<?xml version="1.0" encoding="UTF-8"?><!DOCTYPE article  PUBLIC "-//NLM//DTD Journal Publishing DTD v3.0 20080202//EN" "http://dtd.nlm.nih.gov/publishing/3.0/journalpublishing3.dtd"><article xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" dtd-version="3.0" xml:lang="en" article-type="research article"><front><journal-meta><journal-id journal-id-type="publisher-id">ACES</journal-id><journal-title-group><journal-title>Advances in Chemical Engineering and Science</journal-title></journal-title-group><issn pub-type="epub">2160-0392</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/aces.2012.22036</article-id><article-id pub-id-type="publisher-id">ACES-18916</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Chemistry&amp;Materials Science</subject></subj-group></article-categories><title-group><article-title>
 
 
  Comparison of Co-Current and Counter-Current Flow Fields on Extraction Performance in Micro-Channels
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>ubramaniam</surname><given-names>Pushpavanam</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Benny</surname><given-names>Malengier</given-names></name><xref ref-type="aff" rid="aff2"><sup>2</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib></contrib-group><aff id="aff2"><addr-line>Department of Mathematical Analysis, Ghent University, Ghent, Belgium</addr-line></aff><aff id="aff1"><addr-line>Department of Chemical Engineering, Indian Institute of Technology Madras (IIT Madras), Chennai, India</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>spush@iitm.ac.in(UP)</email>;<email>bm@cage.ugent.be(BM)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>27</day><month>04</month><year>2012</year></pub-date><volume>02</volume><issue>02</issue><fpage>309</fpage><lpage>320</lpage><history><date date-type="received"><day>December</day>	<month>12,</month>	<year>2011</year></date><date date-type="rev-recd"><day>January</day>	<month>24,</month>	<year>2012</year>	</date><date date-type="accepted"><day>February</day>	<month>25,</month>	<year>2012</year></date></history><permissions><copyright-statement>&#169; Copyright  2014 by authors and Scientific Research Publishing Inc. </copyright-statement><copyright-year>2014</copyright-year><license><license-p>This work is licensed under the Creative Commons Attribution International License (CC BY). http://creativecommons.org/licenses/by/4.0/</license-p></license></permissions><abstract><p>
 
 
  Several applications such as liquid-liquid extraction in micro-fluidic devices are concerned with the flow of two immiscible liquid phases. The commonly observed flow regimes in these systems are slug-flow and stratified flow. The latter regime in micro-channels has the inherent advantage that separation of the two liquids at the exit is efficient. Recently extraction in a stratified counter-current flow has been studied experimentally and it has been shown to be more efficient than co-current flow. An analytical as well as a numerical method to determine the steady-state solution of the corresponding convection-diffusion equation for the two flow-fields is presented. It is shown that the counter-current process is superior to the co-current process for the same set of parameters and operating conditions. A simplified model is proposed to analyse the process when diffusion in the transverse direction is not rate limiting. Different approaches to determining mass transfer coefficient are compared. The concept of log mean temperature difference used in design of heat exchangers is extended to describe mass transfer in the system.
 
</p></abstract><kwd-group><kwd>Plug Flow; Diffusion; Extraction; Co-Current; Counter-Current</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>The physical effects which govern the behavior of fluids flowing at the micro-scale and the macro-scale are different. Surface tension, viscous effects, energy dissipation and capillary action begin to dominate system behavior at the micro-scale. Micro-fluidics studies the behavior of the fluids at the micro-scale induced by these effects. It helps exploit the behavior at these scales for new applications by improving the efficiency of current processes.