Viscous flow over a chemically patterned surface. by James Sprittles | Papers by James

Physical Review E

PHYSICAL REVIEW E 76, 021602 2007 Viscous flow over a chemically patterned surface J. E. Sprittles* and Y. D. Shikhmurzaev† School of Mathematics, University of Birmingham, Birmingham, B15 2TT, United Kingdom Received 5 October 2006; published 14 August 2007 The classical fluid dynamics boundary condition of no slip suggests that variation in the wettability of a solid should not affect the flow of an adjacent liquid. However, experiments and molecular dynamics simulations indicate that this is not the case. In this paper we show how flow over a solid substrate with variations of wettability can be described in a continuum framework using the interface formation theory developed earlier. Results demonstrate that a shear flow over a perfectly flat solid surface is disturbed by a change in its wettability, i.e., by a change in the chemistry of the solid substrate. The magnitude of the effect is shown to be proportional to cos 1 − cos 2, where 1 and 2, are the equilibrium contact angles that a liquid-gas free surface would form with the two chemically different parts of the solid surface. DOI: 10.1103/PhysRevE.76.021602 PACS number s : 68.08. p, 47.61. k, 68.43. h I. INTRODUCTION The flow of liquids over chemically patterned surfaces is an exciting and new area of fluid mechanics with applications in many emerging technologies 1 . Such flows are of particular interest in microfluidics where an increasing surface to volume ratio of liquids means that surface effects become of greater significance 2 . The correct description of the physics at liquid-solid interfaces then becomes imperative to the success of any attempt to model this class of flows 3 . It has been shown that by patterning a substrate with hydrophilic and hydrophobic regions it is possible to confine a liquid to a microchannel 4,5 , to improve the accuracy of droplet deposition 6,7 or to create a structured film 8 . Alternatively, when a wettability gradient is present, unbalanced surface tension forces can lead to the movement of liquid drops 9,10 . The effect of variable wettability of the solid substrate on the adjacent flow has been studied theoretically using molecular dynamics simulations 11,12 . In this approach, variations in wettability are modeled by varying an interaction potential between molecules of the solid and the fluid. The results show that a change in wettability does affect the flow, most notably producing a component of velocity normal to the solid surface. Given that “wettability” can be introduced as a macroscopic characteristic of a liquid-solid system, one should be able to model the effects discovered by molecular dynamics macroscopically using an appropriate formulation in the framework of continuum mechanics. In the continuum approximation, molecular properties of the contacting media, as well as molecular length and time scales, do not appear explicitly. Instead, they manifest themselves in the bulk equations and boundary conditions via macroscopic transport coefficients and parameters of constitutive equations. The classical no-slip boundary condition leaves no room for incorporating the effects of variable wettability and, as is well known 13,14 , it becomes inadequate for dealing with processes of dynamic wetting where wettability of the solid plays a key role. *sprittlj@maths.bham.ac.uk † y.d.shikhmurzaev@bham.ac.uk A generalization of no slip often cited in the literature is the Navier slip condition 15,16 , where slip, i.e., the difference between the tangential velocities of the fluid and the solid, is assumed to be proportional to the tangential stress acting from the fluid on the liquid-solid interface. The coefficient of proportionality is referred to as the “slip coefficient” or the “coefficient of sliding friction.” Various expressions for this coefficient have been proposed 17 some of which are based on the results of molecular dynamics simulations 18 . An appropriate choice of the slip coefficient allows one to describe situations in which the characteristic length scales of the flow are small e.g., nanopores , so that the effects of slip become apparent 19 . The problem arises when the approach based on the Navier slip condition is used to describe flows over solid surfaces with variable wettability, since the existing models provide no conceptual link between slip and wettability. Indeed, as reviewed in Sec. 9 of 20 , in the area of dynamic wetting, where the physics of wettability becomes a key factor, the so-called “slip