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A Thesis
          Submitted to the Faculty of Inha University
           In Partial Fulfillment of the Requirements
                        for the Degree of
        Doctor of Philosophy in Mechanical Engineering
Numerical Analysis and Design Optimization of
Pressure- and Electroosmotically-Driven Liquid
        Flow Microchannel Heat Sinks
                              by
                         Afzal Husain
                   under the supervision of
                   Prof. Kwang-Yong Kim
                Mechanical Engineering Department,
                     Inha University, Korea
                       Nov. 16 & 30, 2009
Microchannel Heat Sink (MCHS)
          • Silicon-based microchannels to be fabricated at the inactive side
            of a chip.
          • Typical dimensions 10mm×10mm
          • Typical number of channels ≈ 100, and Heat flux: q = 100W/cm2
          • Coolant : Deionized Ultra-Filtered (DIUF) Water
                           Air                                            ly
             To       Air heat      Ti
                     Exchanger                lx
                                                        Silicon Channels with
                                                           glass cover plate
    Pump
                                                                                      q
          Liquid                         hc
                    Microchannel                                                lz
                     heat sink     Ti              wc                ww         z
              To                                                                     x
                            q
                                                                                      y

Inha University                                                                           2
Background: MCHS (1)

          • Microchannel heat sink (MCHS) has been proposed as an
            efficient device for electronic cooling, micro-heat exchangers
            and micro-refrigerators etc.
          • Experimental studies have been carried out and low-order
            analytical and numerical models have been developed with
            certain assumptions to understand the heat transfer and fluid
            flow in the MCHS.
          • A full model numerical analysis has been proposed as one of
            the most accurate theoretical techniques available for evaluating
            the performance of the MCHS.
          • The growing demand for higher heat dissipation and
            miniaturization have focused studies to efficiently utilize the
            silicon material, space and to optimize the design of MCHS.
Inha University                                                               3
Background: MCHS (2)

          • Alternative designs other than the smooth MCHS had been
            proposed to enhance the performance of MCHS.
          • The growing demand for higher heat flux has raised issues
            of limiting pumping power at micro-scale.


        Characteristics of
       various micropumps
       (Joshi and Wei 2005)

             Limiting values
       Back pressure < 2 bar
       Flow rate < 35 ml/min

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Motivation (1)

          • For a steady, incompressible and fully developed laminar flow:

                                       hd h                         1
                  Nusselt Number    = = const.
                                    Nu                  and    h∝
                                        k                           dh
                                        d h .∆p
                  Friction factor =f    = const.
                                        2 ρ u 2l x
                                                                            2
                                                                    wc 
                                                                   
                                                   ( f Re) µlx .Q. 1 + 
                                      Re µlx .Q 1
                  Pressure drop ∆p 2 f=                             hc 
                                                                   
                       =                       . 2
                                      wc hc     dh          2 wc 3hc

                          wc                                  ∆p   1
                  For        and Q = const.      we have         ∝ 4
                          hc                                  lx  hc

Inha University                                                                 5
Motivation (2)

          • The lack of studies on systematic optimization of full model
            MCHS which could provide a wide perspective for designers
            and thermal engineers.
          • Although the single objective optimization (SOO) has its
            own advantages, a multi-objective optimization (MOO)
            could be more suitable while dealing with multiple
            constraints and multiple objectives.
          • Three-dimensional full model numerical analyses require
            high computational time and resources therefore surrogate
            models could be applied to microfluidics as well.
          • The limitations with the current state-of-the-art micropumps
            motivated the application of unconventional methods of
            driving fluid through microchannels.
Inha University                                                            6
Objectives

          • To optimize the performance of various designs of MCHSs in
            view of fabrication and flow constraints using gradient based
            as well as evolutionary algorithms.
          • To enhance the performance of the MCHS through passive
            micro-structures applied on the walls of the microchannels.
          • To develop surrogate-based optimization models for the
            application to microfluidics.
          • To apply multi-objective evolutionary algorithm (MOAE)
            coupled with surrogate models to economize optimization
            procedure.
          • To enhance the performance of the MCHSs through
            unconventional pumping methods, e.g., electroosmosis.

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Microchannel Heat Sink
                         Designs



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Rectangular and Trapezoidal MCHS
            A MCHS of 10mm×10mm is set to be characterized and
         optimized for minimum pumping power and thermal resistance at
         constant heat flux.
               Microchannel heat sink
                                                   Design variables
                                                ly
                                                                             θ = wc / hc
                                                                             φ = ww / hc
                    lx         Computational
                                 domain        Cover plate                   η = wb / wc
                         ww                    wc
                                                                           wb = wc    Rect.
   hc                                                        lz
                                                     wb      z            0 < wb < wc Trap.
                  Half pitch                                      x
                                                                      y

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Boundary Conditions

                                                          Outflow

                  Symmetric boundary
          Adiabatic boundaries
                                                           Symmetric boundaries



          Silicon substrate                 q
                                            Heat flux
                                  Inflow


                            Computational domain
                         Half pitch of the microchannel

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Roughened (Ribbed) MCHS

          A roughened (ribbed) MCHS is designed and optimized to
           minimize thermal resistance and pumping power.

    wc = 70 µ m                             Outflow
    ww = 30 µ m
                                                      Design variables
    hc = 400 µ m
                                                        α = hr / wc
                                                        β = wr / hr
                                                        γ = wc / pr


            Inflow                         Computational domain
                                         One of the parallel channels
                           q Heat flux
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Numerical Scheme
                  Pressure-driven Flow (PDF)
                  Electroosmotic Flow (EOF)


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Numerical Scheme PDF (1)

          • Silicon-based MCHS with deionized ultra-filtered (DIUF) water
            as coolant.
          • A steady, incompressible, and laminar flow simulation.
          • Finite-volume analysis of three-dimensional Navier-Stokes and
            energy equations.
          • An overall mesh-system of 401×61×16 was used for a 100µm
            pitch for smooth rectangular MCHS after carrying out grid-
            independency test.
          • A 501×61×41 grid was used for roughened (ribbed) MCHS
            after carrying out grid-independency test.