</p><p>Micro-fluidics results in Process Intensification through miniaturization. These systems are characterized by a dominance of viscous forces as compared to inertial forces; hence, typically low Reynolds numbers are encountered. Consequently, the flow regimes observed in these systems is laminar. Mixing in these micro-channels occurs primarily by molecular diffusion. The time needed for mixing by molecular diffusion is proportional to the square of the length of the diff usion path. The marked shortening of the diffusion path in a micro-channel results in relatively good mixing.</p><p>Multiphase liquid-liquid flows arise when two or more partially miscible or completely immiscible fluids are brought in contact and subjected to a pressure gradient. The resulting systems display different kinds of flow behavior, e.g. droplet, slug or stratified flow. These regimes depend on the relative flow rates of the fluid phases involved, the resulting interaction between interfacial and viscous forces and the wetting behavior of the channel walls. Different liquid-liquid two-phase flow patterns in micro-channels have been experimentally analysed, see Dessimoz et al. [<xref ref-type="bibr" rid="scirp.18916-ref1">1</xref>].</p><p>In the context of mass transfer across membranes Guo and Ho [<xref ref-type="bibr" rid="scirp.18916-ref2">2</xref>] have analysed an analytical solution based on separation of variables for co-current and counter-current flows in an annulus. The eigen-functions were obtained using a power series expansion. Here the velocity fields in the two chambers were decoupled as they were separated by a porous membrane. Electro-osmotic flows in micro channels have been frequently proposed as a way to overcome dispersion effects. This causes the velocity profile in the micro-channel to remain almost uniform except for a small region near the walls. The flow-field under these conditions can be approximated as an ideal plug-flow in the micro-channel. Liu et al. [<xref ref-type="bibr" rid="scirp.18916-ref3">3</xref>] and Gao et al. [<xref ref-type="bibr" rid="scirp.18916-ref4">4</xref>] have studied the electro-osmotic flow in a rectangular channel when one fluid is conducting and the other is non conducting as is usually the case in extraction. The flow-profiles were obtained analytically for the two fluids when the non conducting fluid was dragged by the viscous force of the conducting fluid. Wang et al. [<xref ref-type="bibr" rid="scirp.18916-ref5">5</xref>] have studied experimentally as well as theoretically how the interface level can be controlled in a two liquid system under the influence of a pressure drop and an electric field applied to one of the fluids. Their results indicate that the flow profiles in the two fluids can be approximated as plug-flows with a jump discontinuity at the interface for some operating conditions.</p><p>Recent studies have focused on liquid-liquid extraction in the stratified flow regime in the micro-channels. Here the two fluids flow side by side. This flow-pattern can be exploited to facilitate complete separation at the channel exit. The extraction of vanillin dissolved in water using toluene in micro-structured devices made of Poly Di Methyl Siloxane (PDMS) was studied experimentally by Fries et al. [<xref ref-type="bibr" rid="scirp.18916-ref6">6</xref>]. Here the performance of segmented and stratified flow regimes were compared. LIF and microPIV measurements showed a laminar profile for stratified flow, whereas vortices in the slug were detected for segmented flow. The influence of channel width and therefore, the surface-to-volume ratio was investigated for stratified flow. There was a significant enhancement of mass transfer with decrease in the channel cross-sectional area for the stratified flow regime.</p><p>Three different fluid-flow patterns in a Y-shaped micro-channel, contact or stratified flow, segmented flow and emulsification were investigated in Okubo et al. [<xref ref-type="bibr" rid="scirp.18916-ref7">7</xref>]. Here a one-dimensional model for extraction assuming the interface to be at the centre of the channel was used to compare the model predictions with the experimental behavior. A two-dimensional flow-field taking into account the effect of the interface not being at the centre was analysed numerically by Žnidaršič-Plazl and Igor Plazl [<xref ref-type="bibr" rid="scirp.18916-ref8">8</xref>]. They compare their model predictions with experimental results on steroid extraction. Most of the research in stratified flow has been when the fluids flow co-currently i.e. in the same direction. TeGrotenhuis et al. [<xref ref-type="bibr" rid="scirp.18916-ref9">9</xref>] has studied the counter-current mass transfer in a micro-channel when the two fluids are