The microtube heat transfer and fluid flow of dielectric fluids.
Lelea, Dorin ; Cioabla, Adrian ; Laza, Ioan 等
1. INTRODUCTION
Micro Thermal Systems (MTS) (Nishio, 2003), defined as the systems
in which the key size has a length scale of a micrometer, could attain
the high heat transfer coefficients. For instance, they are used as the
cooling devices for LSI chips. On the other hand [mu]--TAS (Micro Total
Chemical Analyzing System), MEMS (Micro Electric--Mechanical Systems) or
bio --chips are some of the examples of MTS. The research reports in
this field, concerning the thermal and hydrodynamic results, are mostly
oriented to the water as a working fluid. However in defense electronics
applications, like radars, lasers or avionics the dielectric fluids are
used due to a sensibility of the operating conditions.
(Morini, 2004) has also presented the review on a single phase
microchannel heat transfer, indicated some of the reasons for a large
dispersion of the experimental results. Both gas and liquid flows have
been considered.
In the recent years, (Lelea et al., 2004), have made the
experimental research on microtube heat transfer and fluid flow with
inner diameters between 100 and 500 pm for laminar regime of the water
flow. These results have shown the good agreement with the conventional
theories even for the entrance region of the tube.
(Lee et al., 2005) have investigated the laminar fluid flow of the
water through the multichannel configuration of the rectangular
cross-section with a hydraulic diameter from 318 to 903 pm. Their
experimental and numerical results shown that, classical continuum
theory can be applied for microchannels, considered in their study. On
the other hand, the entrance and boundary effects have to be carefully
analyzed in the case of theoretical approach.
The outcome of the research reports mentioned above, is that
special attention has to be paid to macroscale phenomena that are
amplified at the microscale. For example, due to a high heat transfer
rate, the temperature variable fluid properties have to be considered.
(Lelea, 2005) has investigated the influence of the temperature
dependent fluid viscosity on Po number. On the other hand, the small
diameter and large length of the tube can result in viscous heating even
in the case of liquid flow, as presented in (Koo & Kleinstreuer,
2004).
Most of the research results have the water as the working fluids.
Due to the sensibility of some specific electronic devices, water might
not be a suitable fluid, so the dielectric fluids must be used. In the
present research the dielectric fluid Novec-7600 is used for
calculations.
2. NUMERICAL DETAILS
In order to discuss the axial conduction influence, the velocity
and temperature distributions were numerically solved taking into
account the temperature variation of the fluid properties, procedure
described in (Lelea et al., 2004).
The computational domain is presented in Fig. 1, as follows: The
fluid flow domain defined at r = 0, [R.sub.i] and z = 0, L; The
temperature field domain defined at r= 0, [R.sub.o] and z=0, L.
The outer portion of the tube has two parts, the heated and
insulated part. So, as shown in Fig. 2, the respective insulated part
was included in the numerical domain. The following set of partial
differential equations is used to describe the phenomena, taking into
account the variable thermophysical properties of the dielectric fluid.
Continuity equation, momentum and energy equations are as follows:
[partial derivative]([rho](T)x u)/[partial derivative]z + 1/4
[partial derivative](r * [rho](T) x v)/[partial derivative]r = 0 (1)
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII]. (2)
[1/r [partial derivative]/[partial derivative]r(k(T) x r [partial
derivative]T/[partial derivative]r) + [partial derivative]/[partial
derivative]z(k(T)[partial derivative]T/[partial derivative]z)] (3)
At the inlet of the tube, the uniform velocity and temperature
field is considered, while at the exit the temperature gradient is equal
to zero. The boundary conditions are
z = 0, 0 < r < [R.sub.o] : u = [u.sub.0], T = [T.sub.w] =
[T.sub.0] (4)
0 < z < [L.sub.tot] :r = 0, [partial derivative]u/[partial
derivative]r = 0, v = 0 r = [R.sub.i], u = v = 0 (5)
The Joule heating of the tube wall can be expressed either by the
uniform heat generation through the tube wall or by the uniform heat
flux imposed on the outer surface of the wall. For the latter case, the
boundary condition is defined as,
[FIGURE 1 OMITTED]
R = [R.sub.o] : [q.sub.o] = [k.sub.s] [partial
derivative]T/[partial derivative]r (for the heated portion of the tube)
(6)
[k.sub.s] [partial derivative]T/[partial derivative]r = 0 (for the
insulated portion of the tube) (7)
where [q.sub.o] is the heat flux based on the outer heat transfer
area of the tube wall.