Inha University                                                          13
Numerical Scheme PDF (2)

            Mathematical Formulation

                   Pumping power        P = Q.∆p = n.uavg . Ac .∆p

                  Global thermal              ∆Tmax
                    resistance          Rth =
                                               qAs

              Maximum temperature      ∆Tmax =Ts ,o − T f ,i
                     rise
                   Fanning friction     Re f = γ
                       factor
                                                     2.α        1
                  Average velocity     uavg   =               .   .P
                                                γµ f (α + 1) n.Lx
                                                            2




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Numerical Scheme EOF
          • Electroosmotic force due to electric field in the presence of
            electric double layer (EDL) can be treated as a body force in
            the Navier-Stokes equations:
                                             (u ⋅∇) ρ u = −∇p + ∇.( µ∇u) + ρe E
          • Poisson-Boltzmann equation:                    2n∞ zb e         zb e 
                                                ∇ψ
                                                =     2
                                                                      sinh  −   ψ
                                                              ε             kbT 
          • Poisson-Boltzmann equation is solved numerically using
            finite volume solver.
          • Linearized Poisson-Boltzmann             ∇ 2ψ = κ 2ψ
            Equation:
          • Linearized Poisson-Boltzmann equation is solved through
            analytical technique:
          • Energy equation:                 u.∇( ρ c pT ) =.(k ∇T ) + E 2 ke
                                                            ∇

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Optimization Procedure



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Single Objective Optimization Technique
                                                 (Problem setup)
              Optimization procedure   Design variables & Objective function


                                             (Design of experiments)
                                             Selection of design points
                  Objective function
                                              (Numerical Analysis)
                                       Determination of the value of objective
                                           function at each design points


                       F = Rth             (Construction of surrogate )
                                          RSA, KRG and RBNN Methods


                                            (Search for optimal point)
                                       Optimal point search from constructed
                     Constraint        surrogate using optimization algorithm



                                                  Is optimal point               No
                                                within design space?
                  Pumping power
                                                           Yes

                                                  Optimal Design

Inha University                                                                       17
Multi-objective Optimization Technique




                   Objective Functions   Rth and P

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Designs for Optimization



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1-Smooth Microchannels
              Design Space: Rectangular and Trapezoidal MCHSs
      • Design points are selected using four-level full factorial design.
                      Design variables      Lower limit     Upper limit
      hc = 400 µ m       wc/hc (=θ )            0.1             0.25
                         ww/hc (=φ )           0.04             0.1

     • Design points are selected using three-level fractional factorial
       design.
                      Design variables Lower limit Upper limit
                         wc/hc (=θ )            0.10            0.35
      hc = 370 µ m
                         ww/hc (=φ )            0.02            0.14
                         wb/wc (=η )            0.50            1.00

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2-Roughened (Ribbed) Microchannel
                  Roughened (ribbed) MCHS with three design variables
                   • Design points are selected using three-level fractional
                     factorial design.

                            Design variables     Lower limit    Upper limit
       wc = 70 µ m
                               hr /wc (=α )          0.3            0.5
       ww = 30 µ m
                               wr /hr (=β)           0.5            2.0
       hc = 400 µ m
                               wc /pr (=γ)          0.056          0.112

                   • Surrogates are constructed using objective function values
                     which are calculated through numerical simulation at each
                     design point defined by Design of Experiments (DOE).
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Numerical Validation



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Numerical Validation PDF (1)
                  • Comparison of numerical simulation results with experimental
                  results of Tuckerman and Pease (1981).
                                       Case1        Case2        Case3
                          wc (µm)        56          55           50
                          ww (µm)        44          45           50
                          hc (µm)       320          287          302
                           h (µm)       533          430          458
                         q (W/cm2)      181          277          790
                         Rth (oC/W)
                                        0.110       0.113        0.090
                         Exp.
                         Rth (oC/W)
                                        0.116       0.105        0.085
                         CFD cal.
                          % Error       5.45         7.08        5.55

Inha University                                                              23
Numerical Validation PDF (2)

           • Comparison of numerically simulated thermal resistances with
             experimental results for smooth MCHS (Kawano et al. 1998).


                                                                 Kawano et al. (1998)
                                        0.5                      Present model
                          Rth,o (K/W)




                                        0.3




                                        0.1

                                              100     200          300           400
                                                            Re


                                              Outlet thermal resistance

Inha University                                                                         24
Numerical Validation EOF

                                      • Validation of present model for pressure driven flow
                                        (PDF) and electroosmotic flow (EOF)

                                                                                                    14
                                                       Arulanandam and Li (2000)
       Volume flow rate (l min )
       -1




                                                       Morini et al. (2006)                                     Morini (1999) slug flow
                                   5E-05               Present model EOF
                                                                                                    12          Present model EOF




                                                                                             Nufd
                                   3E-05                                                            10


                                                                                                     8
                                   1E-05

                                                                                                     6
                                      5E-05   0.0001      0.00015     0.0002       0.00025               0.15      0.2              0.25
                                                           dh (m)                                                   θ

                                                                                     θ = wc / hc

Inha University                                                                                                                            25
Microchannel Heat Sink
                         Analysis



Inha University                            26
Simulation Results PDF (1)
                   Rectangular MCHS:
                   •Variation of thermal resistance with design variables
                    at constant pumping power and heat flux.
                                                                                0.28
                 0.26                                φ = 0.4                                   θ = 0.4
                                                     φ = 0.6                    0.26           θ = 0.6
                                                     φ = 0.8                                   θ = 0.8
                 0.24
                                                     φ = 1.0                    0.24           θ = 1.0




                                                                   Rth (oC/W)
    Rth (oC/W)




                 0.22            θ = wc / hc                                    0.22

                  0.2            φ = ww / hc                                     0.2

                 0.18                                                           0.18

                    0.4   0.5    0.6   0.7   0.8   0.9         1                   0.4   0.5      0.6    0.7   0.8   0.9   1
                                       θ                                                                 φ