separated by a membrane. Here the diff usional resistance through the membrane was incorporated in the analysis. Recently it has been shown that by suitable modification of the channel surface it is possible to have counter-current flow in the micro-channels over a wide range of operating conditions, Aota et al. [<xref ref-type="bibr" rid="scirp.18916-ref10">10</xref>]. They found that a maximum possible theoretical plate number of 4.6 is achievable in counter-current flow as opposed to co-current flow. The pressure drop characteristics in a counter-flow micro-channel have been investigated by Hibara et al. [<xref ref-type="bibr" rid="scirp.18916-ref11">11</xref>]. The velocity profiles in a 100 micron channel with butylacetate and an aqueous phase flowing in a countercurrent manner was measured using micro-PIV, Aota et al. [<xref ref-type="bibr" rid="scirp.18916-ref12">12</xref>].</p><p>The counter-current flow is known to be more eﬃcient in the context of heat exchanger networks. In this work the performance of co-current and counter-current flows in extraction is being studied with focus on micro-channels. Recently it has been experimentally shown that counter-current operation is possible in micro-channels. The primary objective of this work is to establish conditions under which the counter-current operation is superior to the co-current operation. To the best of our knowledge a theoretical analysis of this system has not been carried out. The main motivation is to show that improvements in the extraction performance are possible when the flow is counter-current as opposed to co-current. The convective diffusion equation is solved analytically for the co-current operation. This is a one dimensional model with diffusion being considered only in the direction transverse to the flow direction. Here axial dispersion effects are neglected. The counter-current system is solved numerically. The algorithm proposed exploits the features of the system. A lumped model is analysed where the concentration dependency on the flow direction alone is considered. It is shown that the counter-current flow performs better than the co-current flow. Different methods to compute the mass transfer coefficient as proposed in the literature are compared.</p></sec><sec id="s2"><title>2. Co-Current and Counter-Current Flow</title><p>We consider three different flow regimes for the analysis in this work: 1) co-current laminar flow, 2) co-current plug flow, and 3) counter-current plug flow. The stratified flow (fluids flow side by side as shown in <xref ref-type="fig" rid="fig1">Figure 1</xref>) of two liquid phases is analysed between two infinite horizontal plates extending to infinity in the z-direction. This assumption on the geometry helps us focus on the physics of the problem keeping the mathematics tractable. The distance between the plates (along the x-direction) is taken as H and the liquid-liquid interface is at distance h<sub>l</sub> (subscript l for laminar) from the lower plate. The flow is assumed to be in the y-direction. <xref ref-type="fig" rid="fig1">Figure 1</xref> shows a schematic of the system being analyzed.</p><sec id="s2_1"><title>2.1. Laminar Flow</title><p>In the case of laminar or Poiseuille flow, the velocity profile is obtained assuming the flow to be steady, fully developed and the liquids to be incompressible. The velocity profiles of the system are governed by the equations</p><disp-formula id="scirp.18916-formula38142"><label>(1)</label><graphic position="anchor" xlink:href="15-3700146\1a57ea62-df7d-4413-a26d-55a0bcc151da.jpg"  xlink:type="simple"/></disp-formula><p>These equations are subject to the conditions of no slip at the walls and continuity of velocity and shear stress at</p><p>the interface which is located at h<sub>l</sub>. So</p><disp-formula id="scirp.18916-formula38143"><label>(2)</label><graphic position="anchor" xlink:href="15-3700146\1bbe12b0-a70a-428a-afb8-72fbace13e00.jpg"  xlink:type="simple"/></disp-formula><p>In the above the subscript 1 and 2 are used to denote the fluid in the first and second region respectively. The solutions to the above equation yield the velocity profiles of the two liquids as Equation (3).</p><p>Here the imposed pressure gradient is denoted as<img src="15-3700146\fe1c6257-fcce-4c79-82ba-ce88a5cb596e.jpg" />. Both the fluids are subject to the same pressure drop. The flow behavior is hence similar to the Hagen-Poiseuille flow (parabolic in shape). The velocity field is continuous at the interface h<sub>l</sub> but its derivatives are discontinuous. A schematic of the velocity profile in the channel is shown in <xref ref-type="fig" rid="fig2">Figure 2</xref>.