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Microscopic Marangoni flows cannot be predicted on the basis of pressure gradients

Yawei Liu Beijing Advanced Innovation Center for Soft Matter Science and Engineering, Beijing University of Chemical Technology, Beijing 100029, China State Key Laboratory of Organic-Inorganic Composites, Beijing University of Chemical Technology, Beijing 100029, China    Raman Ganti Department of Chemistry, University of Cambridge, Lensfield Road, Cambridge CB2 1EW, UK    Hugh G. A. Burton Department of Chemistry, University of Cambridge, Lensfield Road, Cambridge CB2 1EW, UK    Xianren Zhang State Key Laboratory of Organic-Inorganic Composites, Beijing University of Chemical Technology, Beijing 100029, China    Wenchuan Wang Beijing Advanced Innovation Center for Soft Matter Science and Engineering, Beijing University of Chemical Technology, Beijing 100029, China    Daan Frenkel df246@cam.ac.uk Department of Chemistry, University of Cambridge, Lensfield Road, Cambridge CB2 1EW, UK
(September 29, 2025)
Abstract

A concentration gradient along a fluid-fluid interface can cause flow. On a microscopic level, this so-called Marangoni effect can be viewed as being caused by a gradient in the pressures acting on the fluid elements, or as the chemical-potential gradients acting on the excess densities of different species at the interface. If the interfacial thickness can be ignored, all approaches should result in the same flow profile away from the interface. However, on a more microscopic scale, the different expressions result in different flow profiles, only one of which can be correct. Here we compare the results of direct non-equilibrium Molecular Dynamics simulations with the flows that would be generated by pressure and chemical potential gradients. We find that the approach based on the chemical potential gradients agrees with the direct simulations, whereas the calculations based on the pressure gradients do not.

Fluid flows can be generated by variations of temperature or solute concentration parallel to a fluid-fluid interface. This phenomenon is known as the Marangoni effect (see e.g. Loewenthal (1931); Hershey (1939)). The ‘continuum’ explanation for this effect is that the gradients in temperature or concentration result in gradients in the surface tension, which then induce shear flow Young et al. (1959); Sternling and Scriven (1959); Levich (1962); Levich and Krylov (1969); Ruckenstein (1981); Anderson (1989); Fanton and Cazabat (1998). For some applications, it would be interesting to have a higher-resolution description of Marangoni flows. The reason is that the local shear in Marangoni flows can be quite large and could become important for nano-fluidics Stone et al. (2004); Squires and Quake (2005); Bocquet and Charlaix (2010); Bocquet and Tabeling (2014). Moreover, the precise Marangoni flow profile might affect the orientation and even conformation of molecules such as proteins near an interface. At present, such microscopic insights in Marangoni flows are lacking.

In this paper, we study the flow induced in a flat liquid-liquid interface by the concentration gradient of a neutral solute (i.e. the ‘solutal’ Marangoni effect). We first review the various (pressure or chemical potential-based) expressions for the force acting on molecules near the interface. We then perform Molecular Dynamics (MD) simulations to compare the flows generated by these forces with the results of direct non-equilibrium simulations.

Let us first consider two immiscible liquids at temperature TT, that meet at a flat liquid-liquid interface at z(x,y)=0z(x,y)=0. When a concentration gradient is applied along xx, flow occurs due to a surface-tension gradient. The surface tension, γ\gamma, can be related to the integral of the difference between the longitudinal and transverse pressures near the interface:

γ=+[pzz(z)pxx(z)]𝑑z,\gamma=\int_{-\infty}^{+\infty}[p^{zz}(z)-p^{xx}(z)]dz, (1)

where pzz(z)p^{zz}(z) and pxx(z)p^{xx}(z) are the normal and transverse components of the pressure tensor at zz, respectively Tolman (1948); Kirkwood and Buff (1949); Marchand et al. (2011). As was pointed out by Schofield and Henderson Schofield and Henderson (1982), the integral in Eq. 1 does not depend on the choice of the expression for the pressure tensor. Nevertheless, the microscopic flow near an interface is expected to depend on the local gradients of the pressure, rather than the gradients of the integral of the pressure tensor. This is important because, close to the interface, the viscosity of the liquid need not be constant, hence making a difference where the forces act.

