This document summarizes key concepts in Chapter 12 on temperature distribution with more than one independent variable. It discusses unsteady heat conduction in solids, including heating of a finite slab and cooling of a sphere in contact with a fluid. It also covers steady heat conduction in laminar incompressible flow, including complete and asymptotic solutions, as well as boundary layer theory for non-isothermal flow. Dimensionless variables, differential equations, boundary conditions, and solution methods like separation of variables and Laplace transforms are presented.
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1. Ch t 12 T t di t ib tiChapter 12. Temperature distribution
with more than one independent variablep
U t d h t d ti i lid• Unsteady heat conduction in solids
• Steady heat conduction in laminar,y ,
incompressible flow
• Steady potential flow of heat in solids• Steady potential flow of heat in solids
• Boundary layer theory for non-isothermal
flow
1
Unsteady heat conduction in solidsUnsteady heat conduction in solids
• Energy equation
T
Tk
t
T
Cˆ p
• For constant k
t
• For constant k
T
T 2
t
2
Heating of a finite slabHeating of a finite slab
I i i l T• Initial temperature = To
• T1 wall temperature at t = 01 p
• Dimensionless variables
1 tyTT
2
01 bbTT
2b
3
Heating of a finite slabHeating of a finite slab
• Differential equationq
2
2
• Boundary conditions
10atIC
2b
01at21BC
4
2. Solvingg
• Separation of variables
gf
• Substitution into equation
gf,
• Substitution into equation
2
22
f1gd1f1gd1 2
22
c
f
f
1
d
gd
g
1f
f
1
d
gd
g
1
• Separation into two differential equationsp q
fc
f
gc
gd 2
2
2
5
fcgc
d 2
Solvingg
• Integrating
ccosCcsinBfcexpAg 2
• Temperature distribution
TT
TT1
TT
22n
01
b
y
2
1
ncos
b
t
2
1
nexp
1
1
2 2
22
0n
n
6
b2b2
2
n0n
7 8
3. 9
U t d h t d ti i lidUnsteady heat conduction in solids
• Cooling of a sphere in contact with a well-
stirred fluidstirred fluid
• Fluid temperature, To
• Sphere temperature, T1
• Insulated tank• Insulated tank
• Determine T=T(t)
10
Cooling of a sphere in contact with ag p
well-stirred fluid
i i l i bl• Dimensionless variables
TT
etemperatursolid
TT
TT
),(
o1
s1
s
fl id
TT
)( f1
o1
etemperaturfluid
TT
TT
)(
o1
f1
f
time
t
coordinateradial
r s
11
time
R
coordinateradial
R 2
Equations and BCsEquations and BCs
• Solid Fluid
3d
s2
2
s 1
t 1
sf
B
3
d
d
t
00t
1Bd
1
0,0at s
1,0at f
,1at fs
12finite,0at s
4. Applying Laplace transform method
• Solid Fluid
s21
p s3
1p
2sp
1
f
B
1p
,1at fs
finite,0at s
13
Solution at the Laplace plan (x and p)p p ( p)
• Solid CC 21
pcosh
C
psinh
C 21
s
0C2BCgsinU 2
• Fluid
p3ptanhpBp3
ptanhp11
3
p
1
f
p3ptanhpBp3p
14
Solution at the plane x and tSolution at the plane x and t
• Temperature of the fluid in function of timeTemperature of the fluid in function of time
1 pN fff VCˆ
1
f
pD
pN
L31
spss
fpff
VCˆ
VC
B
2
kbexp
B6
B
p
1k
2
k
2
k
f
bBB19
p
B6
B1
kb3
btanofrootsareb
15
2
k
kk
Bb3
btanofrootsareb
16
5. Steady heat conduction in laminary
incompressible flow
• Laminar tube flow with constant heat
flux at the wall.
– Complete solution by the method of
separation of variables (Ex 12 2-1)separation of variables (Ex 12.2-1)
– Asymptotic solution for short distance
down the tube by the method ofdown the tube by the method of
combination of variable. (Ex 12.2-2)
A i l i f l di– Asymptotic solution for large distances
down of tube. (§10.8)
17
Complete solutionComplete solution
• Using the dimensionless variables (§ 10 8) a• Using the dimensionless variables (§ 10.8) a
solution is proposed
1
1 2
1 2
,,, d
18
Complete solutionp
• The boundary conditions for the dampingy p g
function is
01at00at dd
00at d
• Assumption
0,0at d
ZX,d
19
Complete solutionp
• Separation of variablesSeparation of variables
0X1c
XdXd1
Zc
Zd 22
0X1c
dd
Zc
d
k
2
kk XcexpB,,
1 2
1k
1 22
1
0
2
k
k
d1X0,
B
20
1
0
22
k
k
d1X
6. Asymptotic solution for the entrance region
• Assumptions
– No curvature effects, flat surface. Using y=R-r
– Fluid is a semi-infinite medium
– Linear velocity profile
RPP 2–
L2
RPP
v
R
y
vyv
2
L0
00z
2
2
o
y
T
z
T
R
y
v
• Can be solved by combination of variables
yzR
21
• Can be solved by combination of variables
Boundary layer theory for non-isothermal
flow
C ti it • Continuity
• Motion 0
y
v
x
v yx
TT
vvvv x
2
exx
yx
TTg
yx
v
y
v
x
v x2
xe
e
x
y
x
x
• Energy
2
x
2
2
yxp
vT
k
T
v
T
vCˆ
22
2yxp
yyyx
Von Karman momentum and energy
balances
M t• Momentum
dyvv
x
v
dyvvv
dx
d
y
v
0
xe
e
xex
0
x
dyTTg
xdxy 000y
• Energy
dyTTg
0
x
dyTTvCˆ
d
dT
k xp
23
y
dxy
xp
00y
24
7. Heat transfer in laminar forced convection.
Von Karman integral method
• Velocity and temperature profiles
43
xyfor
yy
2
y
2
v
v
43
x
yyyTT
v
43
xyfor
yy
2
y
2
TT
TT
TTTo
o
xyfor1
TT
and1
v ox
TTTo
25
xyfor1
TT
and1
v o
ox
Results
• Assuming constant xT
g
ratio and with
x
xT
1
x1260
x
v37
x
x4
x
v
180
1
140
3
15
2
x
43
T
26
18014015
lResults
• Equation for
1653 37132 1653
Pr
315
37
180
1
140
3
15
2
• Solving• Solving
3
1
Pr
27