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    Technical Note

    Thermally fully developed electroosmotic flow through a rectangular microchannel

    Jie Su a, Yongjun Jian a,, Long Chang a,b

    a School of Mathematical Science, Inner Mongolia University, Hohhot, Inner Mongolia 010021, Chinab School of Mathematics and Statistics, Inner Mongolia Finance and Economics College, Hohhot, Inner Mongolia 010051, China

    a r t i c l e i n f o

    Article history:

    Received 11 January 2012Received in revised form 14 May 2012

    Accepted 18 May 2012

    Available online 23 June 2012

    Keywords:

    Rectangular microchannel

    Electroosmotic flow

    Fully developed

    Joule heating

    a b s t r a c t

    This study investigates the velocity and temperature distributions of the thermally fully developed

    electroosmotic flow through a rectangular microchannel. Based on linearized PoissonBoltzmann (PB)equation, NavierStokes equation and thermally fully developed energy equation, analytical solutions

    of normalized velocity, temperature and Nusselt number are derived. They greatly depend on the ratio

    Kof characteristic scale of the rectangular microchannel to Debye length, width to height ratio a andJoule heating to heat flux ratioS. By numerical computation, we found that for prescribed electrokinetic

    width K, increased S yields greater temperature. For small K, the variations of the temperatureh are larger

    than those of large K. The dependence of temperature on Sis more significant for a small K, while at a

    larger Kthe temperature profiles are almost identical. In addition, we illustrate the Nusselt number Nu

    variations withS,a andK. 2012 Elsevier Ltd. All rights reserved.

    1. Introduction

    Microfluidics is a very important research area due to numerouspotential applications in separation and analysis. Most substances

    acquire surface electric charges when in contact with an aqueous

    medium. The rearrangement of the charges on the solid surface

    and in the liquid results in the formation of the electrical double

    layer (EDL) [1]. If an electric field is applied tangentially along a

    charged surface, the electric field will exert a body force on the ions

    in the diffuse layer, resulting in electroosmotic flow (EOF).

    Many experimental observations have shown that flow phe-

    nomena and heat transfer in microscale are quite different from

    those in macroscale. Many hydrodynamics of a fully-developed

    and transient EOF have been analyzed in various micro-capillaries

    geometric domains[27]. Recently, Investigations have been con-

    ducted to better understand the heat transfer characteristics in

    microchannel for applications in electronic cooling. The effect of

    viscous dissipation in fully developed electroosmotic heat transfer

    has been analyzed by Maynes and Webb [8]. Closed form expres-

    sions in a parallel plate or circular microchannel for Nusselt num-

    ber were obtained for electroosmotic heat transfer with or without

    Joule heating effects[911].

    Understanding the heat transfer characteristics of EOF through

    a rectangular microchannel is very important. However, there

    appear to be no studies reported in the literature treating convec-

    tive heat transfer for EOF through a rectangular microchannel. The

    purpose of this study is to present analytical expressions for ther-

    mally and hydrodynamically fully developed EOF in a rectangular

    microchannel with constant wall heat flux.

    2. Mathematical modeling

    2.1. EDL potential distribution

    A straight two dimensional rectangular microchannel of width

    2W, height 2H and length L is shown in Fig. 1. The fluid flow is

    acted upon by an axial steady electric field of strength E. Due to

    the symmetry of the problem, the solution domain can be reduced

    to a quarter cross section of the channel. For a symmetric binary

    electrolyte solution, the electrical potential w of the EDL isdescribed by the PB equation

    @2w

    @x2@2w

    @y22n0zme

    e sinh

    zmew

    kbT0 1

    which is subject to the following boundary conditions

    wjxW f; wjyH f; dw

    dx

    x0

    0; dwdy

    y0

    0 2

    wheree is the dielectric constant of the electrolyte liquid,n0is theion density of bulk liquid,zmis the valence, e is the electron charge,

    kbis the Boltzmann constant, T0is the absolute temperature andfis

    the wall zeta potential. We assume the electrical potential is small

    enough, so that the DebyeHckel linearization approximation can

    be used. Introducing the following dimensionless groups:

    0017-9310/$ - see front matter 2012 Elsevier Ltd. All rights reserved.http://dx.doi.org/10.1016/j.ijheatmasstransfer.2012.05.056

    Corresponding author.