The most intuitive method to obtain the Marangoni force acting on fluid molecules near the interface is to calculate the force per unit volume on a small volume element from the pressure gradient (pxx(z)/x\partial p^{xx}(z)/\partial x), and then obtain the force per particle by dividing the force per volume by the local number density. We now make the assumption that pxx(z)p^{xx}(z) depends on xx only through its dependence on the spatial variation in the bulk concentration ρC\rho_{C} (or, equivalently, the chemical potential) of the species subject to a concentration gradient:

fV(z)=pxx(z)ρCρCx.f^{V}(z)=-\frac{\partial p^{xx}(z)}{\partial\rho_{C}}\frac{\partial\rho_{C}}{\partial x}. (2)

We note that the condition for mechanical equilibrium in the bulk implies, via the Gibbs-Duhem relation, that a concentration gradient in a ‘solute’ also causes a gradient in the concentration of the solvent. However, these other gradients are not independent, and hence we will treat the solute concentration gradient as the independent variable.

The general expression for the local pressure tensor at position 𝐫{\bf r} is given by

pab(𝐫)=ρ(𝐫)kBTδab+1Vij>irijafijbξab(𝐫,𝐫i,𝐫j),p^{ab}({\bf r})=\rho({\bf r})k_{B}T\delta^{ab}\\ +\frac{1}{V}\bigg{\langle}\sum_{i}\sum_{j>i}r_{ij}^{a}f_{ij}^{b}\xi^{ab}\left({\bf r},{\bf r}_{i},{\bf r}_{j}\right)\bigg{\rangle}, (3)

under the condition of 𝑑𝐫ξab(𝐫,𝐫i,𝐫j)=1\int d{\bf r}\xi^{ab}\left({\bf r},{\bf r}_{i},{\bf r}_{j}\right)=1 Irving and Kirkwood (1950); Schofield and Henderson (1982); Gloor et al. (2005). Here, aa and bb denote the cartesian components of the pressure tensor, ρ(𝐫)\rho({\bf r}) is the local density, δab\delta^{ab} denotes the Kronecker delta, rijr_{ij} and fijf_{ij} represent the distance and force between particles ii and jj, and ξab(𝐫,𝐫i,𝐫j)\xi^{ab}\left({\bf r},{\bf r}_{i},{\bf r}_{j}\right) is the fraction of the intermolecular virial from a given pair of molecules at 𝐫i{\bf r}_{i} and 𝐫j{\bf r}_{j} to be assigned to position 𝐫{\bf r}. As was argued in ref. Schofield and Henderson, 1982, there is no unambiguous way to assign the intermolecular virial in the system. All definitions of the pressure tensor that differ only by a function that is divergence-free are acceptable. There are, in fact, several widely used definitions for the local pressure tensor Kirkwood and Buff (1949); Harasima (1953). For example, for a given pair of molecules, the virial definition specifies that half of the contribution to the stress resides in each elemental volume containing the molecule Nijmeijer et al. (1988), while the Irving-Kirkwood definition specifies that the contribution is evenly distributed along a line connecting the two molecules Irving and Kirkwood (1950). These two definitions lead to the same value of the surface tension, but to very different results for the pressure tensor distribution in the interface Walton et al. (1983); Weng et al. (2000).

Gibbs was the first to give a consistent thermodynamic description of the surface tension Gibbs (1957). In particular, Gibbs related the variation of the surface tension with chemical potential of species ii to the excess of that species at the interface. For an nn-component system: dγ=i=1nΓidμid\gamma=-\sum_{i=1}^{n}\Gamma_{i}d\mu_{i}, with Γi\Gamma_{i} the surface excess and dμid\mu_{i} the chemical potential variation due to the concentration gradient. We assume that μi/x{\partial\mu_{i}}/{\partial x} is independent of zz (fast equilibration normal to the interface). Because Γi(ρi(z,x)ρibulk(x))𝑑z\Gamma_{i}\equiv\int_{-\infty}^{\infty}\left(\rho_{i}(z,x)-\rho_{i}^{\text{bulk}}(x)\right)dz, the surface tension gradient along xx is

γx=i=1n(ρi(z,x)ρibulk(x))(μix)dz.\frac{\partial\gamma}{\partial x}=\int_{-\infty}^{\infty}\sum_{i=1}^{n}\left(\rho_{i}(z,x)-\rho_{i}^{\text{bulk}}(x)\right)\left(-\frac{\partial\mu_{i}}{\partial x}\right)dz. (4)