models” treat the behavior of the contact angle, which is the macroscopic “measure” of wettability, and slip, which is used as a boundary condition removing the stress singularity at the moving contact line, as completely independent. On a macroscopic level, any coupling of a formula for the velocity dependence of the dynamic contact angle and a slip boundary condition will produce a new slip model. From a theoretical perspective, this arbitrariness is clearly a weak point. If one steps from the continuum modeling down to molecular dynamics, then all fluid properties, including wettability, will of course naturally be linked. However, to represent and interpret the results macroscopically, one will need a set of macroscopic concepts, i.e., an appropriate macroscopic model of the phenomenon. Applying the no-slip or constant slip coefficient Navier boundary condition at a solid surface implies that the flow of a liquid will not be affected by variations in the wettability of an adjacent solid. This is in direct conflict with the conclusions of molecular dynamics simulations 11,12 that were specifically tailored to investigate this problem. In the present paper we consider flow over a solid surface of variable wettability using a model developed earlier 21 that incorporates wettability in the framework of continuum me©2007 The American Physical Society 1539-3755/2007/76 2 /021602 8 021602-1 J. E. SPRITTLES AND Y. D. SHIKHMURZAEV PHYSICAL REVIEW E 76, 021602 2007 chanics from the following perspective. Given that dynamic wetting is, by its very name, a process of creating a new fresh liquid-solid interface “a wetted solid surface” , an adequate mathematical model of dynamic wetting must have the physics of interface formation process at its core. The model hereafter referred to as the interface formation model has been derived from first principles 21 using methods of irreversible thermodynamics and notably it ensures that all aspects of wettability contact angle, slip, adsorption are interrelated. Embedding dynamic wetting in a general physical framework, as a particular case from a broad class of flows with forming disappearing interfaces, allows one to use the same model, without any ad hoc alterations, to describe other flows from this class 22–24 . This makes it possible to use the values for material constants determined from completely independent experiments. Comparisons with such experiments have confirmed the model’s validity and accuracy 21,25 . We will examine the fully representative case of a plane-parallel shear flow over a smooth solid surface that encounters a transition region between substrates of different wettability. II. PROBLEM FORMULATION Consider the steady flow of an incompressible Newtonian liquid passing over a stationary flat solid surface. The liquid is driven over the solid by a plane-parallel shear of magnitude S in the far field. We consider the bulk flow to be described by the Navier-Stokes equations · u = 0, u· u=− p+ 2 u, 1 where u, p, , and are the fluid’s velocity, pressure, density, and viscosity, respectively. The boundary conditions on a solid surface of uniform wettability, that follow from the interface formation theory 21 are given by n· u+ u * · I − nn + 1 2 = u · I − nn , 2 s u·n= − s e , s e 3 s · ss v =− − , 4 1 vs = u + 2 = s 0 , − vs · n = 0, s 5 6 . Here is the surface tension in the “surface phase,” i.e., a microscopic layer of liquid adjacent to the solid surface subject to intermolecular forces from two bulk phases; s is the surface density mass per unit area of this layer and vs is the velocity with which it is transported; n is the unit vector normal to the solid surface pointing into the liquid; I is the metric tensor; I − nn is a tensor that extracts the tangential component of a vector, for example, u · I − nn = u , where the double line subscript denotes tangential component; , , , , s0 , and s are phenomenological material constants. e The model has previously been discussed in detail e.g., 21 , so that here we will only briefly recapitulate the meaning of the terms. The surface tension is considered as a dynamic quantity related to the surface density via the equation of state in the “surface phase” 6 , which is taken here in the simplest linear form. The constant is associated with the inverse compressibility of the fluid while s0 is the surface density corresponding to zero surface tension. It is worth noting that the bulk fluid is assumed to be incompressible 1 whereas in the surface phase the actual density differs from that in the bulk and the corresponding surface