INT. COMM. HEAT MASSTRANSFER Vol. 15, pp. 203-212, 1988 ©Pergamon Press
MEASUREMENTS OF IN P A R T I A L L Y P O R O U S
NATURAL CONVECTION RECTANGULAR ENCLOSURES
OF A S P E C T
Department
0735-1933/88 $3.00 + .00 . Printed in the United States
plc
RATIO
5
S. B. Sathe and T. W. Tong of M e c h a n i c a l and A e r o s p a c e E n g i n e e r i n g A r i z o n a State U n i v e r s i t y Tempe, AZ 8 5 2 8 7
(Conrmmnicated by J.P. Hartnett and W.J. Minkowycz)
ABSTRACT This paper p r e s e n t s e x p e r i m e n t a l results for s t e a d y - s t a t e natural c o n v e c t i v e heat transfer in p a r t i a l l y porous r e c t a n g u l a r e n c l o s u r e s of aspect ratio 5. A d i a b a t i c and isothermal b o u n d a r y c o n d i t i o n s were imposed for the h o r i z o n t a l and vertical b o u n d a r i e s , respectively. The e n c l o s u r e was d i v i d e d v e r t i c a l l y into a f l u i d - s a t u r a t e d porous region and a f l u i d - f i l l e d region by an i m p e r m e a b l e partition. M e a s u r e m e n t s were c o n d u c t e d for d i f f e r e n t R a y l e i g h numbers, porous m a t e r i a l s and t h i c k n e s s e s of the porous region. The results agreed w i t h an earlier p r e d i c t i o n that heat t r a n s f e r could be m i n i m i z e d by p a r t i a l l y f i l l i n g the e n c l o s u r e with a porous m a t e r i a l rather than f i l l i n g it entirely. A c o r r e l a t i o n has been d e v e l o p e d e x p r e s s i n g the Nusselt number in terms of the g o v e r n i n g parameters.
Introduction Recently, theoretical transfer
Sathe
prediction
[I] e x p e r i m e n t a l l y
of Tong and S u b r a m a n i a n
in a t w o - d i m e n s i o n a l
minimized
as a function
experiment
was
the porous
and fluid
partition.
To date,
results
et al.
conducted
for p a r t i a l l y
partially
of the porous with
regions
porous
region
an e n c l o s u r e separated
porous
enclosures 203
the
[2] that heat enclosure
thickness.
of aspect
by an
there has been very
verified
could be The
ratio
i0 and
impermeable
limited in the
experimental
literature
despite
204
the
S.B. Sathe and T.W. Tong
importance
of s u c h
applications. conducted ratio
Since
objective
for
paper
porous
to m a k e
The m e a s u r e m e n t s and b o t h
commercial
were
Nickel
nickel)
and
distilled
materials
were
chosen
thermal
conductivity medium
(Rc)
R c values
containing
are
a fluid
In a d d i t i o n problem
under Pr,
number
Ra o and
of t h e s e
kef f .
The
arithmetic the
The
mean
experimental
DeWitt
[3].
previously
less
such
for
It is the available
porous
the
porous
one
the
of
These
ratio
conductivity
insulation
test
of the
or a p p r o x i m a t e l y
fluid of the
one.
systems
can be
using
Da,
fraction
in Ref.
S.
I.
of Pr,
Ra,
properties
of the
hot
values
reported
are:
the
Prandtl
The
Rayleigh
definitions
Ha,
Da,
R c and
since
N c and Ha o r e q u i r e
c, kf,
are
for
modified
varied
Da, ~,
A,
Among
independently
of ~ and keff
results
ratio
number
properties:
of t h e s e
parameters
aspect
Darcy
found
temperature runs
the
as the
foam)
medium.
thermal
thermal
thickness
determination
five
than
water
made
(polyurethane
to m a i n t a i n
are Ra,
can be
of t h e m
The
as
material
the d i m e n s i o n l e s s
number
The v a l u e s [i].