This suggests that the local force acting on a volume element at 𝐫{\bf r} is given by i=1nΓi(𝐫)(μi/x)-\sum_{i=1}^{n}\Gamma_{i}({\bf r})\left(-{\partial\mu_{i}}/{\partial x}\right). Such a relation also follows from the Gibbs-Duhem equation Vdp=i=1nNidμiVdp=\sum_{i=1}^{n}N_{i}d\mu_{i} with NiN_{i} the number of particles of component ii in volume VV and pp the pressure. Let us denote the number density of component ii in the mixture by ρi\rho_{i}. Then dp=i=1nρidμidp=\sum_{i=1}^{n}\rho_{i}d\mu_{i}. A concentration gradient of component ii along xx will lead to a chemical potential gradient μi/x\partial\mu_{i}/\partial x. As the pressure remains constant in the bulk, we must have 0=i=1nρibulk(x)(μi/x)0=\sum_{i=1}^{n}\rho_{i}^{\text{bulk}}(x)\left(\partial\mu_{i}/\partial x\right). At a position zz near the interface, a pressure gradient remains giving a force per unit volume

fV(z)=(p(z,x)x)=i=1n(ρi(z,x)ρibulk(x))(μix).f^{V}(z)=\left(-\frac{\partial p(z,x)}{\partial x}\right)\\ =\sum_{i=1}^{n}\left(\rho_{i}(z,x)-\rho_{i}^{\text{bulk}}(x)\right)\left(-\frac{\partial\mu_{i}}{\partial x}\right). (5)

We can interpret (μi/x)\left(-{\partial\mu_{i}}/{\partial x}\right) as the force per-atom acting on the particles of component ii. This expression is convenient, because the imposed chemical potential gradients are constant throughout the system. In the bulk, the composition is such that the forces balance (because the bulk pressure equilibrates rapidly). Upon approaching the interface, the concentration of different components may change, leading to non-zero net forces. In other words: particles of a given species experience the same force regardless of their distance from the interface. The force acting on species ii is then

fi=(μibulkx)=(μibulkρi)Pρi.f_{i}=\left(-\frac{\partial\mu_{i}^{\text{bulk}}}{\partial x}\right)=\left(-\frac{\partial\mu_{i}^{\text{bulk}}}{\partial\rho_{i}}\right)_{P}\cdot\nabla\rho_{i}. (6)

We now have two alternative expressions (Eq. 2 and Eq. 5) for the surface force arising in the solutal Marangoni effect. Both satisfy that the integrated surface force is equal to the surface tension gradient, but otherwise they are not obviously identical.

To test which, if any, of these microscopic expressions is correct, we performed MD simulations on a simple model system. We consider a fluid mixture composed of one solute (CC) and two immiscible solvents(AA and BB, respectively), with two liquid-liquid interfaces, as shown in Fig. 1. All particles are assumed to have the same mass mm and molecular radius σ\sigma. They interact through Lennard-Jones potentials, Uαβ(r)=4ϵαβ[(σ/r)12(σ/r)6]U_{\alpha\beta}(r)=4\epsilon_{\alpha\beta}\left[(\sigma/r)^{12}-(\sigma/r)^{6}\right] (α,β{A,B,C}\alpha,\beta\in\left\{A,B,C\right\}) with interaction energy ϵαβ\epsilon_{\alpha\beta}. All interactions are truncated and shifted at 4σ4\sigma. For simplicity, we focus on ideal solutions composed of identical solvent and solute particles and take ϵAA=ϵBB=ϵCC=ϵAC=ϵBC1.0ϵ\epsilon_{AA}=\epsilon_{BB}=\epsilon_{CC}=\epsilon_{AC}=\epsilon_{BC}\equiv 1.0\epsilon (which defines our unit of energy). However, AA and BB tend to demix because they have a weaker attraction: ϵAB\epsilon_{AB}=0.3 ϵ\epsilon. Throughout this article we use reduced units, with σ\sigma, ϵ\epsilon and mm denoting the units of length, energy and mass respectively.