</p><p>The experimentalist operates the system at fixed flowrates Q<sub>1</sub> and Q<sub>2</sub>.</p><p>They are given by Equation (4).</p><p>These equations can be used to determine the pressure drop ∇P and the height h of the interface for a given combination of flow-rates and fluids. Alternatively, if the pressure drop and height of interface are specified, the velocity profiles in each liquid layer can be found and from this the flow rates can be determined.</p></sec><sec id="s2_2"><title>2.2. Co-Current Plug Flow</title><p>In this case the velocities v<sub>1</sub> and v<sub>2</sub> have the same sign, and are constant within their phase. It is well established that plug flow behavior can be achieved in a micro channel using electro-osmosis [<xref ref-type="bibr" rid="scirp.18916-ref4">4</xref>]. This eliminates axial dispersion effects which arise from laminar flow in micro-channels. The electric field can also be used to control the interface height for a fixed combination of flowrates.</p><p>In the case of plug flow, with equal velocity in both phases, we denote interface as h = h<sub>n</sub>. Here</p><p><img src="15-3700146\efd119a0-b872-41b2-914d-6c5ee0e34e7c.jpg" /></p><p>When plug flow is assumed viscosity does not play any role in determining the interface position. If on the other hand we assume the flow to be laminar, then the interface position is determined by the viscosity of the two fluids.</p></sec><sec id="s2_3"><title>2.3. Counter-Current Plug Flow</title><p>In this case the velocities v<sub>1</sub> and v<sub>2</sub> have an opposite sign. We take <img src="15-3700146\0a1192eb-7753-4f7f-a997-0ef3fc32873a.jpg" /> and<img src="15-3700146\ab996238-6ad4-4310-8fe7-27dd938e0234.jpg" />. Counter-current flow can be theoretically simulated using a combination of Poiseulle flow and a Couette flow. To generate a clear separation of the two phases the interface must be located at</p><disp-formula id="scirp.18916-formula38144"><label>(3)</label><graphic position="anchor" xlink:href="15-3700146\bf85f9ab-56e2-499a-afcd-0d263b6da485.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.18916-formula38145"><label>(4)</label><graphic position="anchor" xlink:href="15-3700146\1755982f-946e-40a7-b8ac-ec83ae276927.jpg"  xlink:type="simple"/></disp-formula><p>the point where the velocity is zero. Alternatively combination of electro osmotic flow with Poiseulle flow can give a counter-current flow when there are two immiscible liquids as the electric field affects the flow of only one of the two fluids. The electric field can be manipulated to increase or decrease the velocity for a fixed flow rate. This can be used to control the interface position “h”. Experimentally counter-current flow has been achieved by surface modifications of the micro-channels [<xref ref-type="bibr" rid="scirp.18916-ref10">10</xref>]. For the sake of mathematical simplicity the velocity in each of the phases is assumed to be uniform across the transverse direction in counter-current flow.</p></sec></sec><sec id="s3"><title>3. Mass Transfer in Extraction</title><p>The mass transfer behavior in stratified flow of a liquid-liquid extraction system in a micro-channel is now analysed. Here we consider the flow of a solute in the first fluid which is being extracted by the second fluid. The concentration in fluid 1, respectively 2 is represented by C<sub>1</sub>, respectively C<sub>2</sub>. Considering steady-state operation with convection in the y-direction and diffusion in the x-direction we obtain the equations which govern the behavior of the system as</p><disp-formula id="scirp.18916-formula38146"><label>(5)</label><graphic position="anchor" xlink:href="15-3700146\5a6c4d76-277e-4417-bafa-db6d5c15ad7e.jpg"  xlink:type="simple"/></disp-formula><p>Here the expressions of v<sub>1</sub>, v<sub>2</sub> take on distinct values for laminar, co-current and counter-current flows. At the interface we have,</p><disp-formula id="scirp.18916-formula38147"><label>(6a)</label><graphic position="anchor" xlink:href="15-3700146\ac494636-29fc-487c-b54a-39790f4eb3cb.jpg"  xlink:type="simple"/></disp-formula><p>at the walls we have</p><disp-formula id="scirp.18916-formula38148"><label>(6b)</label><graphic position="anchor" xlink:href="15-3700146\03c85dd1-0b88-4337-834f-48ee31e08951.jpg"  