(a p o r o u s
distilled
as air.
thermophysical
first
using
to the e f f e c t i v e
to Rc,
the
three
following
in o r d e r
typical
Rayleigh
N a o = R a D a H c. the
of a s p e c t
new measurements
plastic
water
either
parameters
only
performed
consideration
number
Hao,
have
of the E x P e r i m e n t
a foam
with
Such
enclosures
materials.
these
Foametal
saturated
porous
porous
I, the a u t h o r s
literature. Description
fluid,
insulation
of Ref.
partially
two d i f f e r e n t
of this
in t h e r m a l
the p u b l i c a t i o n
measurements
5 using
in the
results
Vol. 15, No. 2
p,
@,
evaluated
and c o l d w a l l s
at
the
for e a c h
in I n c r o p e r a
have been
K and
and
measured
x : 6 . 7 6 x l O -8 m e and k e f f = O . S S 9
of
Vol. 15, No. 2
W/m 2
for
for 24
CONVECTION IN POROUS ~ C L O S U R E S
Nickel
the
foam
plastic.
oC w h e r e a s Two
aspect (lO
ratio
the
same
for
enclosure
m
the
for
For
adjusting
each the
average
are
was plate The heat
entire
the
temperature but
and
earlier
0.2540
(2 in.)
end w a l l s
had b e e n
ratio
from
lO to 5.
This
the
foam plastic.
high,
0.4064
constructed
enclosure
Ra o.
The
was
and h a v e
been
wide. [I]
A smaller
m (16
employed and
m
enclosure
in.)
for the N i c k e l
operation
°C.
investigation
and
for
25
the s a m e
was
m
at
of
with
0.0508
W/m 2
conducted
enclosures
in the
(5 in.)
same
ke~=0.599
~ were
a mean
deep
and
bottom
wide was
smaller
were
conducted
S value,
test
hot
and
temperature
approximately
total
m
for
of the
used
aspect
m2
dimensions,
One
top,
smaller
-7
deep
Foametal
to y i e l d construction
described
of
in d e t a i l s
[1].
1.00.
the
at
(16 in.)
0.1270
The
Measurements
state
m
of the
(l in.)
enclosures
before
were
of d i f f e r e n t
enclosure
was
measurements. measurements
kef f
the m e a s u r e m e n t s
that
and 0 . 0 2 5 4
x=2.369xlO
measurements
employed.
to c h a n g e
used
both
for
0.4064
the w i d t h
doubled was
high,
was
except
those
were
and The
enclosures
in.)
This
Foametal,
205
cold
reached,
the
Nu = Q o d / k f A o
to was
filled
(Th-T c)
for
0.25,
the
different
ambient steady
input
0.50,
to
the
0.75,
Ra w e r e while
hot
made
keeping
temperature. state.
and
It
Once plate
by
the took
steady
heater
and
recorded.
(Nu) the
S=O,
temperatures
reach
were
number
transfer
enclosure
to power
temperatures Nusselt
to
hours
runs
plate
close
8-10
for
was
heat with
defined transfer the
fluid
as
the
by
conduction alone.
ratio
of
the
when
the
Hence:
(1)
206
S.B. Sathe and T.W. Tong
where
Oo
corresponded
plate
heater.
to the
electrical
Results Shown
in T a b l e s
conditions heat Eq.
and
transfer (I).
percent cases
The for
where
tabulated. order
the
are
highest
S=0,
the
and
have been
literature
(shown
difference
when
computer largest with
difference
is 4.2
results
presented
in h e a t 0.25.
for
for
obtained
percent.
from
The
The
For
therefore
are
the
not
included
in
the m e a s u r e m e n t s
are
For
accurate,
some
of
in the
S=0,
of Seki
and 0 . 5 0
the
by
to + 7 . 7
available
S=0.25
the
largest
et al. are
[4]
compared
finite-difference
investigation results
of T o n g
the N i c k e l
was
amount
Foametal
in Fig.
obtained
when
of r e d u c t i o n
[2].
for S=I
The
agree
and S u b r a m a n i a n
increased
from
0.25
transfer
increased
when
S was
is c l e a r
that
heat
Foametal
transfer
thickness.
as s h o w n
1 (a). S was
in h e a t
further
Nickel
at w h i c h
in the e a r l i e r
graphically
transfer The
S was
and
correlations
solution
+2.6
temperatures
those
runs.