All simulations were carried out using LAMMPS Plimpton (1995) in an isothermal, isobaric (NpzzTNp^{zz}T) ensemble. Periodic boundary conditions were imposed in all directions. The temperature and normal pressure during the simulations were maintained at T=0.846T=0.846 and pex=0.012p_{ex}=0.012. The relaxation parameter for the Nosé-Hoover thermostat is set to 0.10.1, and that for the pressure barostat is 11. The velocity-Verlet algorithm with a time step of 0.0010.001 is used for the integration of equations of motion. All simulations were run for 2×1084×1082\times 10^{8}-4\times 10^{8} steps to obtain good statistics.

Refer to caption
Figure 1: (a) Simulation box used to compute the force and flow profiles using the forces obtained from Eq. 6 and Eq. 7. (b) Simulation box used in the non-equilibrium MD simulations with explicitly imposed concentration gradients. The red and blue particles represent the two solvents (AA and BB), the green particles represent the solute (CC), and the black particles represent the solid walls.

The computation of pxx(z)/ρC\partial p^{xx}(z)/\partial\rho_{C} requires several equilibrium simulations at a constant bulk concentration. These can be carried out in a relatively small simulation box, shown in Figure 1(a). The box dimensions were LxL_{x}=16.44 and LyL_{y}=9.86, Lz\langle L_{z}\rangle=42.4 (LzL_{z} fluctuates, and depends very weakly on the solute concentration). The system contained 50405040 particles, approximately equally distributed between the AA-phase and the BB-phase. To compute the composition-dependence of pxx(z)p^{xx}(z), we performed simulations where we varied the concentration of the solute CC, while keeping the total number of particles fixed.

From the numerical estimate of pxx(z)/ρC\partial p^{xx}(z)/\partial\rho_{C}, we computed the corresponding force at ρC=0.02\rho_{C}=0.02 and ΔρC=0.01\Delta\rho_{C}=0.01 using

fV(z)=pxx(z)ρCρCxpρC+ΔρCxx(z)pρCΔρCxx(z)2ΔρCρCf^{V}(z)=-\frac{\partial p^{xx}(z)}{\partial\rho_{C}}\frac{\partial\rho_{C}}{\partial x}\\ \approx-\frac{p^{xx}_{\rho_{C}+\Delta\rho_{C}}(z)-p^{xx}_{\rho_{C}-\Delta\rho_{C}}(z)}{2\Delta\rho_{C}}\cdot\nabla\rho_{C} (7)

We verified that our estimate for the pressure gradient did not depend on our choice of ΔρC\Delta\rho_{C}. Subsequently, we converted the force per unit volume to a force per particle, by dividing by the total number density at height zz, ρ(z)\rho(z). Such a body-force might, for instance, be due to a gravitational field. These per-particle forces were then applied in a non-equilibrium simulation of the fluid with solute density ρC\rho_{C} to measure the corresponding flow profile at ρC\nabla\rho_{C}.

Starting from Eq. 6 we can compute the forces that would result from the gradient of the chemical potentials. These per-atom forces were applied to the solute and the solvent particles. During all these simulations with explicit forces, a constant force is applied to all fluid particles to balance the surface force, to ensure that there is no center-of-mass flow. To measure the local velocity, the simulation box was divided into a series of slabs of thickness dz=0.05dz=0.05 parallel to the interface. The local velocity is computed as the time-averaged center-of-mass velocity of all fluid particles in each slab.

To compare, we performed non-equilibrium simulations where a concentration gradient was explicitly imposed. Figure 1(b) shows the simulation box in which the fluid mixture has a constant bulk concentration gradient along xx. The box size LxL_{x}=59.19 and LyL_{y}=9.86, and Lz\langle L_{z}\rangle= 42.4. The system contained 1814418144 particles, approximately equally distributed between the AA-phase and the BB-phase. Non-equilibrium simulations were carried out to measure the flow profile at a given value of ρC\nabla\rho_{C}. In this case, we employed a box that was terminated on both ends by hard walls perpendicular to the xx-direction. These walls were composed of frozen fluid particles that interact with the fluid via Lennard-Jones potentials where ϵWA=ϵWB=ϵWC=1.0ϵ\epsilon_{WA}=\epsilon_{WB}=\epsilon_{WC}=1.0\epsilon. Next to each wall, we defined a ‘source’ region with a width of 88. During the simulations, every 500500 steps, the types of the fluid particles in the bulk of these source regions are reset to maintain constant bulk concentrations on the two sides and a steady gradient along xx. In the simulation, flow in the interface, set in motion by the surface force, is accompanied by a bulk back-flow caused by the presence of the walls.

