1-21t
TRANSCRIPT
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CHEE 405 (G)
Process Heat Transfer
Chapter 2: 1-6
Instructor:
William Chirdon, Ph.D.
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Temperature Dependence of
Thermal Conductivity
• Most physical properties are temperature dependent
• Including thermal conductivity
(see Fig. 1-6)• Often fitted to a linear function of T
– No strict scientific basis
– More complicated functions would be possible and more
accurate – Choose a function (constant, linear, other) based on the
available data and the demands of the project
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Temperature Dependence of
Thermal Conductivity
2
10
2
1 )1( :WallD-1For
T
T
x
x T T Ak xq
)1(0 T k k
xT AT k q
)1(0
q = heat flow (W)
k = thermal conductivity (W/m oC)
A = area perpendicular to heat flow (m2)
T = temperature (oC)
x = thickness of wall (m)
)(
2
)( 2
1
2
2120 T T T T
x
Ak q
(Eqn 2-2)
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Multi-Component Systems
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Multi-layer Walls
k a k b k c
xa
x b
xc
q
c
c
b
b
aa
x
T T Ak q
x
T T Ak q
x
T T Ak q
)(
)(
)(
34
23
12
T1 T2 T3 T4
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Multi-layer Walls
c
c
b
b
a
a
x
T T Ak q
x
T T Ak q
x
T T Ak q
)(
)(
)(
34
23
12
41
43
32
21
T T Ak
xq
Ak
xq
Ak
xq
T T Ak
xq
T T Ak
xq
T T Ak
xq
c
c
b
b
a
a
c
c
b
b
a
a
Ak
x
Ak
x
Ak
x
T T q
c
c
b
b
a
a
41
(equation 2-3)
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Multi-layer Wall
n
i
overall
cba
overall
c
c
b
b
a
a
ii
ii
R
T
R R R
T
Ak
x
Ak
x
Ak
x
T T q
Aq
T R
1
41
resistancethermal/
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Multi-layer Wall
n
i
overall
i
slab
ii
ii
R
T q
Ak
x R
Aq
T R
1
/
k a k b k c
xa x b xc
q
T1 T2 T3 T4
R a R b R c
Electrical Analogy
q current
T voltage
R i resistance
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Multi-mode Heat Transfer
n
i
overall
ii
convection
i
slab
ii
i
i
R
T Ah
R
Ak
x R
Aq
T
R
1
1
/
ha k b hc
q
R a R b R c
Co-Current Heat Exchanger
flow flow
T1 T2 T3 T4
solid
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Multi-mode Heat Transfer
n
i
overall
R A
U
T UAq
1
1
ha k b hc
q
R a R b R c
Co-Current Heat Exchanger
flow flowsolid
T1 T2 T3 T4
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Thermal Resistance and R-values
• Conceptually similar, but not interchangeable
• Watch units!
– Thermal Resistance = °C/W
– R-value =
°C m
2
/W
i
i
i
i
k
x R
Ak
x R
value-
resistancethermal
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Cylindrical Heat ExchangerFluid (Ta) Fluid (T b)
wall
oo
io
ii
ba
iowall cylinder
io
oiwall cylinder
ii
ii
AhkL
r r
Ah
T T q
kL
r r R
r r
T T kLq
Aq
T R
1
2
)/ln(1
2
)/ln()/ln(
)(2
/
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Insulated Pipe/Wire
Conduction + Convection
o
io
air i
oo
hr k
r r
T T Lq
Lr A
1)/ln(
)(2
2
r i
r o
h, Tair
How will increasing r o affect
the heat transfer rate?
o
io
air i
hAkL
r r
T T q
1
2
)/ln(
NOTE: Table 2-1 contains
pipe insulation values.
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Critical Insulation Thickness
h
k
r
hr k hr kr hr kr
o
ooooo
11,
11,0
1122
o
io
air i
hr k
r r T T Lq 1)/ln( )(2
r i
r o
h, Tair
01)/ln(
11
)(2
2
2
o
io
ooair i
o
hr k
r r
hr kr T T L
dr
dq
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Critical Insulation Thickness
• If r o < r c, then increasing r o will increase the
heat transfer rate
– Due to the increased surface area for convection
• If r o > r c, then increasing r o will decrease the
heat transfer rate
– Due to conduction through the wall
hk r c
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Composite Wall System (1D Transfer)
a
b
c
d h
f
e g
T1T2
q
R a
R b R g
R d
R e
R c
R f
R h
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Steady State Heat Generation
in a 1-D Slab
0
0
2
2
2
2
dx
T d
k
q
dx
T d
T cq
x
T k
x
dot
dot
1-D Heat Conduction Equation:
Steady-state Assumption:
Steady-state Assumption, no heat generation:
(Note: 3-D and spherical/cylindrical coordinates are in your textbook)
Occurs in nuclear reactors,
electrical resistance, chemical
reactions, (e.g. fresh concrete)
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Steady State Heat Generation
in a 1-D Slab
21
2
2
2
2
0
C xC xk
qT
k
q
dx
T d
dot
dot
Steady-state Assumption:
Eq 2-22a: x = - L
x = + L
x = 0
Define T at x = 0 as T0 , so that C2 = T0
If Tx=+L = Tx=-L , then C1 = 0
2
0 2 x
k
qT T dot
General Solution:
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Steady State Heat Generation
in a 1-D Slab
2
02
xk
qT T dot Eq 2-22a:
x = - L
x = + L
x = 0
If T = Tw
at +/- L, then:
k
q
L
T T dot w
22
0
2
0
0
L
x
T T
T T
w
Eq 2-22b:
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Steady State Heat Generation
in a Cylinder
222
4r R
k
qT T dot
w Eq 2-25a:
r = R
r = 0
2
0
1
R
r
T T
T T
w
wEq 2-26:
r = R
(see your text)
21
2ln
4C r C r
k
qT dot
General Solution: