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Online proceedings - EDA Publishing Association

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7-9 October 2009, Leuven, Belgium<br />

For the simulation of global flow variables, the model from θ ( x)<br />

and<br />

s θ ( x)<br />

are the non-dimensional solid and fluid<br />

f<br />

Bau is used, assuming fully developed laminar flow. This<br />

temperatures; Nu ( α ) is the Nusselt number;<br />

model calculates the non-dimensional mass flow rate m,<br />

α<br />

max<br />

= maxα( x)<br />

is<br />

0≤x≤1<br />

defined relative to the mass flow rate scale<br />

* * * * *<br />

m ( )<br />

0<br />

= hc Δp<br />

ν L . the maximum aspect ratio of the channel; k s is the ratio<br />

*<br />

*<br />

h is the channel’s height;<br />

c<br />

Δ p is the pressure drop over the<br />

between the conductivity of solid and fluid k * s /k * f ; A s and A f<br />

are the areas of the cross-sections of the solid and fluid<br />

*<br />

channels; ν is the kinematic viscosity of the coolant. The<br />

*<br />

region, non-dimensionalized with ( L ) 2<br />

;<br />

* * * *<br />

χ = ( k<br />

dimensionless mass flow m depends on the aspect ratio shape<br />

f<br />

L / c m<br />

) with<br />

0<br />

profile<br />

* *<br />

α ( x ) = wc ( x) h c<br />

along the channel:<br />

c * the fluid heat capacity. The parameter χ is inverse<br />

1<br />

−1<br />

*<br />

proportional to<br />

⎛ 1 (1 + α)²<br />

⎞<br />

Δ p .<br />

m = ⎜ ( ) ⎟<br />

8∫ Po α dx<br />

(1)<br />

³<br />

The three terms in (3) represent respectively the heat<br />

⎝ α<br />

0 ⎠<br />

source, the convective heat transfer from solid wall to the<br />

*<br />

Herein is Po (α ) the Poiseuille number and x = x * L is the coolant and axial conductive heat transfer in the solid wall.<br />

In these equations –using<br />

*'' * *<br />

Q s<br />

hc<br />

k III. OPTIMIZATION PROCEDURE<br />

f<br />

The shape of the channels is optimized with respect to two<br />

dimensionless axial coordinate. For the determination of the<br />

Poiseuille number, following correlation for fully developed<br />

flow is used [10] ( 0 ≤ α ≤1):<br />

Similarly, the three terms in (4) represent convective heat<br />

transfer from solid to coolant, the axial conductive heat<br />

transfer in the coolant and the capacitive heating of the fluid.<br />

2<br />

3<br />

Po ( α ) = 96(1 −1.3553α<br />

+ 1.9467α<br />

−1.7012α<br />

(2)<br />

A constant heat flux correlation for Nu ( α ) is used in the<br />

4<br />

5<br />

+ 0.9564α<br />

− 0.2537α<br />

).<br />

assumption of fully developed flow with three-wall heating<br />

The simulation of the axial temperature profiles introduces [10] ( 0 ≤ α ≤1):<br />

2<br />

3<br />

some differences with the model from Bau. In this model, Nu ( α ) = 8.235(1 −1.883α<br />

+ 3.767α<br />

− 5.814α<br />

(5)<br />

axial temperature distribution is calculated for both the fluid<br />

4 5<br />

+ 5.361α<br />

− 2α<br />

).<br />

and the solid wall region including axial conduction. The set of modeling equations (3)-(4) is solved numerically<br />

Therefore, a set of 2 dimensionless heat transfer equations – using finite volume discretization with appropriate boundary<br />

one for each region– is introduced.<br />

conditions. The fluid inlet has a specified temperature. The<br />

The equation describing heat transfer in the solid wall is:<br />

Nu<br />

( )<br />

( α )( 1+<br />

α )( 2 + α ) fluid outlet and both ends of the solid wall have adiabatic<br />

d ⎛ dθ<br />

s ⎞<br />

α<br />

max<br />

+ w<br />

f<br />

−<br />

⋅ ( θ<br />

s<br />

−θ<br />

f<br />

) + ⎜ks<br />

As<br />

⎟ = 0 boundary conditions.<br />

2α<br />

dx ⎝ dx ⎠<br />

If the axial conduction terms in (3)-(4) are ignored, the<br />

(3) modeling equations of Bau are retrieved. It is recalled in (6):<br />

The heat transfer in the fluid region is described by:<br />

Nu( α )( 1 + α )( 2 + α ) ⎛ 2α<br />

χ ⎞<br />

θ<br />

d ⎛ dθ<br />

f ⎞ m dθ<br />

s<br />

( x)<br />

= ( α + w ) ⎜<br />

+ ⋅ x⎟ (6)<br />

max f<br />

f<br />

⋅ ( θ<br />

s<br />

−θ<br />

f<br />

) + ⎜ A ⎟<br />

f<br />

= ⋅ (4)<br />

⎝ Nu( α )( 1+<br />

α )( 2 + α ) m ⎠<br />

2α<br />

dx<br />

dx<br />

⎝ ⎠ χ dx<br />

objectives. The first objective J consists of the<br />

1<br />

minimization of the wall temperature gradient. This is<br />

formulated as the Euclidian norm of the local wall<br />

temperature gradient dθ s<br />

(x)<br />

:<br />

dx<br />

2<br />

⎛ ⎞<br />

= 1 dθ<br />

s<br />

J ∫ ⎜ ⎟ ( ) 0<br />

⎝ dx<br />

dx<br />

α x ⎠<br />

(7)<br />

The second objective J that is regarded is the<br />

2<br />

minimization of the thermal resistance, which is defined as<br />

the maximum dimensionless wall temperature along the<br />

channel:<br />

J = min maxθ<br />

( )<br />

s<br />

α ( x)<br />

x<br />

(8)<br />

The primary variable describing the shape of the channels<br />

is the aspect ratio profile α (x), which is a dimensionless<br />

representation of the channel width. This shape profile is in<br />

fact a continuous function defined over the entire length of<br />

the channel. Conventional optimization routines are only<br />

suitable for a finite number of variables. Therefore a<br />

Fig. 1: Schematic of the channels cross-section<br />

©<strong>EDA</strong> <strong>Publishing</strong>/THERMINIC 2009 158<br />

ISBN: 978-2-35500-010-2

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