Refer to caption
Figure 2: (a) The bulk concentration profiles along xx from the non-equilibrium simulations. (b) The density profiles along zz near one interface at z=10.6z=10.6 from the non-equilibrium simulation at ρC=0.0005\nabla\rho_{C}=0.0005 (dashed lines), and from the equilibrium simulation at ρC0.02\rho_{C}\sim 0.02 (solid lines). The density profiles near another interface at 10.6-10.6 are the same.
Refer to caption
Figure 3: (a-b) The pressure profiles along zz near one interface at z=10.6z=10.6 calculated by the Irving-Kirkwood definition (a) and virial definition (b) at ρC0.01\rho_{C}\sim 0.01. The black dashed line shows the external pressure of pex=0.012p_{ex}=0.012. (c) The volume force profiles per unit concentration gradient along zz near one interface at z=10.6z=10.6 calculated by different methods at ρC0.02\rho_{C}\sim 0.02. The horizontal dashed line corresponds to the force of zero.

Figure 2(a) shows the bulk concentration profiles along xx for the non-equilibrium simulations. The figure shows that the concentration profile is linear between the limiting values imposed at the walls. The concentration gradients in two independent simulations were ρC=0.001\nabla\rho_{C}=0.001 and ρC=0.0005\nabla\rho_{C}=0.0005, respectively. Figure 2(b) shows the density profiles for each component along zz from the simulation of ρC=0.0005\nabla\rho_{C}=0.0005. As the average bulk concentration is 0.020.02, the density profiles from the equilibrium simulation at ρC0.02\rho_{C}\sim 0.02 are also plotted here for comparison. The results show good agreement for the local densities from the two simulations, indicating that in the non-equilibrium simulation, fluid states are still close to equilibrium and that equilibration along zz is fast. Both are assumptions we adopted to calculate the surface force via Eq. 2 and Eq. 5.

In order to calculate the surface force at ρC0.02\rho_{C}\sim 0.02 via Eq. 2, we computed the pressure-tensor profile at ρC0.01\rho_{C}\sim 0.01 and ρC0.03\rho_{C}\sim 0.03. Figure 3 shows the pressure profiles along zz near a liquid-liquid interface at ρC0.01\rho_{C}\sim 0.01 using the Irving-Kirkwood and virial definitions. In the bulk where the fluid is homogeneous, both definitions lead to the same value since pzz=pxx=pex=0.012p^{zz}=p^{xx}=p_{ex}=0.012. Upon approaching the interface, pzzp^{zz} from the Irving-Kirkwood definition is (necessarily) the same as the bulk pressure, reflecting mechanical equilibrium along zz [Fig. 3 (a)]. As is well known the virial expression for pzzp^{zz} is not constant [Fig. 3 (b)]. We verified that the two expressions for the pressure tensor did yield the same value of surface tension. We find (from Eq. 1) that the surface tension is 1.141.14 at ρC0.01\rho_{C}\sim 0.01 and 1.051.05 at ρC0.03\rho_{C}\sim 0.03.

The chemical potential for component ii is given by μi=μi0+kBTlnρibulk+μiexc\mu_{i}=\mu_{i}^{0}+k_{B}T\ln\rho_{i}^{\text{bulk}}+\mu_{i}^{exc}, with kBk_{B} the Boltzmann constant. μi0\mu_{i}^{0} denotes a (constant) reference value and μiexc\mu_{i}^{exc} denotes the excess chemical potential due to intermolecular interactions. Because the bulk solutions are ideal, μiexc\mu_{i}^{exc} does not depend on the concentration of CC. Thus, at ρC0.02\rho_{C}\sim 0.02, with ρAbulk=ρBbulk=0.742\rho_{A}^{\text{bulk}}=\rho_{B}^{\text{bulk}}=0.742 and ρCbulk=0.019\rho_{C}^{\text{bulk}}=0.019 [Fig. 2(b)], if ρC=1.0\nabla\rho_{C}=1.0, we obtain fA=fB=1.14f_{A}=f_{B}=1.14 and fC=44.53f_{C}=-44.53 from Eq. 5 (i.e. we do indeed have force balance in the bulk).