[5]
to
9 percent.
The
Heat
reported
hot
test
respectively.
meaningless
with
to the
results
the b o u n d a r y - l a y e r
within
also
program
Ra,
the m e a s u r e m e n t s
The m e a s u r e m e n t s
numerical
to the
of Nu as d e f i n e d
from
the p a r e n t h e s e s ) .
compared
of the
experimental
in t e r m s
ranges
compared
within
the
lowest
cold wall
the
the
the
temperature
supplied
summaries
in Nu r a n g e d
and
To d e m o n s t r a t e
with
all
presented
w e r e made.
is 5 p e r c e n t .
the
R c and Ra o w e r e
The hot
results
for
uncertainties
power
and D i s c u s s i o n
2 are
results
results
the
to s h o w
1 and
Vol. 15, No. 2
Significant increased
transfer
to 0.50, changed
and
in Fig.
became from
zero
are
the
as
to 0.75. 1.00.
as a f u n c t i o n
1 (b)
to
smaller
0.50 to
I are
reduction
from
from 0.75
can be m i n i m i z e d Shown
in T a b l e
It
of the
results
VOI. 15, NO. 2
O3NVEC~ICN IN POROUS ~ X ~ O S U R E S
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N38NITN 1 7 3 8 $ N N
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208
S.B. Sathe and T.W. Tong
Summary
Run
of e x p e r i m e n t a l Nickel Foametal,
Ra
S
Rc
Vol. 15, No. 2
TABLE ] conditions and results A=5, Da=l. O 4 8 x l O -4.
Ra o
Pr
0 0 0 0 0 0 0
O0 O0 O0 O0 O0 O0 O0
0 0 0 1 1 2 2
61 80 95 25 66 30 34
Nu
Th
Tc
(oC)
(°C)
6.79 6.96 6.79 6.68 6.86 6.75 6.70
22.52 22.13 23.33 24.65 24.78 26.90 27.24
19.48 18.05 18.62 18.53 16.44 15.56 15.76
5.98(6.23) a 6.75(6.68) a 6.87(6.94) a 7.67(7.45) a 8.23(8.01) a 8.79(8.68) a 8.99(8.72) a
xlO - s
1 2 3 4 5 6 7
for
8 9 lO ll 12
0.25 0.25 0.25 0.25 0.25
0.79 1.09 1.48 1.91 2.22
0.696 0.695 0.694 0.693 0.693
57.57 79.40 107.62 138.67 161.17
6.78 6.85 7.01 7.li 7.03
23.01 23.40 23.64 24.21 25.41
19.09 17.93 16.06 14.25 13.99
2.72(2.84) 2.95(2.97) 3.15(3.10) 3.25 3.38
13 14 15 16 17
0.50 0.50 0.50 0.50 0.50
0.53 0.97 1.48 1.72 2.03
0.694 0.694 0.694 0.694 0.693
38.32 70.62 107.62 125.10 147.38
6.94 7.00 6.96 6.96 7.13
21.54 22.38 23.86 24.38 24.45
18.86 17.41 16.33 15.62 13.88
1.82(1.83) b 2.08(2.03) 0 2.19(2.25) b 2.31 2.44
18 19 20 21 22
0.75 0.75 0.75 0.75 0.75
0.99 1.36 1.65 2.10 2.38
0.695 0.694 0.693 0.695 0.696
71.89 98.90 I19.83 152.99 173.68
6.86 7.00 7.05 7.11 6.98
23.12 23.35 23.85 24.75 25.97
18.17 16.38 15.33 13.82 13.83
1.85 2.01 2.20 2.38 2.55
23 24 25 26 27 28
1.00 l . O0 l . O0 1.O0 1.O0 1.00
0 I 1 l 1 2
0 0 0 0 0 0
57.33 79.53 102.12 i15.98 117.43 160.97
6.79 6.79 6.71 6.71 6.71 6.85
22.95 23.69 24.82 25.26 25.36 26.17
19.04 18.25 17.95 17.42 17.43 15.11
2.57(2.76) 3.02(3.25) 3.45(3.66) 3.76(3.91) 3.88(3.94) 4.39(4.58)
79 09 40 59 61 21
a Results
from
b Results
obtained
c Results
from
696 696 696 696 696 695
correlation from
the
boundary-layer
for
laminar
computer solution
flow
program [5]
0 b b
c c c c c c
[4] reported
in
Ref.