density i.e., mass per unit area can vary 4 . The reason for this “duality” is that the bulk incompressibility is associated with the smallness of the Mach number, i.e., it is a limitation on macroscopic hydrodynamics, whereas the surface phase’s compressibility is controlled by independent factors as the surface phase is subject to asymmetric intermolecular forces that are singularly strong compared to the forces involved in macroscopic hydrodynamics. As in Gibbs’ theory of capillarity, the surface tension itself may be positive or negative depending on whether the solid is hydrophobic or hydrophilic. Gradients in surface tension influence the flow, firstly, via the tangential stress boundary condition 2 , i.e., via the Marangoni effect, and, secondly, in 5 by forcing the surface velocity vs, which is parallel to the solid surface, to deviate from that generated in the surface phase by the outer flow. It is noteworthy that, as pointed out by Gibbs 26 , physically, the surface phase is a thin layer of liquid adjacent to the solid surface and hence the velocity vs, being the average velocity associated with the mass flux in this layer, differs from the bulk velocity u evaluated on the liquid facing side of the liquid-solid interface. The constants and characterize the response of the interface to surface tension gradients and an external torque, respectively; in the simplest variant of the theory both are properties of the fluid and have no relation to the wettability of the solid. Mass exchange between the bulk and surface phases, caused by the possible deviation of the surface density from its equilibrium value s , is accounted for in the e boundary condition for the normal component of bulk velocity 3 and in the surface mass balance equation 4 . The parameter is the surface tension relaxation time. One would expect a generalized set of boundary conditions to have the no-slip condition as its limiting case. For the interface formation model this limiting case follows from the limits / L , U / L → 0, where L and U are characteristic length and velocity scales of the flow, applied to Eqs. 2 – 6 . Estimates for the phenomenological constants and , obtained from experiments on dynamic wetting 25 , suggest that, say, for L 10−2 cm, U 1 cm s−1, and 10 g cm−1 s−1 one has / L 10−5 and U / L 10−6. Then for flows which, unlike dynamic wetting, are not associated with infinitesimal length scales, boundary conditions 2 – 6 to leading order in / L and U / L, reduce to no slip. 021602-2 VISCOUS FLOW OVER A CHEMICALLY PATTERNED… PHYSICAL REVIEW E 76, 021602 2007 Conditions 2 – 6 were derived using methods of irreversible thermodynamics assuming that the equilibrium surface density s , determined by the wettability of the solid e substrate, is a constant, i.e., for a solid surface of a uniform wettability. This constant is related to the equilibrium contact angle that a liquid-gas free surface would form with the solid via the Young equation in the following way. If we assume that the equilibrium surface tension of the solid-gas interface is negligible, the Young equation takes the form sl = − lg cos , action occurring in the surface phase and between the surface phase and the bulk. As a result, one can expect effective or “apparent” slip, i.e., the difference between the velocity on the liquid-facing side of the interface and the velocity of the solid surface, that is, in our case, u · I − nn 0 and a nonzero normal component of velocity a flux in out of the surface phase, i.e., u · n 0 . It is convenient to nondimensionalize Eqs. 1 – 10 using U= −1 lg, L = US−1, P = S, 7 lg, s 0 , where sl and lg are the equilibrium surface tensions of the liquid-solid and liquid-gas interfaces and is the equilibrium contact angle that the free surface forms with the solid. Thus, s s since according to Eq. 6 , sl = 0 − e for a given liquid the Young equation 7 allows one to express s in terms of e see Eq. 19 below . In order to modify Eqs. 2 – 6 for a solid of variable wettability we must replace, in Eqs. 2 and 5 , → + s ss as the scales for velocities, length, pressure, surface tension, and surface density. Then in the bulk one has · u = 0, Re u · u = − p + 2 u, 11 while on the surface, where we use the notation u, v, and vs = vs for tangential bulk velocity, normal bulk velocity, and tangential surface velocity, respectively, 1d u v + + + 2 dx y x v=Q s s s e s e F, where Fs = s e s e ds e = ¯ u, dx 12 13 . 