    E-mail address:[email protected](Y. Jian).

    International Journal of Heat and Mass Transfer 55 (2012) 62856290

    Contents lists available atSciVerse ScienceDirect

    International Journal of Heat and Mass Transfer

    j o u r n a l h o m e p a g e : w w w . e l s e v i e r . c o m / l o c a t e / i j h m t

    http://dx.doi.org/10.1016/j.ijheatmasstransfer.2012.05.056mailto:[email protected]://dx.doi.org/10.1016/j.ijheatmasstransfer.2012.05.056http://www.sciencedirect.com/science/journal/00179310http://www.elsevier.com/locate/ijhmthttp://www.elsevier.com/locate/ijhmthttp://www.sciencedirect.com/science/journal/00179310http://dx.doi.org/10.1016/j.ijheatmasstransfer.2012.05.056mailto:[email protected]://dx.doi.org/10.1016/j.ijheatmasstransfer.2012.05.056
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    x xH

    ; y yH

    ; w zvewkbT0

    ; f zvefkbT0

    ;

    j 2

    n0

    z

    2

    me

    2

    ekbT0 1=2

    ; K jH 3

    Wherej is DebyeHckel parameter, Kis called the electrokineticwidth. Thus the normalized Eq. (1) and boundary conditions Eq.

    (2)can now be expressed as

    @2w

    @x2 @

    2w

    @y2 K2w 4

    @w0; y@x

    0; @wx;0@y

    0 5a

    wa; y f; wx;1 f 5bwherea = W/His the ratio of the width to height of the channel sec-tion,fis the dimensionless wall zeta potential. The solution to the

    linearized PB Eq. (4) subjected to the boundary conditions Eq. (5)

    can be obtained as[12]

    w 4fX1m1

    cosh

    ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiK2 b2m

    q x

    Em

    cosbmy

    4fX1n1

    cosh

    ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiK2 c2n

    q y

    Fn

    coscnx 6

    where bm2m 1p

    2 ; cn

    2n 1p2a

    ; m; n 1;2;3; . . .

    7a

    Em2m 1p cosh

    ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiK2 b2m

    q a

    1m1

    ;

    Fn2n 1p cosh

    ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiK2 c2n

    q 1n1

    7b

    The detail derivation can be found in Ref. [13]. The ionic net charge

    density gives

    qe ej2wkbT0zve

    8

    Once the distributions of charge density are known, the Cauchymomentum can be solved analytically.

    2.2. The analytical solutions of the Cauchy momentum equation

    We consider the only axial velocity component u(x,y) along

    positivezdirection in the rectangular microchannel. For a hydro-

    dynamic fully developed pure EOF, the Cauchy momentum equa-

    tion can be simplified to

    l

    @2u

    @x2@2u

    @y2 ! qeE 9

    where qeis the net volume charge density, andl is the fluid viscos-ity. Eq. (9) is subjected to the following no-slip and symmetric

    boundary conditions

    uW;y 0; ux;H 0 10a

    @u0;y@x

    0; @ux;0@y

    0 10b

    Using the following dimensionless steady EOF velocity

    U uUeo

    ; Ueo ekbET0lzve 11

    The normalized form of Eqs. (9)and (10) are

    @2U

    @x2 @

    2U

    @y2 K2 w 12

    Ua; y 0; Ux;1 0; @U0; y@x

    0; @Ux;0@y

    0 13

    Similar to our recent work [13], the solution of Eq. (12) can be

    written as

    Ux; y X1j1

    cosffiffiffiffikj

    p x

    Yjy 14

    where

    Yjy

    A cosh ffiffiffiffikjp y ffiffiffiffi

    kjp

    coshffiffiffiffikj

    p X1

    n1

    QnjJnj

    Fn X1

    m1

    PmjImj

    Em( )

    AX1n1

    Qnj cosh

    ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiK2 c2n

    q y

    cosh ffiffiffiffikjp y

    FnK2 c2n kj

    8>>>:

    X1m1

    Pmj coshffiffiffiffikj

    p y

    cosbmy Emkj b2m

    ) 15a

    A 8aK2f; kj j 1=2pa

    2; j 1;2;3; . . . 15b

    Imjffiffiffiffikj

    pkj

    b2m

    cosh

    ffiffiffiffikjp

    cosbmh i 15c

    Jnjffiffiffiffikj

    pK2 c2n kj

    cosh

    ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiK2 c2n

    q cosh

    ffiffiffiffikj

    p 15d

    Qnj

    a=2 n j1

    2

    1

    cnffiffiffikj

    p sincn

    ffiffiffiffikj

    p a

    1cn ffiffiffikjp sincn ffiffiffiffikjp a

    nj

    8>>>>>>>>>:

    15e

    Pmj 1K2 b2m kjffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiK2 b2m

    q sinh

    ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiK2 b2m

    q a cos

    ffiffiffiffikj

    p a

    ffiffiffiffikjp cosh ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiK2 b2mq a sin ffiffiffiffikjp a 15f

    Fig. 1. Sketch of thermally and hydrodynamically fully developed EOF through a

    rectangular microchannel.

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    2.3. Temperature distribution

    Based on the above velocity field, the energy equation can be

    written as

    qcpu@T

    @z kr2T rE2 lU 16

    whereq is the fluid density,cp is the specific heat at constant pres-sure, Tis the temperature,kis thermal conductivity,ris the electri-cal conductivity, and U is the viscous dissipation function. In Eq.

    (16), the second term in right hand side represents a volumetric

    heat generation due to Joule heating and the third term represents

    a local volumetric heating due to viscous dissipation [9]. For dis-

    tilled water, Gleeson [14]found the ratio of Joule heating to viscous

    heating is very large. Hence, for the present analysis, we neglect the

    viscous heating and consider only the Joule heating effects.

    Assuming the EOF within the rectangular microchannel is ther-

    mally fully developed with constant physical properties, we have

    @

    @z

    Twz Tx;y;zTwz Tmz

    0 17

    whereTw(z) andTm(z) are the local wall and the bulk temperatures,

    respectively. Under imposed constant heat flux boundary condi-

    tions on the wall, we have

    @Tx;y;z@z

    dTmzdz

    dTwzdz

    const: and @2Tx;y;z

    @z2

    0 18Under these situations, energy equation(16)reduces to

    qcpudTmdz

    k @2T

    @x2 @

    2T

    @y2

    ! rE2 19

    The relevant boundary conditions for the energy equation are as

    follows

    @T0;y

    @x 0; q00s k@T

    W;y

    @x 20a

    @Tx;0@y

    0; q00s k@Tx;H

    @y or TjyH Twz 20b

    whereq00s is constant wall heat flux. It should be noted that for the

    thermal fully developed flow in microchannels, usually the wall

    axial thermal conduction cannot be neglected, especially at very

    low Reynolds number. Thus the temperature on the wall is thefunc-

    tion ofz.

    Furthermore, from an overall energy balance for an elemental

    control volume on a length of duct dz, it follows that

    4q00s H Wdz 4rE2HWdz q~uHWcpdTmdz

    dz 21

    where~u is axial mean velocity, and its dimensionless form can be

    written as

    u ~uUeo

    R10

    Ra0Udxdy

    HW 22

    Rearranging Eq. (21), the axial bulk temperature gradient in the

    thermally fully developed situation is

    dTmdz

    q00s H W rE2HW

    mcp23

    Introducing the following dimensionless temperature for fully

    developed flow

    hx;

