical (squares) penetration length versus scaled pressure drop. (d) Steady state greyscale snapshot of invariant shear rate for pressure drop for (aspect ratio rescaled for clarity).
Figure 3: Greyscale of the experimentally measured velocity component in the channel cross-section for , at an early downstream location before the instability has set in (a) and far downstream (b), with the fully developed pattern. (c) Corresponding numerical snapshot of the fully developed pattern with , , and periodic boundaries in . (d) Numerically computed secondary flow field for the same conditions.

Results I: basic state and confinement effect — First we explore the “basic state” that is observed across the channel cross-section in the zone far enough from the inlet for the local rheology to have attained a stationary banded state, but close enough that the interfacial instability has not set in, paying close attention to the role of the lateral walls of the channel () in breaking translational invariance in the direction. Given the high aspect ratio of our channel (), we might expect the flow profile to be almost independant except for regions close to the lateral walls. Indeed for Newtonian flows it is known that for these regions have a size of order . The new phenomenon we report is that for pressure gradients beyond the onset of shear-banding, the velocity field can vary significantly with across the entire channel cross-section.

To quantify this, we measure for each the centerline velocity profiles and a penetration length , characterising the size of the lateral regions affected by the walls. is defined by with the maximum velocity. This criterion is chosen such that for Newtonian flow for . For our shear banding fluid, profiles (Fig. 2a,b) and plotted vs. pressure gradient (Fig. 2c) compare with striking quantitative agreement between theory and experiment.

Three regimes are evident. Below the onset of banding (regime I, ) the flow is Newtonian to good approximation: profiles are invariant over a large zone around the centrepoints (Fig. 2a,b solid line) and as remarked above. At the onset of regime II a thin band of high shear rate nucleates along each of the long walls around the centrepoints , these being the locations at which the shear stress is maximum and so first exceeds the plateau (banding) stress of the bulk flow curve as is increased. These bands are seen in our numerical maps of the invariant shear rate in Fig. 2d, top. It is at this onset that the centreline profile suddenly becomes strongly bowed (Fig. 2a,b, dotted line). Reflecting this is the dramatic jump of to . As increases further the thickness of the high shear bands increases, and so does their lateral spread along the long walls (Fig. 2d, middle). At the onset of regime III, shear bands finally form along the short walls (Fig. 2d, bottom; and Fig. 2a,b long dashed and dot-dashed). then shows a downward kink into a decline to at high .

How can the large value of in regime II be understood? For a shear-banding fluid, smooth stress inhomogeneities across the channel cross section are strongly magnified in the velocity field via the nucleation of lubricating bands at the long walls. For a complete slip at these walls the system would “forget” the short dimension altogether and show parabolic Poiseuille flow across the long centreline. Simulations at fixed in regime II indeed show to increase with decreasing viscosity of the high shear band (not shown). This has important implications for a broad class of flows with stress dependent wall slip, to be explored in future.

Figure 4: Solid circles: experimental wavevector of the interfacial undulations as a function of applied pressure drop. Open squares: corresponding numerical results for the fully non-linear state computed with . The numerical wavevector is constrained by the cell length to be heavily quantised as . We therefore also show results (open circles) for the maximally unstable mode in a linear stability analysis, which does not suffer quantisation. Insert shows the experimental amplitude in units of .

Results II: instability —We describe first the steady state experimental velocity profiles at different downstream locations , for a fixed pressure drop, in a cross sectional area by containing the high shear phase together with the interface near the bottom wall. Close to the inlet (, Fig. 3a) the interface between the bands is smoothly bowed, corresponding to the basic state discussed above. In contrast, far downstream (, Fig. 3b) the interface has undulations with wavevector along the axis, with wavelength of the order of the channel height . This pattern is steady in time, and invariant with respect to further progression downstream. (At intermediate downstream locations , the instability develops via interfacial corrugations that emerge close to the lateral walls, and progressively invade towards the cell centre with increasing ; not shown.)

Such interface instabilities have already been predicted  Fielding2005 (); Fielding2007 () and observed developing in time  Lerouge2006 () in Couette geometry. Similarly to these former predictions, ongoing linear stability analysis of Poiseuille flow shows the concurrence of unstable and interfacial modes of wavelengths comparable to , over a range of parameter values. Unfortunately our measurement averages velocities over which precludes observation of wavevectors . We do, though, concentrate on exploring with our setup any instability to modulation in the vorticity direction. Thanks to our flow cell aspect ratio , there is a domain of around the middle of the channel () over which the curvature of the basic state due to the enhanced confinement effect (Fig. 3a) is negligible compared to the interface modulation for around ten wavelengths (Fig. 3b). We perform our analysis in this large aspect ratio domain that can be considered invariant in . Our corresponding numerics are therefore performed with periodic boundaries in , assuming translational invariance in . The numerical counterpart of the fully developed velocity pattern shows good correspondence (Fig. 3c).

Associated with the interfacial undulations are counter-rotatory streamwise vortices seen numerically in the secondary flow field (Fig. 3d). Experimentally, focal plane constraints make measurement of , and so direct comparison with this numerical map impossible. However an analysis of (not shown) indicates spatial modulation at an identical wavelength to that in , at least consistent with streamwise recirculation.

We analyse the developed pattern by measuring the wavelength of the interfacial undulations across a range of . We compare the size of the wavevector with linear stability analysis and full non-linear simulations of the final steady state in the DJS model (Fig. 4). For the range explored we find a decreasing wavevector, and good quantitative agreement between theory and experiment (higher values of for which saturation of wavevector is predicted numerically are unattainable in our experiments). The amplitude of the interface position undulations in (Fig.4, inset) increases with and is a few percent of the channel height.

Conclusion — Careful 3D velocimetric study of a shear banding wormlike micellar surfactant solution in microchannel flow reveals a strongly enhanced confinement effect induced by the edges, and an interfacial instability with wavevector in the vorticity direction. Striking quantitative agreement is obtained with a numerical study of the DJS model, without free parameter fitting. Given that this model is highly phenomenological, with only crude representation of the microscopic rheology, this suggests robustness of the phenomena to underlying microscopic details, hinging only on the presence of a non-monotonic constitutive curve and a normal stress jump across the interface between the shear bands. The confinement effect, here due to inhomogeneous banding on the walls, may prove generic in a broader class of inhomogeneous confined flows, a conjecture we shall explore more fully in future work.

Our observation of the interfacial instability in planar flow, combined with its linearly unstable nature, provides strong evidence in favour of scenario (ii) of the introduction. Experimental resolution unfortunately averages possible modes, predicted by linear stability analysis to be concurrent with ones (ongoing work). It thus remains an open challenge both theoretically and experimentally to delineate the effect of nonlinear coupling between these modes; and to study the interplay between the interfacial instability and the enhanced confinement effect reported here.

SMF thanks Mike Evans and Peter Olmsted for discussions; and the UK’s EPSRC for funding (EP/E5336X/1). The authors acknowledge Guillaume Degré, Jonathan Rothstein, Alexander Morozov, Elie Raphaël and Mike Cates for discussions; and Total, CNRS and ESPCI for their support.

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