8 − s , s e The reaction force F acts on the liquid-solid interfacial layer from the solid surface and by balancing gradients of the s equilibrium surface tension e = e , ensures the existence of a state of equilibrium. Consider the equilibrium surface density of the form s e d v =− dx ss − s s e , 14 = 1 2 s 1e + s 2e + 1 2 s 2e − s 1e tanh x/l , 9 1 d + vs = u + ¯ 2 dx = s e ds e , dx 15 16 17 s s where 1e and 2e are the equilibrium surface densities in the far field as x → − and x → , respectively; l is the length of the transition region; x is a Cartesian coordinate in the plane of the solid surface. The equilibrium surface density in the form of Eq. 9 allows one to investigate the role of a transition region between solids of different wettabilities and, after taking the limit l / L → 0, find what boundary conditions for the surface variables one should use if this region is modeled as a solid-solid-liquid contact line. Finally, we will assume that the flow is plane-parallel in the x , y plane of a Cartesian coordinate system, the origin of which is at the center of the transition region, and that it is generated by constant shear of magnitude S in the far field, 1− s , = 1s 1s s s ¯ ¯ + ¯ 2e + ¯ 2e − ¯ 1e tanh x/l , 2 1e 2 u → 1,v → 0 as x2 + y 2 → . s 0 lg s ie s 0 and in the far field 18 Here Re = 2 lg 3, S =S , ¯= s 0 lg lg 2 S , Q= , ¯= S lg 2 , u → Sij · r as r → , 10 ¯ = Sl , l lg = , ¯s = ie i = 1,2 . where i and j are unit vectors in the x and y directions and r is the radius vector. Equations 1 – 10 now completely specify the problem. It is important to emphasize that in the derivation of the model it is assumed that on the solid-facing side of the liquid-solid interface one has impermeability and no slip. However, it is the velocity on the liquid-facing side of the liquid-solid interface that is the boundary condition for the Navier-Stokes equations 1 . In the classical no-slip condition it is assumed that there is no difference in velocity between the solid-facing and liquid-facing side of the interface, whereas in the interface formation model, the velocity on the liquid-facing side of the interface is determined by the inter- It is noteworthy that, unlike the classical Navier condition in Eq. 12 , which can be regarded as its generalization, the tangential stress the first term on the left-hand side includes v / x. The deviation of s from its equilibrium value and the resulting adsorption desorption lead to v 0 via Eq. 13 . Then, the spatial nonuniformity of this process makes v / x 0, thus “switching on” this term in the tangential stress in Eq. 12 and hence contributing to the apparent slip. The parameter Q in Eq. 13 is the ratio of the characteristic mass flux into out of the liquid-solid interface associated with the adsorption desorption process triggered by the deviation of the surface density from its local equilibrium 021602-3 J. E. SPRITTLES AND Y. D. SHIKHMURZAEV PHYSICAL REVIEW E 76, 021602 2007 y ψ=0.032 0.15 ψ=0.024 ψ=0.016 0.1 ψ=0.008 0.05 ψ=0 ψ=−0.002 0 −0.15 −0.05 0.05 0.15 x value and the characteristic mass flux due to convection in the bulk, whereas −1 characterizes the ratio of the former and the characteristic divergence of the convective mass flux in the surface phase. In the present context, is simply the product of the magnitude of shear in the far field S and the surface-tension-relaxation time . Given that it is the equilibrium contact angle , which a liquid-gas free surface would form with a solid, that we use as a measure of the wettability of a solid substrate, it is convenient to eliminate ¯ s , which are “internal” parameters ie of the model, in favor of i using Eqs. 7 and 16 as follows: ¯s ie =1+ −1 cos i i = 1,2 . 19 Hereafter we will refer to the portion of the solid substrate with equilibrium contact angle 1 and 2 as “solid 1” and “solid 2,” respectively. Following from 25 , where it was shown by analyzing −1 , we will further experiments on dynamic wetting that assume that = 1 and hence that, in terms of our nondimensional parameters, ¯ ¯ = 1. The analysis of experiments in 25 also provides estimates for the magnitude of phenomenological constants in the interface formation model’s equa1 g cm−3, tions. Using these estimates and taking −1 2 −1 −1 2 −1 10 – 10 g cm s , S lg 10– 10 dyn cm , 3 5 −1 −6 −5 10 – 10 s , and l 10 – 10 cm one arrives at a typical range of values for the magnitudes of the nondimensional groups Re Q 10−9 – 103, l 10−3 – 103, ¯ i FIG. 1. Streamlines of flow over a chemically patterned surface in which values of the streamfunction are given. Parameter values l Re= 0.01, = 0.01, ¯ = 10, Q = 100, ¯ = 0.1, = 10, 1 = 10°, and 2 = 100°. 