    y T

    Tw

    q00sH=k 24

    The normalized energy equation may be written as

    @2h

    @x2 @

    2h

    @y2 a1U S 25

    where

    S rE2H

    q00s

    ; a1 H WuW

    Su

    26

    The parameterSdenotes the ratio of Joule heating to wall heat flux

    from rectangular wall. Corresponding normalized temperature

    boundary conditions are

    @h0; y@x

    0; @ha; y@x

    1 27a

    @hx;0@y

    0; @hx;1@y

    1 or hjy1 0 27b

    Similar to our recent work[13], the solution of normalized temper-

    ature of Eq.(25)is

    hx; y X1

    j1

    cos ffiffiffiffikjp xYjy 28

    where theYjy is expressed as

    Yjy C

    1j Pj C2jffiffiffiffikj

    p cosh ffiffiffiffikjp cosh

    ffiffiffiffikj

    p y C

    1j y sinh ffiffiffiffikjp y

    2ffiffiffiffikj

    p Bcosh

    ffiffiffiffikj

    p y 1

    kj Aa1ffiffiffiffi

    kjp X1

    n1

    Qnj

    FnK2 c2n kj

    ffiffiffiffikj

    pK2 c2n kj

    coshffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiK2 c2n

    q y cosh

    ffiffiffiffikj

    p y

    y sinhffiffiffiffikj

    p y

    2

    ! Aa1

    ffiffiffiffikjpX1m1

    Pmj

    Emb2m kj

    y sinhffiffiffiffikj

    p y

    2

    ffiffiffiffikj

    pb2

    m kjcosh

    ffiffiffiffikj

    p y cosbmy

    !29

    where Pj 12sinh

    ffiffiffiffikj

    p ; Sj 1ffiffiffiffi

    kjp cosh ffiffiffiffikjp 1 30a

    Rnjffiffiffiffikj

    pK2 c2n kj

    coshffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiK2 c2n

    q cosh

    ffiffiffiffikj

    p

    12sinh

    ffiffiffiffikj

    p

    30b

    Tmj 12sinh

    ffiffiffiffikj

    p

    ffiffiffiffikj

    pb2m kj

    coshffiffiffiffikj

    p cosbm 30c

    C1j

    a1Affiffiffiffikj

    p cosh ffiffiffiffikjp

    X1n1

    QnjJnjFn

    X1m1

    PmjImjEm

    " # 30d

    C2j a1A

    X1n1

    QnjRnj

    FnK2 c2n kjX1m1

    PmjTmj

    Emb2m kj

    ! BSj 30e

    Finally, the solution ofhx; y can be obtained by inserting Eq.(29)

    into Eq.(28).

    The dimensionless bulk temperature is given by

    hmR10

    Ra0Uhdxdy

    R1

    0

    Ra0Udxdy

    31

    The heat transfer rate can be expressed in terms of Nusselt numberas

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    Nu hDhk

    q00sDhkTw Tm

    1hm

    32a

    where q 00s hTw Tm; hmTm Twq00sH=k

    32b

    whereh is heat transfer coefficient, Dh is so called hydrodynamic

    diameter and Dh= Hfor a square microchannel. The Nusselt number

    obtained in the present study and the one given in previous work

    [15]are in quite agreement.

    3. Numerical results and discussion

    Two dimensionless parameters have been defined above for the

    general flow behavior of thermally fully developed electroosmoticflow through a rectangular microchannel. They are the ratio of the

    characteristic scale of the rectangular microchannel to Debyelength K= Hj, and the ratio of Joule heating to wall heat fluxS rE2H=q00s . The dependence of normalized temperature distribu-tions and Nusselt number on Kand Swill be investigated over their

    relevant ranges in this section. In all computational results, the

    normalized wall zeta potential f 1 in order to use the linearized

    PB equation.

    Firstly, the normalized velocity distributions across the rectan-

    gular microchannel should be computed. For brevity, we ignored

    these similar figures which can be found in Ref. [13]. Based on

    velocity distributions, temperature distributions can be calculated.

    Fig. 2[(a), (c) and (e) forK= 5; (b), (d) and (f) forK = 50] illus-

    trates the three dimensional temperature distributions for differ-

    ent ratioS(5, 0 and 5). Both positive and negative values of the

    wall heat flux are considered, where the negative value of the Scorresponds to fluid cooling scenario, and the positive value of

    Fig. 2. Dimensionless temperature distribution for different ratio S(a= 1). (a)K= 5,S= 5, (b)K= 50,S= 5, (c)K= 5,S= 0, (d)K= 50,S= 0, (e)K= 5,S= 5, (f)K= 50, S= 5.