2
Vol. 15, NO. 2
CONVECgION IN PORfTJS ~ L O S U R E S
Summary
Run
S
209
TABLE 2 of e x p e r i m e n t a l c o n d i t i o n s and r e s u l t s the f o a m p l a s t i c , A=5, D a = 9 . 1 7 5 x l O -s.
Ra
Rc
Ra o
Pr
Th
Tc
(oc)
(oC)
6.15 6.34 6.21 6.15
26.67 27.18 28.58 29.14
23.20 20.24 20.68 20.29
xl0-V
for
Nu
11.41(12.02) 13.29(13.07) 13.89(13.86) 14.13(14.47)
1 2 3 4
0.00 0.00 0.00 0.00
0.87 1.62 1.98 2.29
5 6 7 8
0.25 0.25 0.25 0.25
0.87 1.46 2.00 2.61
1.018 1.018 1.018 1.018
812.9 1364.2 1868.8 2438.7
6.16 6.16 6.21 6.18
26.52 27.72 28.60 29.97
23.05 21.88 20.44 19.45
4.37 5.15 5.95 6.88
9 10 11 12 13
0.50 0.50 0.50 0.50 0.50
0.83 1.39 1.46 1.91 2.62
1.018 1.018 1.018 1.018 1.018
775.5 1298.8 1364.2 1784.7 2448.1
6.16 6.14 6.18 6.18 6.19
26.52 27.69 27.66 28.54 29.90
23.05 22.18 21.74 20.80 19.26
3.69 4.70 4.90 5.43 6.33
14 15 16 17 18 19 20
0.75 0.75 0.75 0.75 0.75 0.75 0.75
0.84 0.85 1.37 1.86 1.95 2.47 2.58
1.018 1.018 1.018 1.018 1.018 1.018 1.018
784.9 794.2 1280.1 1738.0 1822.0 2307.9 2410.7
6.15 6.16 6.13 6.24 6.19 6.21 6.16
26.60 26.51 27.66 28.17 28.59 29.54 29.98
23.23 23.11 22.23 20.51 20.67 19.45 19.62
4.09 4.08 4.71 5.48 5.47 5.95 6.29
21 22 23 24 25 26
1.00 1.00 1.00 1.00 1.00 1.00
0.83 1.38 1.90 1.97 2.61 2.65
1.018 1.018 1.018 1.018 1.018 1.018
775.5 1289.4 1775.3 1840.7 2438.7 2476.1
6.15 6.15 6.19 6.23 6.21 6.22
26.53 27.66 28.45 28.44 29.85 29.90
23.24 22.16 20.72 20.32 19.20 19.02
laminar
flow
a Result
from
correlation correlation
for
b Results
from
for
c Results
from boundary-layer
transition solution
[5]
[4] flow
[4]
a b b b
6.32(6.77) c 7.93(8.68) c 9.37(10.14) c 9.52(10.31) c 10.92(11.79) c 10.84(11.90) c
210
for
S.B. Sathe and T.W. Tong
the
foam plastic.
The
existence
Vol. 15, No. 2
of a m i n i m u m
is e v i d e n t
again. The given
expl
in d e t a i l
Foametal, combined
increase
transfer
in the
because
decrease trends
increased
was
heat
in c o n v e c t i v e
change
transfer
1 (a)
and
the
the
region
(b)
transfer
foam
was
fluid
are
in
heat
plastic,
increased
increase
in the
the
in c o n v e c t i v e
of
been
of N i c k e l
when
heat
as S was
when
in the p o r o u s
in Figs.
for A = I O
In the c a s e
Nu has
case
Nu o c 9 ~ r e d
by the d e c r e a s e
occured
heat
in the
and c o n d u c t i v e
did not
transfer
in
offset
by
region.
consistent
the The
with
those
[I].