Z = [L.sub.tot] 0 < r < [R.sub.o]: [partial
derivative]T/[partial derivative]z = 0 (8)
where qo is the heat flux based on the outer heat transfer area of
the tube wall.
R = [R.sub.I] : [T.sub.S][absolute value of Ri+ = [T.sub.f]]Ri- (9)
[k.sub.s][([partial derivative][T.sub.s]/[partial
derivative]r).sub.Ri+] = [k.sub.f][([partial
derivative][T.sub.f]/[partial derivative]r).sub.Ri-] (10)
The fluid properties of the Novec-7600 were considered as
temperature dependent with following equations (3M Engineering fluids,
2008): Dynamic viscosity, density, thermal conductivity and specific
heat are:
[mu](t) = (1587.5-1.755 x t) x [10.sup.-6] * e 464.403382/t+133
2.881482 (11)
[rho](t) = 1587.5-1.755 x t (12)
k(t) = 0.078-0.0003 x t (13)
[c.sub.p](t) = 3.1631 x t+1240.2 (14)
The partial differential equations (1)-(3) together with boundary
conditions, are solved using the finite volume method described in
(Patankar, 1980). First, the parabolic flow field condition is
considered and the velocity field is solved. The temperature field, as a
conjugate heat transfer problem, was then solved as the elliptic problem
using the obtained velocity field. As a consequence of the temperature
dependent fluid properties, iterative procedure is needed to obtain the
convergence of the fluid properties (viscosity, thermal conductivity,
density and specific heat capacity) through the successive solution of
the flow and temperature field. Further details regarding the numerical
code are presented in (Lelea, 2007).
3. RESULTS AND CONCLUSIONS
The microtube conjugate heat transfer analysis was made for two
values of the wall thickness [D.sub.i]/[D.sub.o] = 125.4/300 /an and
silicon substrate (k = 198 W/m K). In order to investigate the axial
conduction behavior in the tube wall, the low Re range was considered Re
< 800. The input heat transfer rate was constant for all the runs
[Q.sub.0] = 0.75 W.
[FIGURE 2 OMITTED]
[FIGURE 3 OMITTED]
The following outcomes might be emphasize from the results
presented in the Figs. 2 and 3:
Due to the poor fluid properties of the Novec-7600 the wall and
bulk temperatures are higher for both cases. For u=0.5 m/s and
Novec-7600 [T.sub.w,max]=94 [degrees]C and [DELTA]T=17 [degrees]C and
for water [T.sub.wmax]=67 [degrees]C and [DELTA]T=3 [degrees]C. If u=6
m/s and Novec-7600 [T.sub.wmax]=43 [degrees]C and [DELTA]T=13[degrees]C
while for the water [T.sub.wmax]=29[degrees]C and [DELTA]T=2[degrees]C.
Despite the large temperature difference and higher maximum wall
temperature, microchannel heat transfer might be a good candidate for
heat dispersion of dielectric fluids.
4. ACKNOWLEDGEMENTS
This work has been financially supported by the Romanian National
University Research Council (CNCSIS) and Ministry of Education and
Research of Romania, grant nr. 670/2009.
5. REFERENCES
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*** (2008) www.3M.com/electronics--3M[TM] Novec[TM] 7600 Engineered
Fluid, 3M Electronics Markets Materials Division, Accessed on:
2009-05-15