10−6 – 10−2, 10−6 – 101, ¯ 101 – 107 , 2 – 102 , 0 ° ,180 ° i = 1,2 . As mentioned earlier, it is the double limit ¯ −1 → 0, → 0 applied to Eqs. 12 – 16 that results in the no slip condition and hence all effects associated with deviation from the classical no slip are at leading order in these parameters. III. SOLUTION can see i a positive normal velocity and ii variation in tangential velocity on the surface. The origin of the first of these effects is relatively straightforward. When fluid particles forming the interface are driven by the outer flow toward the region of lower equilibrium surface density, one has s that in the disturbed equilibrium s e, and hence, according to Eq. 13 , v 0. Importantly, it can be seen in Fig. 1 that the flux out of the surface phase occurs both in the hydrophilic x 0 and hydrophobic x 0 regions of the solid and extends itself well outside the transition zone. When solid 1 is more hydrophobic than solid 2 one observes the reverse effect, with the normal component of velocity directed towards the surface, corresponding to a flux into the surface phase. Once again this occurs on both sides of the transition region. In order to understand the distribution of the tangential component of the bulk velocity on the surface we consider the terms on the left-hand side of the generalized Navier The problem was solved numerically using the finite element method. Figure 1 shows the streamlines of the flow for the case where solid 1 is more hydrophilic than solid 2; the values of the dimensionless constants are given in the figure caption. As one can see, when the outer flow drives the fluid from a hydrophilic to a hydrophobic zone, there appears a normal flux from the surface phase into the bulk. It is noteworthy that, as shown in Fig. 1, the vertical component of bulk velocity is nonzero at y = 0, whereas for the classical Navier condition with different coefficients of sliding friction one has v = 0 at y = 0 12 and the normal component of velocity away from the solid appears solely due to the disturbance of the tangential flow at y = 0. In Figs. 2–6 the distributions of the bulk velocity components along the solid surface are shown for the case in which solid 1 is more hydrophilic than solid 2. In each graph one FIG. 2. Variation of the “generators” of slip the terms on the left-hand side of the generalized Navier condition 12 in response to a variation in the solid surface wettability. In curve 1, T = u/ y+ v/ x−1 while in curve 2, T = d / dx ss + / e d s / dx / 2. Results are obtained for parameter values e Re= 0.01, = 0.01, ¯ = 100, Q = 1, ¯ = 0.1, = 20, 1 = 10°, 2 = 100°. l 021602-4 VISCOUS FLOW OVER A CHEMICALLY PATTERNED… PHYSICAL REVIEW E 76, 021602 2007 (a) (a) (b) (b) FIG. 4. Dependence of u x , 0 and v x , 0 on Re, Q, and . Curve 2 corresponds to Re= 0.01, Q = 1, = 20; 1: = 50; 3 indistinguishable within the graphical accuracy : Re= 10; 4: Q = 2. l Parameters = 0.01, ¯ = 100, ¯ = 0.1, 1 = 10°, 2 = 100° for all curves. (c) FIG. 3. Distribution of u x , 0 and v x , 0 for different and ¯ . Curves 1–5 correspond to = 0.01, ¯ = 500; = 0.01, ¯ = 200; = 0.01, ¯ = 100; = 0.02, ¯ = 100; = 0.05, ¯ = 100, respectively; for all curves Re= 0.01, Q = 1, ¯ = 0.1, = 20, 1 = 10°, and 2 = 100°. l condition 12 , which determine u x , 0 . For a plane-parallel shear flow over a homogeneous surface, i.e., far away from the wettability transition region, there is no deviation of the surface density from its equilibrium value s = s and hence e no desorption from or adsorption into the liquid-solid interface v = 0 . This is an obvious solution of Eqs. 11 – 18 . In dimensionless variables, the tangential stress on the surface u / y + v / x has magnitude 1 u / y = 1, v / x = 0 . As one approaches the transition region, the situation changes. Curve 1 in Fig. 2 shows the distribution of the deviation of the tangential stress the first term on the lefthand side in Eq. 12 from the value 1 across this region. Importantly, there are now contributions to the tangential stress from both u / y and v / x since the latter becomes nonzero due to variation in the normal velocity along the surface as a result of the spatially nonuniform desorption adsorption process caused by the deviation of s from its local equilibrium value. As discussed earlier, this effect could follow neither from the standard Navier condition nor from any of its generalizations if the interface formation process and the associated mass exchange between the interface and the bulk are not taken into account. The other factors that, according to Eq. 12 , lead to slip on the liquid-solid interface behave as follows. As mentioned in the previous