xlink:type="simple"/></disp-formula><p>and at the inlet y = 0 we have</p><disp-formula id="scirp.18916-formula38149"><label>(7)</label><graphic position="anchor" xlink:href="15-3700146\2a9b1e75-def7-405c-93f9-c65641c0f8cf.jpg"  xlink:type="simple"/></disp-formula><p>The film interface conditions result in a discontinuous concentration profile, while keeping the mass flux continuous. If K &gt; 1, C<sub>2</sub> remains below the value of C<sub>1</sub> at the interface. When K &lt; 1 the reverse is true and the second fluid extracts the solute out of the first strongly. Here the concentration C<sub>1</sub> is depleted at the interface and we obtain a larger C<sub>2</sub> concentration. In our computations we use C<sup>in</sup> = 1 mol/m<sup>3</sup>.</p><p>In the co-current flow (superscript co) the concentrations of the outlet streams both tend to an equlibrium and this limits the extraction. In the counter-current flow (superscript cc) this limitation does not exist and hence the performance is much better.</p><p>For co-current (laminar or plug flow), the conservation of mass states that</p><p><img src="15-3700146\f07cdaef-0ee1-48dc-9e05-3ed5940e7228.jpg" /></p><p>under steady-state conditions. This is valid for a long channel when the two exiting streams are in equilibrium. Hence</p><p><img src="15-3700146\c4a0ca0f-ee61-49c5-b2a9-595d41789f2c.jpg" /></p><p>For counter-current flow the overall mass balance gives</p><p><img src="15-3700146\8f1b5316-94f6-4b82-b432-4709e1dd3de9.jpg" /></p><p>This is used to check the numerical solution. The mixed cup average concentration at a particular “y” is given by<img src="15-3700146\21f88a95-ff8a-4f68-89a4-a97df96637a0.jpg" />.</p></sec><sec id="s4"><title>4. Analytical Solution for Co-Current Plug Flow</title><p>The convection diffusion equation can be solved analytically and elegantly under the assumptions of 1) the co-current Plug Flow Regime (PFR) when the velocity in the two fluids is uniform (v<sub>1</sub> and v<sub>2</sub> are constant), and 2) a constant transverse diffusion coefficient (D<sub>1</sub> and D<sub>2</sub>). We start with non dimensionalizing the equations with respect to their characteristic lengths and initial concentrations,</p><p><img src="15-3700146\ddcb7cc8-1d32-4521-852f-d66a030ef748.jpg" /></p><p>which gives the dimensionless form as</p><disp-formula id="scirp.18916-formula38150"><label>(8)</label><graphic position="anchor" xlink:href="15-3700146\ec4e6778-fa09-4dd3-b772-f4e1b5e48b32.jpg"  xlink:type="simple"/></disp-formula><p>For simplicity, we drop the superscript * from now on. We seek the solution C<sub>i </sub>(x, y) in the form g<sub>i</sub>(y) f<sub>i</sub>(x). Substituting this in (8) gives</p><p><img src="15-3700146\cdf73382-5ebb-43fd-b65d-e10d4d5039ca.jpg" /></p><p>Or</p><disp-formula id="scirp.18916-formula38151"><label>(9)</label><graphic position="anchor" xlink:href="15-3700146\5c42f41f-2a8e-4afa-a452-f797e3f96c24.jpg"  xlink:type="simple"/></disp-formula><p>This results in an eigen value problem in the x direction whose solution is</p><disp-formula id="scirp.18916-formula38152"><label>(10)</label><graphic position="anchor" xlink:href="15-3700146\f50f7dd1-5585-44a3-ab59-c6f306f67cbf.jpg"  xlink:type="simple"/></disp-formula><p>The boundary conditions at x = 0, 1 yield a = c = 0. At x = h, the boundary condition C<sub>1</sub> = KC<sub>2</sub> implies</p><disp-formula id="scirp.18916-formula38153"><label>(11a)</label><graphic position="anchor" xlink:href="15-3700146\759e8cf9-c7e2-467c-a599-e1f4b9d18d1f.jpg"  xlink:type="simple"/></disp-formula><p>while <img src="15-3700146\5b435627-d61f-4ea4-ae29-8947774b363a.jpg" /> implies</p><disp-formula id="scirp.18916-formula38154"><label>(11b)</label><graphic position="anchor" xlink:href="15-3700146\298aee53-93f8-46e2-963f-f9e2e445d3c2.jpg"  xlink:type="simple"/></disp-formula><p>We seek b and d to be non-zero. This yields the characteristic equation which determines the eigen values λ as the solution to</p><disp-formula id="scirp.18916-formula38155"><label>(12)</label><graphic position="anchor" xlink:href="15-3700146\8410c572-f420-4d61-a7e3-2b702141d75f.jpg"  xlink:type="simple"/></disp-formula><p>where<img src="15-3700146\481f7daa-643b-44c5-824b-9c540418c60f.jpg" />. The eigen functions corresponding to the nth eigen value is</p><disp-formula id="scirp.18916-formula38156"><label>(13)</label><graphic position="anchor" xlink:href="15-3700146\b34b83ac-38d9-45ac-9ee7-c05ade93ab33.jpg"  