                 Variation of thermal resistance                                 Variation of thermal resistance
                       with channel width                                                with fin width
Inha University                                                                                                            27
Simulation Results PDF (2)
          Trapezoidal MCHS: variation of thermal resistance with design
          variables at constant pumping power and heat flux.
                                                                                                                0.32
                                                                             η = 0.5                                                                        η = 0.75
                               0.34                                          φ = 0.02                                                                       φ = 0.02
                                                                             φ = 0.06                                                                       φ = 0.06
                                                                             φ = 0.1                            0.28                                        φ = 0.1
                                0.3




                                                                                                   Rth ( C/W)
                  Rth ( C/W)




                                                                                                                0.24
                  o




                                                                                               o
                               0.26


                               0.22                                                                              0.2


                               0.18
                                                                                                                0.16
                                      0.1   0.15                   0.2             0.25                                 0.1                0.15       0.2         0.25
                                                    θ                                                                                             θ
                                                                0.26                                                          η = 1.0
                                                                                                                              φ = 0.02

                                                                                                                                                      θ = wc / hc
                                                                                                                              φ = 0.06
                                                                0.24                                                          φ = 0.1
                                                   Rth ( C/W)




            hc = 370 µ m                                                                                                                              φ = ww / hc
                                                                0.22
                                                   o




                                                                 0.2


                                                                0.18
                                                                                                                                                      η = wb / wc
                                                                0.16
                                                                       0.1              0.15                      0.2               0.25
                                                                                               θ

Inha University                                                                                                                                                          28
Simulation Results PDF (3)
                                   Roughened (ribbed) MCHS:
                                   • Thermal resistance characteristics with mass flow rate and
                                     pumping power.
                                                  = 0.3, and γ 0.113
                                                         α =
                                    0.2                                                                                                 0.2
                                                                                  0.6
        Thermal resistance (K/W)




                                                                                                            Thermal resistance (K/W)
                                                               β=0.0
                                                                                                                                                                    β=0.0




                                                                                        Pumping power (W)
                                                               β=0.5
                                                                                                                                                                    β=0.5
                                                                                  0.4
                                   0.15                                                                                                0.15


                                                                                  0.2


                                    0.1                                                                                                 0.1
                                                                                  0
                                          2E-05          4E-05            6E-05                                                               0.1        0.3        0.5
                                                  Mass flow rate (kg/s)                                                                             Pumping power (W)


                                                  = h= wr / hr and γ wc / pr
                                                   α r / wc , β =
Inha University                                                                                                                                                             29
Simulation Results EOF

                         • Velocity profiles for PDF, EOF and combined flow
                           (PDF+EOF).

                        1           mixed (PDF+EOF)                            1
                                    EOF
                                    PDF
                       0.8                                                    0.8
             u (ms )




                                                                    u (ms )
            -1




                                                                    -1
                       0.6                                                    0.6
                                                                                           mixed (PDF+EOF)
                                                                                           EOF
                       0.4                                                    0.4          PDF

                       0.2                                                    0.2

                        0                                                      0
                         0    0.1    0.2          0.3   0.4   0.5               0   0.25    0.5      0.75    1
                                           y/wc                                            z/hc




                       = 0.175, ww / hc 0.075 and hc 400 µ m
                       wc / hc = =

Inha University                                                                                                  30
Optimization Results
              Pressure-driven Flow (PDF)



Inha University                            31
Single Objective Optimization PDF (1)

                  Smooth Rectangular MCHS:
                  • Comparison of optimum thermal resistance at constant heat
                    flux and pumping power using Kriging model (KRG) with
                    reference design.
                  • Two design variables consideration.

                                       θ       φ           Rth
                       Models
                                     wc/hc   ww/hc   (CFD calculation)
                   Tuckerman and
                                 0.175 0.138              0.214
                    Pease (1981)
                     Optimized   0.174 0.053              0.171

Inha University                                                             32
Single Objective Optimization PDF (2)

                  Smooth Trapezoidal MCHS:
                  • Optimum thermal resistance using Radial Basis Neural
                    Network (RBNN) model at constant heat flux and pumping
                    power.
                  • Three design variables consideration.
                               θ        φ        η     Rth (Surrogate Rth (CFD
              Model
                             wc/hc    ww/hc    wb/wc        pred.)      cal.)
       Kawano et al.
                     0.154            0.116    1.000        0.1988    0.1922
         (1998)
         Present     0.249            0.036    0.750        0.1708    0.1707


Inha University                                                                33
Single Objective Optimization PDF (3)

                                    Smooth Trapezoidal MCHS:
                                    • Sensitivity of objective function with design variables.

                                   0.02
                                                                 θ                                                                          θ
                                                                 φ                                           0.0012                         φ
                                                                 η




                                                                                     (Rth-Rth,opt)/Rth,opt
                                                                                                                                            η
           (Rth-Rth,opt)/Rth,opt




                                   0.01

                                                                                                             0.0008
                                      0


                                                                                                             0.0004
                                   -0.01


                                                                                                                 0
                                       -10        -5        0         5         10                               -10       -5         0         5         10
                                             Deviation from Optimal Point (%)                                          Deviation from Optimal Point (%)


                                             Kawano et al. (1998)                                                               Optimized
                                               = wc / hc , φ ww / hc= wb / wc
                                                θ =                 and η
Inha University                                                                                                                                                34
Multi-objective Optimization PDF (1)

                  Smooth Rectangular MCHS:
                  • Multiobjective optimization using MOEA and RSA
                    (Response Surface Approximation).

                                                0.16
                                                                             NSGA-II
                     Thermal Resistance (K/W)




                                                           A                 Hybrid method
                                                0.14                         Clusters
                                                                             POC

                                                                                                   Pareto-optimal
                                                0.12
                                                                       B                               Front
                                                 0.1
                                                                                      C

                                                0.08
                                                       0       0.2     0.4      0.6          0.8
                                                               Pumping Power (W)

Inha University                                                                                                     35
Multi-objective Optimization PDF (2)

                  Smooth Trapezoidal MCHS:
                  • Multiobjective optimization using MOEA and RSA.
                  • Pareto-optimal front.

                                      0.15                                                                                                                                                                                                                                      Hybrid method
                                                 x
                                                  x

                                                               7                                                                                                                                                                    x




                                                                                                                                                                                                                                                                                7 Clusters
                                                      x
                                                       x
                                                        x
                                                         x
                                                          x
                                                           x
                                                            x
                                                             x
                                                              x
                                                               x



                                                                                                                                                                                                                                                                                NSGA-II
                                                                xx
                                                                     x




                                                                                                  6
                                                                         x


                                      0.13                                   x
                                                                                 x
                                                                                  x
                          Rth (K/W)




                                                                                      x
                                                                                          x
                                                                                          x

                                                                                              x
                                                                                              x
                                                                                                  x
                                                                                                      x
                                                                                                                                                                                                                                                                                POC
                                                                                                          x
                                                                                                           x
                                                                                                               x
                                                                                                                   x

                                                                                                                       x




                                                                                                                                                     5
                                                                                                                           x
                                                                                                                            x



                                      0.11
                                                                                                                                x
                                                                                                                                 x
                                                                                                                                     x
                                                                                                                                         x
                                                                                                                                             x
                                                                                                                                                 x
                                                                                                                                                     x




                                                                                                                                                                                                          4
                                                                                                                                                         x
                                                                                                                                                             x
                                                                                                                                                                 x
                                                                                                                                                                     x
                                                                                                                                                                         x
                                                                                                                                                                             x
                                                                                                                                                                                 x
                                                                                                                                                                                     x




                                                                                                                                                                                                                                                   3
                                                                                                                                                                                         x
                                                                                                                                                                                             x
                                                                                                                                                                                                 xx
                                                                                                                                                                                                      x
                                                                                                                                                                                                          x x
                                                                                                                                                                                                                x x
                                                                                                                                                                                                                    x
                                                                                                                                                                                                                        x x



                                      0.09                                                                                                                                                                                                                                                         2
                                                                                                                                                                                                                              x x
                                                                                                                                                                                                                                        xx
                                                                                                                                                                                                                                             x x
                                                                                                                                                                                                                                                   xx
                                                                                                                                                                                                                                                        x x




                                                                                                                                                                                                                                                                                                                                 1
                                                                                                                                                                                                                                                            x x
                                                                                                                                                                                                                                                                x x
                                                                                                                                                                                                                                                                    x x
                                                                                                                                                                                                                                                                          xx
                                                                                                                                                                                                                                                                               x x
                                                                                                                                                                                                                                                                                 x
                                                                                                                                                                                                                                                                                     x x
                                                                                                                                                                                                                                                                                           x x
                                                                                                                                                                                                                                                                                               x x
                                                                                                                                                                                                                                                                                                   xx
                                                                                                                                                                                                                                                                                                      x   xx x
                                                                                                                                                                                                                                                                                                               x x x
                                                                                                                                                                                                                                                                                                                       x   x   x x   x   x   x x




                                      0.07
                                             0                                                                                                           0.5                                                                                                        1                                                                1.5
                                                                                                                                                                                                                    P (W)

Inha University                                                                                                                                                                                                                                                                                                                                    36
Multi-objective Optimization PDF (3)

                                Trapezoidal MCHS:
                                • Sensitivity of objective functions to design variables along
                                  Pareto-optimal front.

                           1                                                                      1                                                θ
                                                                                                                                                   φ
                                                                                                                                                   η




                                                                              Design Variables
       Design Variables




                          0.8                                                                    0.8

                          0.6                                         7                          0.6       7

                          0.4                                  6                                 0.4           6

                          0.2                                             θ                      0.2
                                                    5                     φ
                                                                                                                   5                     2
                                 12     3 4                                                                              4      3            1
                           0                                              η                       0

                                 0.08         0.1       0.12       0.14                                0           0.5               1       1.5
                                                Rth (K/W)                                                                    P (W)


                                        = wc / hc , φ ww / hc= wb / wc
                                         θ =                 and η
Inha University                                                                                                                                    37
Multi-objective Optimization PDF (4)

                  Roughened (ribbed) MCHS:
                  • Multiobjective optimization using MOEA and RSA.
                  • Pareto-optimal front.
                                                     0.188
                                                                C
                          Thermal Resistance (K/W)




                                                                                   NSGA-II
                                                     0.184
                                                                                   Hybrid Method
                                                                                   Clusters
                                                                                   POC
                                                      0.18
                                                                             B


                                                     0.176
                                                                                          A


                                                     0.172
                                                             0.04   0.06    0.08    0.1       0.12
                                                                      Pumping Power (W)

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Optimization Results
                  Electroosmotic Flow (EOF)



Inha University                               39
Single Objective Optimization EOF

            • Design variables at different optimal points obtained at various
              values of pumping source for combined flow (PDF+EOF).


                               Ex         θ          φ
                  Δp (kPa)                                  Rth (K/W)
                             (kV/cm)     wc/hc     ww/hc
                    7.5        10        0.250     0.060     0.1865
                    7.5        15        0.250     0.062     0.1799
                    7.5        20        0.250     0.062     0.1776
                     10        10        0.249     0.078     0.1703
                     15        15        0.185     0.066     0.1435



Inha University                                                              40
Multi-objective Optimization EOF

                  • Pareto-optimal front with representative cluster solutions
                    at dp=15kPa and EF=10kV/cm.


                                   0.045                        NSGA-II (PDF+EOF)
                                             A                  Clusters (PDF+EOF)

                                   0.035
                           P (W)




                                                  B
                                   0.025
                                                      C

                                   0.015                             D
                                                                                     E

                                   0.005
                                           0.15           0.2              0.25
                                                          Rth (K/W)




Inha University                                                                          41
Conclusions



Inha University                 42
Conclusions (1)
            • The ratio of microchannel width-to-depth is the most and ratio
              of fin width-to-depth of microchannel is the least sensitive to
              thermal resistance and pumping power.
            • Ribbed MCHS: the application of the rib-structures in the
              MCHSs strongly depends upon the design conditions and
              available pumping source.
            • The prediction of objective function values by the surrogate
              models are close to the numerically calculated values which
              suggests the scope for the surrogate-based optimization
              techniques in microfluidic as well.
            • Surrogate-based optimization techniques can be utilized to
              microfluidic systems to effectively reduce the optimization
              time and expenses.
Inha University                                                              43
Conclusions (2)
            • The Pareto-optimal front obtained through multi-objective
              evolutionary algorithm offers useful trade-offs between
              thermal resistance and pumping power.
            • Multi-objective evolutionary algorithms (MOEA) coupled
              with surrogate models can be applied to economize
              comprehensive optimization problems of microfluidics.
            • The bulk fluid driving force generated by electroosmosis
              can be effectively utilized to assist the existed driving
              source.
            • The thermal resistance of the MCHS can be significantly
              reduced by the application of electric potential in the
              presence of electric double layer (EDL).

Inha University                                                           44
Thanks for your patient listening




Inha University                                       45
Comments and Suggestions




Inha University                              46
Comments and Suggestions
            1. Explanation of various terms in the expression of overall
               thermal resistance.
            2. Correction of Co-ordinate systems for Figures.
            3. Explicit mention of velocity approximate/empirical
               relations.
            4. Repetitive sentences in the model descriptions and results
               and discussion.
            5. Roughened microchannel and ribbed microchannel
            6. Corrections in the Korean Abstract.
            7. There were some formatting mistakes.
            8. Thesis-Title modification.

Inha University                                                             47
Comments and Suggestions
             1. Explanation of various terms of overall thermal resistance:
                  Rth = Rth ,cond + Rth ,conv + Rth ,cal
                   t                   1                   1
     = =
     Rth ,cond            , Rth ,conv   =   and Rth ,cal
               k s l xl y             hA fs              
                                                         mc p f
             2. Co-ordinate system for Figs.

                                                                              x
                                          ly                                                         ly
                                                                                  y

                   lx                                                     z           lx
                                          Cover plate                                                Cover plate




        hc                                                           hc
                                                        lz                                                         lz
                        wc           ww                 z                                  wc   ww
                                                             x
                                                                 y




Inha University                                                                                                         48
Comments and Suggestions
            3(a). The explicit mention about the approximate expression
             used for calculating velocity at constant pumping power for
             rectangular MCHS: Knight et al. (1992) approximated that
                        (θ 2 + 1)
                     G=                          f = 4.70 + 19.64G
                                                   Re
                        (θ + 1) 2
            3(b). Again London and Shah (1978) proposed empirical
             relation
                           f Re = − 1.3553θ + 1.9467θ 2 − 1.7012θ 3
                                 24(1
                                         + 0.9564θ 4 − 0.2537θ 5 )

                                                   2θ          1
                                    uavg =                           P
                                             f Re µ f (θ + 1) nm .lx
                                                             2




Inha University                                                            49
Comments and Suggestions
            4. Repetitive Discussion:
                  The repetitive discussion has been corrected at various
                  locations
            5. Roughened microchannel has been replaced with ribbed
             microchannel.
            6. Formatting Comments:
                   The various formatting mistakes have been corrected.
            7. Abstract in Korean language has been Corrected.




Inha University                                                             50
Comments and Suggestions
    8. Thesis-Title Modification
                                       Original Title
                  Microchannel Heat Sinks: Numerical Analysis and Design
                                       Optimization

                               Modified Titles
    1- Numerical Analysis and Design Optimization of Pressure- and
       Electroosmotically-Driven Liquid Flow Microchannel Heat sinks

    2- Numerical Analysis and Design Optimization of Pressure-Driven
       and Electroosmotic Liquid Flow Microchannel Heat Sinks

    3- Numerical Analysis and Design Optimization of Pressure-Driven
       and Electroosmotic Flow Microchannel Heat Sinks

Inha University                                                            51
Comments and Suggestions


                                Selected Title
         Numerical Analysis and Design Optimization of Pressure- and
         Electroosmotically-Driven Liquid Flow Microchannel Heat sinks




Inha University                                                      52

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Final Phd Defence Presentation

  • 1. A Thesis Submitted to the Faculty of Inha University In Partial Fulfillment of the Requirements for the Degree of Doctor of Philosophy in Mechanical Engineering Numerical Analysis and Design Optimization of Pressure- and Electroosmotically-Driven Liquid Flow Microchannel Heat Sinks by Afzal Husain under the supervision of Prof. Kwang-Yong Kim Mechanical Engineering Department, Inha University, Korea Nov. 16 & 30, 2009
  • 2. Microchannel Heat Sink (MCHS) • Silicon-based microchannels to be fabricated at the inactive side of a chip. • Typical dimensions 10mm×10mm • Typical number of channels ≈ 100, and Heat flux: q = 100W/cm2 • Coolant : Deionized Ultra-Filtered (DIUF) Water Air ly To Air heat Ti Exchanger lx Silicon Channels with glass cover plate Pump q Liquid hc Microchannel lz heat sink Ti wc ww z To x q y Inha University 2
  • 3. Background: MCHS (1) • Microchannel heat sink (MCHS) has been proposed as an efficient device for electronic cooling, micro-heat exchangers and micro-refrigerators etc. • Experimental studies have been carried out and low-order analytical and numerical models have been developed with certain assumptions to understand the heat transfer and fluid flow in the MCHS. • A full model numerical analysis has been proposed as one of the most accurate theoretical techniques available for evaluating the performance of the MCHS. • The growing demand for higher heat dissipation and miniaturization have focused studies to efficiently utilize the silicon material, space and to optimize the design of MCHS. Inha University 3
  • 4. Background: MCHS (2) • Alternative designs other than the smooth MCHS had been proposed to enhance the performance of MCHS. • The growing demand for higher heat flux has raised issues of limiting pumping power at micro-scale. Characteristics of various micropumps (Joshi and Wei 2005) Limiting values Back pressure < 2 bar Flow rate < 35 ml/min Inha University 4
  • 5. Motivation (1) • For a steady, incompressible and fully developed laminar flow: hd h 1 Nusselt Number = = const. Nu and h∝ k dh d h .∆p Friction factor =f = const. 2 ρ u 2l x 2  wc   ( f Re) µlx .Q. 1 +  Re µlx .Q 1 Pressure drop ∆p 2 f=  hc   = . 2 wc hc dh 2 wc 3hc wc ∆p 1 For and Q = const. we have ∝ 4 hc lx hc Inha University 5
  • 6. Motivation (2) • The lack of studies on systematic optimization of full model MCHS which could provide a wide perspective for designers and thermal engineers. • Although the single objective optimization (SOO) has its own advantages, a multi-objective optimization (MOO) could be more suitable while dealing with multiple constraints and multiple objectives. • Three-dimensional full model numerical analyses require high computational time and resources therefore surrogate models could be applied to microfluidics as well. • The limitations with the current state-of-the-art micropumps motivated the application of unconventional methods of driving fluid through microchannels. Inha University 6
  • 7. Objectives • To optimize the performance of various designs of MCHSs in view of fabrication and flow constraints using gradient based as well as evolutionary algorithms. • To enhance the performance of the MCHS through passive micro-structures applied on the walls of the microchannels. • To develop surrogate-based optimization models for the application to microfluidics. • To apply multi-objective evolutionary algorithm (MOAE) coupled with surrogate models to economize optimization procedure. • To enhance the performance of the MCHSs through unconventional pumping methods, e.g., electroosmosis. Inha University 7
  • 8. Microchannel Heat Sink Designs Inha University 8
  • 9. Rectangular and Trapezoidal MCHS A MCHS of 10mm×10mm is set to be characterized and optimized for minimum pumping power and thermal resistance at constant heat flux. Microchannel heat sink Design variables ly θ = wc / hc φ = ww / hc lx Computational domain Cover plate η = wb / wc ww wc wb = wc Rect. hc lz wb z 0 < wb < wc Trap. Half pitch x y Inha University 9
  • 10. Boundary Conditions Outflow Symmetric boundary Adiabatic boundaries Symmetric boundaries Silicon substrate q Heat flux Inflow Computational domain Half pitch of the microchannel Inha University 10
  • 11. Roughened (Ribbed) MCHS A roughened (ribbed) MCHS is designed and optimized to minimize thermal resistance and pumping power. wc = 70 µ m Outflow ww = 30 µ m Design variables hc = 400 µ m α = hr / wc β = wr / hr γ = wc / pr Inflow Computational domain One of the parallel channels q Heat flux Inha University 11
  • 12. Numerical Scheme Pressure-driven Flow (PDF) Electroosmotic Flow (EOF) Inha University 12
  • 13. Numerical Scheme PDF (1) • Silicon-based MCHS with deionized ultra-filtered (DIUF) water as coolant. • A steady, incompressible, and laminar flow simulation. • Finite-volume analysis of three-dimensional Navier-Stokes and energy equations. • An overall mesh-system of 401×61×16 was used for a 100µm pitch for smooth rectangular MCHS after carrying out grid- independency test. • A 501×61×41 grid was used for roughened (ribbed) MCHS after carrying out grid-independency test. Inha University 13
  • 14. Numerical Scheme PDF (2) Mathematical Formulation Pumping power P = Q.∆p = n.uavg . Ac .∆p Global thermal ∆Tmax resistance Rth = qAs Maximum temperature ∆Tmax =Ts ,o − T f ,i rise Fanning friction Re f = γ factor 2.α 1 Average velocity uavg = . .P γµ f (α + 1) n.Lx 2 Inha University 14
  • 15. Numerical Scheme EOF • Electroosmotic force due to electric field in the presence of electric double layer (EDL) can be treated as a body force in the Navier-Stokes equations: (u ⋅∇) ρ u = −∇p + ∇.( µ∇u) + ρe E • Poisson-Boltzmann equation: 2n∞ zb e  zb e  ∇ψ = 2 sinh  − ψ ε  kbT  • Poisson-Boltzmann equation is solved numerically using finite volume solver. • Linearized Poisson-Boltzmann ∇ 2ψ = κ 2ψ Equation: • Linearized Poisson-Boltzmann equation is solved through analytical technique: • Energy equation: u.∇( ρ c pT ) =.(k ∇T ) + E 2 ke ∇ Inha University 15
  • 17. Single Objective Optimization Technique (Problem setup) Optimization procedure Design variables & Objective function (Design of experiments) Selection of design points Objective function (Numerical Analysis) Determination of the value of objective function at each design points F = Rth (Construction of surrogate ) RSA, KRG and RBNN Methods (Search for optimal point) Optimal point search from constructed Constraint surrogate using optimization algorithm Is optimal point No within design space? Pumping power Yes Optimal Design Inha University 17
  • 18. Multi-objective Optimization Technique Objective Functions Rth and P Inha University 18
  • 20. 1-Smooth Microchannels Design Space: Rectangular and Trapezoidal MCHSs • Design points are selected using four-level full factorial design. Design variables Lower limit Upper limit hc = 400 µ m wc/hc (=θ ) 0.1 0.25 ww/hc (=φ ) 0.04 0.1 • Design points are selected using three-level fractional factorial design. Design variables Lower limit Upper limit wc/hc (=θ ) 0.10 0.35 hc = 370 µ m ww/hc (=φ ) 0.02 0.14 wb/wc (=η ) 0.50 1.00 Inha University 20
  • 21. 2-Roughened (Ribbed) Microchannel Roughened (ribbed) MCHS with three design variables • Design points are selected using three-level fractional factorial design. Design variables Lower limit Upper limit wc = 70 µ m hr /wc (=α ) 0.3 0.5 ww = 30 µ m wr /hr (=β) 0.5 2.0 hc = 400 µ m wc /pr (=γ) 0.056 0.112 • Surrogates are constructed using objective function values which are calculated through numerical simulation at each design point defined by Design of Experiments (DOE). Inha University 21
  • 23. Numerical Validation PDF (1) • Comparison of numerical simulation results with experimental results of Tuckerman and Pease (1981). Case1 Case2 Case3 wc (µm) 56 55 50 ww (µm) 44 45 50 hc (µm) 320 287 302 h (µm) 533 430 458 q (W/cm2) 181 277 790 Rth (oC/W) 0.110 0.113 0.090 Exp. Rth (oC/W) 0.116 0.105 0.085 CFD cal. % Error 5.45 7.08 5.55 Inha University 23
  • 24. Numerical Validation PDF (2) • Comparison of numerically simulated thermal resistances with experimental results for smooth MCHS (Kawano et al. 1998). Kawano et al. (1998) 0.5 Present model Rth,o (K/W) 0.3 0.1 100 200 300 400 Re Outlet thermal resistance Inha University 24
  • 25. Numerical Validation EOF • Validation of present model for pressure driven flow (PDF) and electroosmotic flow (EOF) 14 Arulanandam and Li (2000) Volume flow rate (l min ) -1 Morini et al. (2006) Morini (1999) slug flow 5E-05 Present model EOF 12 Present model EOF Nufd 3E-05 10 8 1E-05 6 5E-05 0.0001 0.00015 0.0002 0.00025 0.15 0.2 0.25 dh (m) θ θ = wc / hc Inha University 25
  • 26. Microchannel Heat Sink Analysis Inha University 26
  • 27. Simulation Results PDF (1) Rectangular MCHS: •Variation of thermal resistance with design variables at constant pumping power and heat flux. 0.28 0.26 φ = 0.4 θ = 0.4 φ = 0.6 0.26 θ = 0.6 φ = 0.8 θ = 0.8 0.24 φ = 1.0 0.24 θ = 1.0 Rth (oC/W) Rth (oC/W) 0.22 θ = wc / hc 0.22 0.2 φ = ww / hc 0.2 0.18 0.18 0.4 0.5 0.6 0.7 0.8 0.9 1 0.4 0.5 0.6 0.7 0.8 0.9 1 θ φ Variation of thermal resistance Variation of thermal resistance with channel width with fin width Inha University 27
  • 28. Simulation Results PDF (2) Trapezoidal MCHS: variation of thermal resistance with design variables at constant pumping power and heat flux. 0.32 η = 0.5 η = 0.75 0.34 φ = 0.02 φ = 0.02 φ = 0.06 φ = 0.06 φ = 0.1 0.28 φ = 0.1 0.3 Rth ( C/W) Rth ( C/W) 0.24 o o 0.26 0.22 0.2 0.18 0.16 0.1 0.15 0.2 0.25 0.1 0.15 0.2 0.25 θ θ 0.26 η = 1.0 φ = 0.02 θ = wc / hc φ = 0.06 0.24 φ = 0.1 Rth ( C/W) hc = 370 µ m φ = ww / hc 0.22 o 0.2 0.18 η = wb / wc 0.16 0.1 0.15 0.2 0.25 θ Inha University 28
  • 29. Simulation Results PDF (3) Roughened (ribbed) MCHS: • Thermal resistance characteristics with mass flow rate and pumping power. = 0.3, and γ 0.113 α = 0.2 0.2 0.6 Thermal resistance (K/W) Thermal resistance (K/W) β=0.0 β=0.0 Pumping power (W) β=0.5 β=0.5 0.4 0.15 0.15 0.2 0.1 0.1 0 2E-05 4E-05 6E-05 0.1 0.3 0.5 Mass flow rate (kg/s) Pumping power (W) = h= wr / hr and γ wc / pr α r / wc , β = Inha University 29
  • 30. Simulation Results EOF • Velocity profiles for PDF, EOF and combined flow (PDF+EOF). 1 mixed (PDF+EOF) 1 EOF PDF 0.8 0.8 u (ms ) u (ms ) -1 -1 0.6 0.6 mixed (PDF+EOF) EOF 0.4 0.4 PDF 0.2 0.2 0 0 0 0.1 0.2 0.3 0.4 0.5 0 0.25 0.5 0.75 1 y/wc z/hc = 0.175, ww / hc 0.075 and hc 400 µ m wc / hc = = Inha University 30
  • 31. Optimization Results Pressure-driven Flow (PDF) Inha University 31
  • 32. Single Objective Optimization PDF (1) Smooth Rectangular MCHS: • Comparison of optimum thermal resistance at constant heat flux and pumping power using Kriging model (KRG) with reference design. • Two design variables consideration. θ φ Rth Models wc/hc ww/hc (CFD calculation) Tuckerman and 0.175 0.138 0.214 Pease (1981) Optimized 0.174 0.053 0.171 Inha University 32
  • 33. Single Objective Optimization PDF (2) Smooth Trapezoidal MCHS: • Optimum thermal resistance using Radial Basis Neural Network (RBNN) model at constant heat flux and pumping power. • Three design variables consideration. θ φ η Rth (Surrogate Rth (CFD Model wc/hc ww/hc wb/wc pred.) cal.) Kawano et al. 0.154 0.116 1.000 0.1988 0.1922 (1998) Present 0.249 0.036 0.750 0.1708 0.1707 Inha University 33
  • 34. Single Objective Optimization PDF (3) Smooth Trapezoidal MCHS: • Sensitivity of objective function with design variables. 0.02 θ θ φ 0.0012 φ η (Rth-Rth,opt)/Rth,opt η (Rth-Rth,opt)/Rth,opt 0.01 0.0008 0 0.0004 -0.01 0 -10 -5 0 5 10 -10 -5 0 5 10 Deviation from Optimal Point (%) Deviation from Optimal Point (%) Kawano et al. (1998) Optimized = wc / hc , φ ww / hc= wb / wc θ = and η Inha University 34
  • 35. Multi-objective Optimization PDF (1) Smooth Rectangular MCHS: • Multiobjective optimization using MOEA and RSA (Response Surface Approximation). 0.16 NSGA-II Thermal Resistance (K/W) A Hybrid method 0.14 Clusters POC Pareto-optimal 0.12 B Front 0.1 C 0.08 0 0.2 0.4 0.6 0.8 Pumping Power (W) Inha University 35
  • 36. Multi-objective Optimization PDF (2) Smooth Trapezoidal MCHS: • Multiobjective optimization using MOEA and RSA. • Pareto-optimal front. 0.15 Hybrid method x x 7 x 7 Clusters x x x x x x x x x x NSGA-II xx x 6 x 0.13 x x x Rth (K/W) x x x x x x x POC x x x x x 5 x x 0.11 x x x x x x x 4 x x x x x x x x 3 x x xx x x x x x x x x 0.09 2 x x xx x x xx x x 1 x x x x x x xx x x x x x x x x x xx x xx x x x x x x x x x x x x 0.07 0 0.5 1 1.5 P (W) Inha University 36
  • 37. Multi-objective Optimization PDF (3) Trapezoidal MCHS: • Sensitivity of objective functions to design variables along Pareto-optimal front. 1 1 θ φ η Design Variables Design Variables 0.8 0.8 0.6 7 0.6 7 0.4 6 0.4 6 0.2 θ 0.2 5 φ 5 2 12 3 4 4 3 1 0 η 0 0.08 0.1 0.12 0.14 0 0.5 1 1.5 Rth (K/W) P (W) = wc / hc , φ ww / hc= wb / wc θ = and η Inha University 37
  • 38. Multi-objective Optimization PDF (4) Roughened (ribbed) MCHS: • Multiobjective optimization using MOEA and RSA. • Pareto-optimal front. 0.188 C Thermal Resistance (K/W) NSGA-II 0.184 Hybrid Method Clusters POC 0.18 B 0.176 A 0.172 0.04 0.06 0.08 0.1 0.12 Pumping Power (W) Inha University 38
  • 39. Optimization Results Electroosmotic Flow (EOF) Inha University 39
  • 40. Single Objective Optimization EOF • Design variables at different optimal points obtained at various values of pumping source for combined flow (PDF+EOF). Ex θ φ Δp (kPa) Rth (K/W) (kV/cm) wc/hc ww/hc 7.5 10 0.250 0.060 0.1865 7.5 15 0.250 0.062 0.1799 7.5 20 0.250 0.062 0.1776 10 10 0.249 0.078 0.1703 15 15 0.185 0.066 0.1435 Inha University 40
  • 41. Multi-objective Optimization EOF • Pareto-optimal front with representative cluster solutions at dp=15kPa and EF=10kV/cm. 0.045 NSGA-II (PDF+EOF) A Clusters (PDF+EOF) 0.035 P (W) B 0.025 C 0.015 D E 0.005 0.15 0.2 0.25 Rth (K/W) Inha University 41
  • 43. Conclusions (1) • The ratio of microchannel width-to-depth is the most and ratio of fin width-to-depth of microchannel is the least sensitive to thermal resistance and pumping power. • Ribbed MCHS: the application of the rib-structures in the MCHSs strongly depends upon the design conditions and available pumping source. • The prediction of objective function values by the surrogate models are close to the numerically calculated values which suggests the scope for the surrogate-based optimization techniques in microfluidic as well. • Surrogate-based optimization techniques can be utilized to microfluidic systems to effectively reduce the optimization time and expenses. Inha University 43
  • 44. Conclusions (2) • The Pareto-optimal front obtained through multi-objective evolutionary algorithm offers useful trade-offs between thermal resistance and pumping power. • Multi-objective evolutionary algorithms (MOEA) coupled with surrogate models can be applied to economize comprehensive optimization problems of microfluidics. • The bulk fluid driving force generated by electroosmosis can be effectively utilized to assist the existed driving source. • The thermal resistance of the MCHS can be significantly reduced by the application of electric potential in the presence of electric double layer (EDL). Inha University 44
  • 45. Thanks for your patient listening Inha University 45
  • 47. Comments and Suggestions 1. Explanation of various terms in the expression of overall thermal resistance. 2. Correction of Co-ordinate systems for Figures. 3. Explicit mention of velocity approximate/empirical relations. 4. Repetitive sentences in the model descriptions and results and discussion. 5. Roughened microchannel and ribbed microchannel 6. Corrections in the Korean Abstract. 7. There were some formatting mistakes. 8. Thesis-Title modification. Inha University 47
  • 48. Comments and Suggestions 1. Explanation of various terms of overall thermal resistance: Rth = Rth ,cond + Rth ,conv + Rth ,cal t 1 1 = = Rth ,cond , Rth ,conv = and Rth ,cal k s l xl y hA fs  mc p f 2. Co-ordinate system for Figs. x ly ly y lx z lx Cover plate Cover plate hc hc lz lz wc ww z wc ww x y Inha University 48
  • 49. Comments and Suggestions 3(a). The explicit mention about the approximate expression used for calculating velocity at constant pumping power for rectangular MCHS: Knight et al. (1992) approximated that (θ 2 + 1) G= f = 4.70 + 19.64G Re (θ + 1) 2 3(b). Again London and Shah (1978) proposed empirical relation f Re = − 1.3553θ + 1.9467θ 2 − 1.7012θ 3 24(1 + 0.9564θ 4 − 0.2537θ 5 ) 2θ 1 uavg = P f Re µ f (θ + 1) nm .lx 2 Inha University 49
  • 50. Comments and Suggestions 4. Repetitive Discussion: The repetitive discussion has been corrected at various locations 5. Roughened microchannel has been replaced with ribbed microchannel. 6. Formatting Comments: The various formatting mistakes have been corrected. 7. Abstract in Korean language has been Corrected. Inha University 50
  • 51. Comments and Suggestions 8. Thesis-Title Modification Original Title Microchannel Heat Sinks: Numerical Analysis and Design Optimization Modified Titles 1- Numerical Analysis and Design Optimization of Pressure- and Electroosmotically-Driven Liquid Flow Microchannel Heat sinks 2- Numerical Analysis and Design Optimization of Pressure-Driven and Electroosmotic Liquid Flow Microchannel Heat Sinks 3- Numerical Analysis and Design Optimization of Pressure-Driven and Electroosmotic Flow Microchannel Heat Sinks Inha University 51
  • 52. Comments and Suggestions Selected Title Numerical Analysis and Design Optimization of Pressure- and Electroosmotically-Driven Liquid Flow Microchannel Heat sinks Inha University 52