    6288 J. Su et al. / International Journal of Heat and Mass Transfer 55 (2012) 62856290

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    the Srelates to fluid heating case. From Fig. 2 we can see that a po-sitive value ofS(surface heating) will result in a greater tempera-

    ture variation across the microchannel, while the opposite trend is

    true forS(surface cooling) comparing with the case ofS= 0.

    Moreover, from the form of the surface heat flux q0s= koT(x,H)/

    oy= h(Tw Tm), which requires that the surface temperature gradi-

    ent should be kept constant. Importantly, with an increasing Joule

    heating parameter S, Tw also increases along with Tm in order to

    maintain the constant heat flux condition.

    For small electrokinetic widthK[seeFig. 2(a), (c) and (e)], the

    variations of the amplitude of temperatureh are larger than those

    of large electrokinetic width K[see Fig. 2(b), (d) and (f)]. The reason

    is that when the thickness of the EDL approaches to half height of

    the microchannel, the effects of Joule heating are prominently felt

    almost over the entire channel section, unlike for the case withinfinitesimally thin EDL. These figures clearly demonstrate the

    appreciable change in the local temperature across almost the en-

    tire channel cross section with increasing magnitude of the Sdue

    to appreciable penetration of the EDL into the bulk fluid for small

    K. Moreover, the dependence of temperature on Sis more signifi-

    cant for a small K, while for larger Kthe temperature profiles are

    almost identical.

    Fig. 3 shows fully developed Nusselt number Nuvariations with

    S, a and K. It can be seen from Fig. 3(a) that Nu monotonicallydecreases with increases Swhatever the electrokinetic width Kis

    larger or small. IncreasedKyields the increase of the Nu over the

    rectangular microchannel cross section for a prescribed S. This

    behavior may be explained byFig. 3(b). Increasing values ofSlead

    to higher bulk temperatures with negative sign. This can be ex-plained from Eq. (32) that the larger S produces to higher mean

    temperature with negative sign, which leads to lower values ofNusselt number. In addition,Fig. 3(c) and (d) shows Nu variations

    with electrokinetic width Kfor different ratio a of the width toheight of the channel section for different S(2,2). It can be seen

    thatNu decreases with the increase of width to height ratio a nomatter whetherSis positive or negative.

    4. Conclusions

    This study investigates the velocity and temperature distribu-

    tions of the thermally fully developed electroosmotic flow through

    a rectangular microchannel. Based on linear PB equation, Navier

    Stokes equation and thermally fully developed energy equation,

    analytical solutions of normalized velocity, temperature and Nus-selt number are derived using the method of variable separation.

    They greatly depend on the electrokinetic width K, width to height

    ratioa and Joule heating to heat flux ratio S.By numerical computations, we found that for prescribed K, in-

    creasedSyields greater variation of the temperature over the rect-

    angular microchannel cross section. The dependence of

    temperature on Sis more significant for a smallK, while at a larger

    K the temperature profiles are almost identical. In addition, we

    illustrate theNu number variations with Joule heating to heat flux

    ratioS, width to height ratio a and electrokinetic widthK. TheNunumber monotonically decreases with increases S no matter the

    electrokinetic widthKis larger or small. IncreasedKyields the in-

    crease of theNu number over the rectangular microchannel cross

    section for a given S. Moreover,Nu decreases with the increase ofwidth to height ratioa no matter whetherSis positive or negative.

    Fig. 3. The variations ofNu withS, Kand a.a = 1 for (a) and (b), (c)S= 2, (d) S= 2.

    J. Su et al. / International Journal of Heat and Mass Transfer 55 (2012) 62856290 6289

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    Acknowledgments

    The work was supported by Ph.D. Programs Foundation of Min-

    istry of Education of China (No. 20111501120001), Opening fund of

    State Key Laboratory of Nonlinear Mechanics, the National Natural

    Science Foundation of China (No. 11062005), the Natural Science

    Foundation of Inner Mongolia (Grant No: 2010BS0107), the

    research start up fund for excellent talents at Inner Mongolia Uni-versity (Grant No. Z20080211) and the support of Natural Science

    Key Fund of Inner Mongolia (Grant No: 2009ZD01).

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