section, in equilibrium the surface force ss / e d s / dx / 2, and the surface tension gradient e d / dx / 2, balance each other to ensure that there is no perpetual motion. However, when a shear flow in the far field is imposed, it disturbs the surface phase, and the above two terms are no longer in balance since they obviously depend differently on the variable surface density s. The deviation of the second term on the left-hand side of Eq. 12 from 021602-5 J. E. SPRITTLES AND Y. D. SHIKHMURZAEV PHYSICAL REVIEW E 76, 021602 2007 (a) (a) (b) (b) FIG. 5. Velocity on the surface for different widths of transition l l region. Curves 1–3 correspond to ¯ = 1, ¯ = 0.1, and ¯ = 0.01, respecl tively; for all curves Re= 0.01, = 0.01, ¯ = 100, Q = 1, = 20, 1 = 10°, and 2 = 100°. FIG. 6. Velocity on the surface for different solid-solid pairs. Curve 1: 1 = 10°, 2 = 60°; 2: 1 = 60°, 2 = 110°; 3: 1 = 10°, 2 = 110°, respectively. For all curves Re= 0.01, = 0.01, ¯ = 100, Q = 1, ¯ = 0.1, = 20. l zero is shown as curve 2 in Fig. 2. One can see that it is the variation in this second term in Eq. 12 that dominates and hence it is the imbalance between the surface tension gradient and the tangential surface force caused by shear flow that is mainly responsible for a variation in slip on the surface as its wettability changes. The corresponding right-hand side of Eq. 12 and the normal velocity for these parameter values are shown by curve 3 of Fig. 3. Figure 3 illustrates the effect that the size of the parameters and ¯ have on the solution. As was mentioned, all effects associated with deviations from no slip, most clearly the nonzero normal velocity, are proportional to and ¯ −1, and the results shown in the figure support this conclusion. Noticeably, the normal velocity on the surface appears to be symmetric about the center of the transition region, where it achieves its maximum value. The tangential velocity seems to be antisymmetric about the origin, with a decrease in slip on solid 1 and increase in solid 2. Figure 4 shows the effect on the solution of the parameters Re, Q, and . Curves 2 and 3, which are almost indistinguishable, demonstrate that the Reynolds number has almost no effect on the dynamics of the surface. The local Reynolds number near the surface is always small due to the smallness of velocities in the vicinity of the solid surface even when the value associated with the global flow is relatively large, and one should indeed expect inertial effects to have little impact on dynamics in the surface phase. The parameter Q determines the degree of mass exchange between bulk and surface phase 13 . Curves 2 and 4 in Fig. 4 show that the greater its value, the more pronounced the effect will be. By varying one can see that the effect increases with the compressibility of the fluid. Figure 5 shows that for a smaller transition region one has a sharper effect. In all cases the disturbance, i.e., the nonzero normal component of the bulk velocity and variation in slip, runs well outside the region of varying wettability. The results suggest that if instead of a region, one treated the transition in wettability as a solid-solid-liquid contact line, then the disturbance to the bulk flow would be sharper than the effect associated with a finite transition region but would still occur over a finite region of the interface. It is interesting to note that although the shape of the curves in Fig. 5 differs, the integral of the normal velocity, i.e., the total flux out of the surface phase per unit time 021602-6 VISCOUS FLOW OVER A CHEMICALLY PATTERNED… PHYSICAL REVIEW E 76, 021602 2007 J= − v dx, 20 which we consider as a measure of the effect that a patterned surface has on an adjacent flow, remains unchanged. The value of J is a sensible choice of measure as we have seen that it is the normal component of velocity that causes the noticeable deviation from plane-parallel shear flow. Given that the change in solid does indeed alter the flow of an adjacent liquid, consider how the magnitude of the effect is dependent on the choice of solids. This can be illustrated by looking at three different solids characterized by contact angles of 10°, 60°, and 110° that a free surface would form with them. Figure 6 shows the velocity components for three different combinations of solids for the case where the first solid is more hydrophilic. The results suggest that the normal flux per unit time is proportional to the difference cos 1 − cos 2, which explains the ordering in Fig. 6, where we can see the case 10° → 60° gives a far smaller effect than 60° → 110° despite the difference in contact angles being the same. The numerical analysis of the problem made it possible to advance and then verify the following approximate formula for J: FIG. 7. Dependence of flux on parameters Q, , ¯ , and . Parameters are varied around a base state, the results of which are represented by vertical crosses, of ¯ = 100, Q = 1, = 0.01, = 20. Then, diamonds: = 0.02; squares: Q = 2; triangles: ¯ = 200; diagonal crosses: = 40. For all curves 1 = 90° while 2 is varied, and Re= 0.01. Curves 1–3 represent the predicted flux given by Eq. 21 . Jdim J= Q cos ¯ 2 1 Sh lg cos 1 − cos 2 . 