xlink:type="simple"/></disp-formula><p>It has been shown in [<xref ref-type="bibr" rid="scirp.18916-ref13">13</xref>] that this system is self-adjoint in the inner product when the velocities in the two fluids are equal i.e., v<sub>1</sub> =v<sub>2</sub><sub></sub></p><disp-formula id="scirp.18916-formula38157"><label>(14)</label><graphic position="anchor" xlink:href="15-3700146\bdaebb07-a749-4072-b6ab-20817c626e0f.jpg"  xlink:type="simple"/></disp-formula><p>The eigen functions are normalized with respect to this inner product and the constants b<sub>n</sub>, d<sub>n</sub> are obtained as</p><disp-formula id="scirp.18916-formula38158"><label>(15)</label><graphic position="anchor" xlink:href="15-3700146\6394bee2-087c-484b-b868-ed327734eb9c.jpg"  xlink:type="simple"/></disp-formula><p>The solution for the y dependency is <img src="15-3700146\4b1bdf1e-7136-4bc9-8886-8f7f8183fca6.jpg" />.</p><p>For co-current extraction the initial condition is C<sub>1</sub> = 1 for 0 &lt; x &lt; h and C<sub>2</sub> = 0 for h &lt; x &lt; 1. The coefficient k<sub>n</sub> can be obtained from the initial condition as</p><p><img src="15-3700146\553584ae-5698-471c-9419-cab06b24f212.jpg" /></p><p>Since the boundary conditions are homogeneous Neumann in the x-direction, λ = 0 is also an eigen value, which corresponds to n = 1. The eigen-function corresponding to this is the equilibrium solution and is given by</p><disp-formula id="scirp.18916-formula38159"><label>(16)</label><graphic position="anchor" xlink:href="15-3700146\977596d5-0a7a-49c3-8fd7-fe9745050712.jpg"  xlink:type="simple"/></disp-formula><p>The complete solution to the convection diffusion equation is hence</p><disp-formula id="scirp.18916-formula38160"><label>(17)</label><graphic position="anchor" xlink:href="15-3700146\30c7f891-8cba-4b0a-a9cf-8dbe2b078a4b.jpg"  xlink:type="simple"/></disp-formula><p>It was found that it was sufficient to take the first fifty terms in the summation in the above solution to obtain convergence. This implies that the eigen-value problem (14) is solved for the first 50 roots. Care must be taken to ensure that no roots are missed and no roots are calculated more than once. This analytical solution is used to validate the numerical code based on the method of lines with a second order finite difference scheme in the transverse direction (x). The numerical method was used to determine the concentration profiles in the laminar flow regime.</p><p>In <xref ref-type="fig" rid="fig3">Figure 3</xref> we show how the analytical solution for the co-current plug flow based on the separation of variables (solid line) validates the predictions of the numerical code (points) based on finite differences. It is seen that both the average concentration as well as the concentration at a fixed y using the two approaches agree quantitatively.</p><p>The numerical code was then used to simulate the behavior for the laminar flow profile in co-current mode.&#160; Here the velocity profile obtained in Equation (3) is used to simulate the laminar behavior. The comparison of the cup-averaged concentration profiles obtained using the laminar flow and the plug flow behavior in a microchannel is shown in <xref ref-type="fig" rid="fig4">Figure 4</xref>. For the plug flow simulation the average velocity of the laminar flow is used. It is seen that the extraction performance under laminar flow conditions is superior to that of the plug flow conditions.</p></sec><sec id="s5"><title>5. Numerical Solution Counter-Current Flow</title><p>For the counter-current plug flow the convective-diffusion equations are solved numerically. Two challenges arise in this and need to be addressed. These are, 1) the jump discontinuity in concentrations at the interface and 2) the inlet of the two fluid streams being at the two end points. The latter renders the system a boundary value problem.</p><p>The numerical algorithm we use for solving the steady-state convection diffusion equation for extraction under counter-current flow is now described:</p><p>1) The channel length is divided into Ny grids in the “y” direction. The values of the solute concentrations at the interface on the fluid1 side are assumed.</p><p>2) The values of the concentrations at the interface on the fluid 2 side are obtained using the equilibrium condition.