We are now in a position to compare the force profiles that follow from the pressure tensor gradients with those that follow from the chemical potential gradient. Figure 3 (c) shows the profiles of the volume force at ρC0.02\rho_{C}\sim 0.02 with ρC=1.0\nabla\rho_{C}=1.0. As can be seen from the figure, the two expressions for the surface force (Eq. 2 and Eq. 5) produce significantly different results at the interface. Not surprisingly, the forces calculated from the chemical potentials (Eq. 5), are concentrated where there is an excess of solute [Fig. 2(b)]. However, the forces calculated by using the local pressure tensors computed via the Irving-Kirkwood and virial definitions (Eq. 2), extend over larger distances and vary in sign. The Irving-Kirkwood and virial definitions lead to force profiles that are very similar. We verified that the integrated Marangoni force is effectively the same for all methods used: 4.7±0.1-4.7\pm 0.1 for the chemical potential, 4.8±0.1-4.8\pm 0.1 for the virial and 4.8±0.1-4.8\pm 0.1 for the Irving-Kirkwood, respectively. Moreover, these values agree with the surface tension gradient calculated from the values of surface tension at different concentrations, which is 4.8±0.1-4.8\pm 0.1 at ρC0.02\rho_{C}\sim 0.02 with ρC=1.0\nabla\rho_{C}=1.0 (calculated via (γ/ρC)ρC(\partial\gamma/\partial\rho_{C})\nabla\rho_{C}).

Refer to caption
Figure 4: The velocity profiles along zz from different methods at ρC=0.0010\nabla\rho_{C}=0.0010 (a-b) and at ρC=0.0005\nabla\rho_{C}=0.0005 (c-d). The horizontal dashed line corresponds to the velocity of zero.

The fact that pressure-tensor and chemical potential routes lead to different force profiles implies that they would result in different flow profiles. At most, one can be correct. To test this, we applied the force profiles that we computed to the fluid mixture at ρC0.02\rho_{C}\sim 0.02 and measured the flow profile as a function of zz for fixed ρC\nabla\rho_{C}. The Irving-Kirkwood and virial definitions lead to very similar results for the surface force, and hence we show only the virial flow profile. Figure 4(a) shows the predicted velocity profiles at ρC=0.001\nabla\rho_{C}=0.001. We see that although the velocity profiles are very similar in the bulk, they are significantly different near the interface. For the sake of comparison, the velocity profile obtained in a non-equilibrium MD simulation with an imposed concentration gradient of ρC=0.001\nabla\rho_{C}=0.001 was determined in a region with 10<x<10-10<x<10 (x=0x=0 at the center of the box). The result is shown in Fig. 4(b). We see that the velocity profile that follows from the direct simulation differs markedly from the one obtained from the pressure tensor gradients. However, it agrees quite well with the predictions based on the chemical-potential gradient calculations. The same results were found at ρC=0.0005\nabla\rho_{C}=0.0005 [Fig. 4 (c) and (d)].

This finding is interesting because it indicates that the use of local pressure-tensor gradients leads to incorrect prediction of the Marangoni flow profile near the interface, even though the velocity in the bulk is still reliable. The latter finding is consistent with our previous work Ganti et al. (2017), which showed that bulk thermo-osmotic flow computed via local pressure gradients agrees well with the flow predicted by its reciprocal mechano-caloric coefficient. Our results suggest that the chemical potential route, which is anyway the simplest, should be the preferred route to compute microscopic Marangoni flows.

In their original hydrodynamic formulation of the stress tensor Irving and Kirkwood (1950), Irving and Kirkwood note that a boundary or interface can cause the stress to depend on gradients of the pairwise atomic density, which can be neglected in the standard Irving-Kirkwood expression for fluids in the absence of gradients. The present work provides evidence that the problem hinted at by Irving and Kirkwood indeed becomes important in a gradient near an interface, as the potential part of the stress tensor then depends not only on the distance of two points between which a force acts, but also on the absolute coordinates of these points.

Acknowledgements.
This work was supported by the European Union through ETN NANOTRANS grant 674979 MSC the Sackler Fund. YL would like to acknowledge the hospitality of the Chemistry Department of the University of Cambridge.

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