22 − cos 2 . 21 Given that h is typically very small a few nm for simple fluids 27 , the above estimate highlights the subtle nature of the effects that we have described. IV. CONCLUSION This formula, which very accurately represents the numerical data over a wide range of parameter values, has been obtained as follows. The proportionality of the flux between the surface and bulk phases to the cosines of the contact angle is in fact what one should expect given that according to Eqs. 6 and 7 , cos is a linear function of the equilibrium surs s face density, and it is the difference ¯ 1e − ¯ 2e that determines the flux. This conjecture of the linear dependence of J on cos 1 − cos 2 is the only nontrivial step in obtaining Eq. 21 and it has to be verified numerically. We also have to find the coefficient of proportionality in this dependence in terms of the dimensionless parameters of the problem. In order to do this, we used the following procedure. For the fixed values of 1 and 2, we chose a base state in terms of the remaining parameters and then varied one of these parameters away from its base state to consider the effect this variation produces on J. After repeating this operation for all parameters we arrive at Eq. 21 , which now has to be verified by independently varying all dimensionless parameters, including 1 and 2. The accuracy with which this equation represents J is illustrated in Fig. 7. Order of magnitude arguments for the phenomenological parameters and the analysis of experiments on dynamic wet/ h, where h is the thickness of ting 25 suggest that the interfacial layer modeled here as an “interface” of zero thickness . Using this estimate, for the dimensional flux per unit time out of the surface phase in a liquid-solid-solid system one has As was shown, the interface formation model applied to the flow over a solid surface of variable wettability allows one to describe the main features of this flow observed in molecular dynamics simulations, most notably the nonzero component of the bulk velocity normal to the solid surface. A natural link between “wettability” interpreted in terms of the concept of the “contact angle” featuring in the spreading of liquids on solid surfaces and a viscous flow over chemically patterned solids with no free surface present has been established. Importantly, the interface formation model, which is discussed in further detail in 28 , deals with these phenomena entirely within the approach of continuum mechanics with no artificial inclusion of intermolecular forces in its framework. An interesting feature that follows from the results is that slip, i.e., the difference between the tangential component of the fluid’s velocity and the corresponding component of the velocity of the solid surface, results primarily from the disturbance of the force balance in the “surface phase” and not from the tangential stress, as follows from the standard Navier condition. ACKNOWLEDGMENTS The authors kindly acknowledge the financial support of Kodak European Research and the EPSRC via a Mathematics CASE award. 021602-7 J. E. SPRITTLES AND Y. D. SHIKHMURZAEV 1 Y. Xia, D. Qin, and Y. Yin, Curr. Opin. Colloid Interface Sci. 6, 54 2001 . 2 A. A. Darhuber and S. M. Troian, Annu. Rev. Fluid Mech. 37, 425 2005 . 3 T. M. Squires and S. R. Quake, Rev. Mod. Phys. 77, 977 2005 . 4 B. Zhao, J. S. Moore, and D. J. Beebe, Science 291, 1023 2001 . 5 H. Gau, S. Herminghaus, P. Lenz, and R. Lipowsky, Science 283, 46 1999 . 6 S. E. Burns, P. Cain, J. Mills, J. Wang, and H. Sirringhaus, MRS Bull. 28, 829 2003 . 7 A. Dupuis and J. M. Yeomans, FGCS, Future Gener. Comput. Syst. 20, 993 2004 . 8 H. G. Braun and E. Meyer, Thin Solid Films 345, 222 1999 . 9 M. K. Chaudhury and G. M. Whitesides, Science 256, 1539 1992 . 10 S. Daniel, M. K. Chaudhury, and J. C. Chen, Science 291, 633 2001 . 11 N. V. Priezjev, A. A. Darhuber, and S. M. Troian, Phys. Rev. E 71, 041608 2005 . 12 T. 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