</p><p>3) Now the convection diffusion equation in each fluid is solved using the method of lines. This is possible as we have a Dirichlet boundary condition at one end (the interface) and a Neuman condition at the other end (wall) with known inlet conditions. Here a second order scheme is used to discretise the equations in the transverse direction and the equations are integrated along the axial direction.</p><p>4) After the solutions are obtained the fluxes at the Ny grid points are calculated in each fluid. The difference in the fluxes at the interface has to be zero. This condition is used to iterate on the concentrations at the interface on fluid 1 till convergence is achieved using a NewtonRaphson technique.</p><p>The above algorithm is implemented in Matlab. The cup-mixed average concentration profile along the axis obtained using the above algorithm is shown in <xref ref-type="fig" rid="fig5">Figure 5</xref>.</p></sec><sec id="s6"><title>6. Simplified Model for Co-Current and Counter-Current Flow</title><p>To obtain a quick physical insight into the behavior obtained in the two flow-regimes of co-current and countercurrent flow, a simplified model is proposed in this Section. It is valid under the assumptions of a very small height H of the channel (as prevailing in micro-channels),</p><p>and large diffusion coefficients D<sub>i</sub>. Under these conditions the concentration variation in the direction transverse to the flow can be neglected and the evolution of the average concentration along the axial direction is governed by ordinary differential equations. For simplicity we assume the velocity profile to follow plug flow.</p><sec id="s6_1"><title>6.1. Co-Current Flow</title><p>The simplified equations of mass balance are now given by</p><disp-formula id="scirp.18916-formula38161"><label>(18a)</label><graphic position="anchor" xlink:href="15-3700146\f176f7f7-cd00-419c-a661-5c3f86658b16.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.18916-formula38162"><label>(18b)</label><graphic position="anchor" xlink:href="15-3700146\e98a3887-0d40-45b4-ad12-04fe8e2724d2.jpg"  xlink:type="simple"/></disp-formula><p>with <img src="15-3700146\168cda22-17eb-4745-b8d0-60007a072579.jpg" />and initial condition</p><p><img src="15-3700146\d013723d-66e9-426f-95c2-733d71cf3ac0.jpg" /></p><p>Here <img src="15-3700146\03a8c491-08bf-46ee-9a9e-1a11498b42e3.jpg" /> represents an overall mass transfer coefficient (between the two phases). We now define</p><p><img src="15-3700146\6f4fd227-d0f6-4bd1-8af7-59500abb2d47.jpg" /></p><p>The solution to the above two equations is given by</p><disp-formula id="scirp.18916-formula38163"><label>(19a)</label><graphic position="anchor" xlink:href="15-3700146\a45f7c98-a829-481a-8492-316ef0d6ef60.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.18916-formula38164"><label>(19b)</label><graphic position="anchor" xlink:href="15-3700146\7c93b78a-9a6a-4a8e-99b3-f2c30ea504a2.jpg"  xlink:type="simple"/></disp-formula></sec><sec id="s6_2"><title>6.2. Counter-Current Flow</title><p>The simplified equations are now given by</p><disp-formula id="scirp.18916-formula38165"><label>(20a)</label><graphic position="anchor" xlink:href="15-3700146\d4eaa6e7-a0d7-4b22-bac4-40875af89e67.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.18916-formula38166"><label>(20b)</label><graphic position="anchor" xlink:href="15-3700146\6815cd38-c719-4ae9-aa3d-459c41f82ac7.jpg"  xlink:type="simple"/></disp-formula><p>with initial condition</p><p><img src="15-3700146\45780d4e-5131-44a3-8c2c-2e842f540b95.jpg" /></p><p>Introducing <img src="15-3700146\c68cfc60-f891-4ad1-a4f2-75d34ddbbbf1.jpg" /> and <img src="15-3700146\0fbde94b-689c-4aa9-9d1e-9cf3f5b2e9be.jpg" /> as before, the solution is given by</p><disp-formula id="scirp.18916-formula38167"><label>(21a)</label><graphic position="anchor" xlink:href="15-3700146\ddd6ab8a-a8d4-415b-b938-915f7cc9a4fd.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.18916-formula38168"><label>(21b)</label><graphic position="anchor" xlink:href="15-3700146\742e3731-1cdd-465b-bb34-61ad007ec8f6.jpg"  xlink:type="simple"/></disp-formula><p>We now describe how the mass transfer coefficient k<sub>l</sub> can be estimated for a system experimentally.</p><p>For Co-current flow, the simplified equations (18a) and (18b) can be rearranged to yield</p><disp-formula id="scirp.18916-formula38169"><label>(22a)</label><graphic position="anchor" xlink:href="15-3700146\adf95176-2eda-46ce-8d40-fbe279a41be2.