A correlation relevant
Basically,
region.
The m i n i m u m
of the m i n i m u m
the m i n i n u m
offset
fluid
displayed
observed
[i,2].
component
Rc=l.
convective
the e x i s t e n c e
in c o n v e c t i v e
region
conductive
for
before
as S was
the p o r o u s
the
~tion
has
governing
been
obtained
parameters.
The
for Nu form
in t e r m s
of the
of the
correlation
is
(2)
Nu = i / C + a o N a o a x f 1 ( S ) + b o R a b l f 2 ( S ) where C = l+S(Nc-l), The
constants
separately software
for
the
components increases
NLIN
They
1/C t e r m
component.
a I,
Nickel
package
respectively. that
a o,
fl(S)
to fit
b o,
RHS
and
the p o r o u s
and
of Eq.
the
and
foam
fluid
the
plastic
in T a b l e s
(2)
terms
= ( l - S b2 ) b3
b 2 and b 3 w e r e
in T a b l e
third
to one,
b I,
the d a t a
given
on the
from zero
a 3,
Foametal
are
The s e c o n d for
a 2,
f2 (S)
: l - ( l - S a 2 ) a3'
3.
It can be
the
regions,
convective
using
I and
represents are
evaluated the
2, verified
the
[2]
conductive
convective
respectively.
component
in the
As S
Vol. 15, NO. 2
C~ION
TABLE 3 in Equation
Constants ao
aI
IN POROUS ~I~CLOSU~
az
211
(2).
aa
bo
b z
b z ........ b.3
Nickel Fosmetal
0.0288
0.9190
0.3000
0.1129
0.~26
0.2884
0.3000
1.2759
foam plastic
0.1314
0.5545
0.2000
0.2294
0.1632
0.2598
0.2000
1.1308
porous fluid and data
region region
(b).
increases
while
decreases.
For Nickel
is 7.2 percent.
the data points
the c o n v e c t i v e
Equation
Foametal,
the
(2)
is p l o t t e d
largest
Eq.
in the
in Figs.
difference
For the foam plastic,
to within
component
(2)
1 (a)
from the
agrees w i t h
7.7 percent. Conclusions
Experimental with
a porous
was 5.
Nickel
porous
medium.
from
zero
minimized
m e d i u m were Foametal
were
of the porous showed
of the porous
partially
The e n c l o s u r e
and a foam p l a s t i c
The results
as a function
for e n c l o s u r e s
performed.
The t h i c k n e s s
to one.
correlation governing
measurements
that heat region
aspect
employed
region
filled ratio
as the
was v a r i e d
transfer
thickness.
has been
developed
expressing
Nu in terms
parameters
including
the porous
region
could be A
of the
thickness.
Acknowledgement The authors National
Science
a@e grateful Foundation
for the support
un~der grant
of this work by the
MEA 86-96062.
References i.
S. B. Sathe, T. W. Tong and M. A. Faruque, AIAA J o u r n a l T h e r m o p h y s i c s and Heat Transfer, i, 260 (1987).
2.
T. W. Tong and E. Subramanian, and Fluid Flow, 7, 3~(1986).
International
Journal
of
of Heat
212
S.B. Sathe and T.W. Tong
Vol. 15, No. 2
Introduction
3.
F. P. I n c r o p e r a and D. P. DeWitt, Transfer, Wiley, New York (1985).
4.
N. Seki, S. F u k u s a k o and H. Mechanics, 84, 695 (1978).
5.
T. W. Tong and E. Subramanian, I n t e r n a t i o n a l and Mass Transfer, 28, 563 (1985).
Inaba,
Journal
to Heat
of Fluid
Journal
of Heat