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.18916-formula38170"><label>(22b)</label><graphic position="anchor" xlink:href="15-3700146\3273ab6c-4303-45e4-83d6-b519b0431049.jpg"  xlink:type="simple"/></disp-formula><p>The rate at which mass is transferred when the concentration drops to c<sub>1</sub> or c<sub>2</sub> in the system is</p><disp-formula id="scirp.18916-formula38171"><label>(23a)</label><graphic position="anchor" xlink:href="15-3700146\285816ca-54d4-4813-8c08-c2b4c5f66cbb.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.18916-formula38172"><label>(23b)</label><graphic position="anchor" xlink:href="15-3700146\1bd4cf79-d53b-4710-b6cb-131492f9c516.jpg"  xlink:type="simple"/></disp-formula><p>Using these equations, we obtain</p><p><img src="15-3700146\8333735b-b1db-4778-9265-c5f7da7782ec.jpg" /></p><p>Rearranging and eliminating the terms containing the interface position “h” using (22b) we obtain</p><disp-formula id="scirp.18916-formula38173"><label>(24)</label><graphic position="anchor" xlink:href="15-3700146\d3225560-ec8c-455b-9ef4-cc7b63bf6409.jpg"  xlink:type="simple"/></disp-formula><p>At y = L, the exit <img src="15-3700146\867ab6fc-f6bb-456c-a4ca-89c9208b3048.jpg" /></p><p>The logarithmic mean concentration difference is defined as</p><disp-formula id="scirp.18916-formula38174"><label>(25a)</label><graphic position="anchor" xlink:href="15-3700146\20a75761-8f94-4371-99e4-ec252daef80d.jpg"  xlink:type="simple"/></disp-formula><p>In a similar manner, k<sub>l</sub> can be calculated for countercurrent flow, using the simplified equations (20a) and (20b). Following the procedure for co-current flow it can be seen that</p><disp-formula id="scirp.18916-formula38175"><label>(25b)</label><graphic position="anchor" xlink:href="15-3700146\cbc78f67-65db-47a2-8e97-2e87e383e2ab.jpg"  xlink:type="simple"/></disp-formula><p>The mass transfer coefficient k<sub>l</sub> can also be defined using the driving force for extraction to be the deviation from equilibrium value, see Dessimoz [<xref ref-type="bibr" rid="scirp.18916-ref1">1</xref>]. This gives the mass transfer coefficient as</p><disp-formula id="scirp.18916-formula38176"><label>(26)</label><graphic position="anchor" xlink:href="15-3700146\61ee03af-550d-4825-8b89-55be3fac807e.jpg"  xlink:type="simple"/></disp-formula></sec></sec><sec id="s7"><title>7. Results and Discussion</title><p>In order to compare the results of our simulations and to be consistent with the literature, and evaluate the performance of a specific micro-channel set-up, we introduce some characteristic quantities. These are now defined.</p>Characteristic Quantities<p>The first is the efficiency E, defined in terms of the mixed cup concentrations as</p><disp-formula id="scirp.18916-formula38177"><label>(27)</label><graphic position="anchor" xlink:href="15-3700146\3e424da4-5462-4c23-82b1-55be05c4143b.jpg"  xlink:type="simple"/></disp-formula><p>where <img src="15-3700146\87b5ea86-840f-4136-8e34-4057d8e9b578.jpg" /> is the concentration of the solute in the second region after equilibrium is attained, and typically<img src="15-3700146\6808236c-8cf0-4b29-be88-679791a825d0.jpg" />. “E” is a measure of how close the exiting stream is to equilibrium. The overall residence time t<sub>res</sub> for co-current flow is defined as</p><disp-formula id="scirp.18916-formula38178"><label>(28)</label><graphic position="anchor" xlink:href="15-3700146\ed88fb66-84ac-48c0-9568-f7542e0fe54a.jpg"  xlink:type="simple"/></disp-formula><p>For a given length L, a unique residence time and an extraction efficiency E(L) is obtained. E = 1 corresponds to the situation when the exiting streams are in equilibrium and no further separation can take place.</p><p>The second characteristic which can describe the system is the extraction ratio E<sub>r</sub>. It represents the fraction of the amount of solute that has been fed to the system which is removed by the second fluid. This is defined as</p><disp-formula id="scirp.18916-formula38179"><label>(29)</label><graphic position="anchor" xlink:href="15-3700146\ed661d94-4f72-4b2a-bfc0-0d285ed165db.jpg"  xlink:type="simple"/></disp-formula><p>Note that for co-current flow</p><disp-formula id="scirp.18916-formula38180"><label>(30)</label><graphic position="anchor" xlink:href="15-3700146\ebff0f55-213b-4414-93e9-88a332716db9.jpg"  xlink:type="simple"/></disp-formula><p><xref ref-type="fig" rid="fig6">Figure 6</xref> shows the dependency of concentration along</p></sec></body><back><ref-list><title>References</title><ref id="scirp.18916-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">A.-L. Dessimoz, L. Cavin, A. Renken and L. 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