The document discusses heat conduction equations in various coordinate systems and geometries:
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This file contains Introduction to Heat Transfer and Fundamental laws governing heat transfer.
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Lectures on Heat Transfer - Introduction - Applications - Fundamentals - Gove...tmuliya
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This chapter contains:-.
Analytical Methods of two dimensional steady state heat conduction
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This chapter contains:-.
Analytical Methods of two dimensional steady state heat conduction
Finite difference Method application on two dimensional steady state heat conduction.
Finite difference method on irregular shape of a system
The probe type is determined by the measurement task. The selection of the most suitable temperature sensor is made according to the following criteria:
- Measurement range
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Indigenized remote control interface card suitable for MAFI system CCR equipment. Compatible for IDM8000 CCR. Backplane mounted serial and TCP/Ethernet communication module for CCR remote access. IDM 8000 CCR remote control on serial and TCP protocol.
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Indigenized remote control interface card suitable for MAFI system CCR equipment. Compatible for IDM8000 CCR. Backplane mounted serial and TCP/Ethernet communication module for CCR remote access. IDM 8000 CCR remote control on serial and TCP protocol.
Key Features
Indigenized remote control interface card suitable for MAFI system CCR equipment. Compatible for IDM8000 CCR. Backplane mounted serial and TCP/Ethernet communication module for CCR remote access. IDM 8000 CCR remote control on serial and TCP protocol.
• Remote control: Parallel or serial interface
• Compatible with MAFI CCR system
• Copatiable with IDM8000 CCR
• Compatible with Backplane mount serial communication.
• Compatible with commercial and Defence aviation CCR system.
• Remote control system for accessing CCR and allied system over serial or TCP.
• Indigenized local Support/presence in India.
Application
• Remote control: Parallel or serial interface.
• Compatible with MAFI CCR system.
• Compatible with IDM8000 CCR.
• Compatible with Backplane mount serial communication.
• Compatible with commercial and Defence aviation CCR system.
• Remote control system for accessing CCR and allied system over serial or TCP.
• Indigenized local Support/presence in India.
• Easy in configuration using DIP switches.
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Sachpazis:Terzaghi Bearing Capacity Estimation in simple terms with Calculati...
(3) heat conduction equation [compatibility mode]
1. HEAT CONDUCTION EQUATION
Prabal TalukdarPrabal Talukdar
Associate Professor
Department of Mechanical EngineeringDepartment of Mechanical Engineering
IIT Delhi
E-mail: prabal@mech.iitd.ac.inp
2. Heat TransferHeat Transfer
Heat transfer has direction as well as
magnitude, and thus it is a vector quantity
P.Talukdar/Mech-IITD
3. Coordinate SystemCoordinate System
The various distances and angles involved when describing the
location of a point in different coordinate systems
P.Talukdar/Mech-IITD
location of a point in different coordinate systems.
4. Fourier’s law of heat conduction
for one-dimensional heat conduction:
)Watt(
dx
dT
kAQcond −=&
If n is the normal of the isothermal surface at
point P, the rate of heat conduction at that point
can be expressed by Fourier’s law as
The heat transfer vector is
)Watt(
n
T
kAQn
∂
∂
−=&
always normal to an isothermal
surface and can be resolved
into its components like any
other vectorother vector
kQjQiQQ zyxn
r
&
r
&
r
&
r
& ++=
P.Talukdar/Mech-IITD x
T
kAQ xx
∂
∂
−=&
y
T
kAQ yy
∂
∂
−=&
z
T
kAQ zz
∂
∂
−=&
5. Steady versus Transient Heat
Transfer
• The term steady implies noy p
change with time at any point
within the medium, while
transient implies variationtransient implies variation
with time or time dependence.
Therefore, the temperature or
heat flux remains unchanged
with time during steady heat
transfer through a medium atg
any location, although both
quantities may vary from one
location to anotherlocation to another
P.Talukdar/Mech-IITD
6. Multidimensional Heat
Transfer
• Heat transfer problems are also classified as being one-p g
dimensional, two-dimensional, or three-dimensional,
depending on the relative magnitudes of heat transfer rates in
different directions and the level of accuracy desireddifferent directions and the level of accuracy desired
Ex: 1‐D heat transfer:
Heat transfer through the glass of a
i d b id d t bwindow can be considered to be one‐
dimensional since heat transfer through
the glass will occur predominantly in one
direction (the direction normal to the (
surface of the glass) and heat transfer in
other directions (from one side
edge to the other and from the top edge
to the bottom) is negligible
P.Talukdar/Mech-IITD
to the bottom) is negligible
7. Heat GenerationHeat Generation
• A medium through which heat is conducted may involve the
conversion of electrical nuclear or chemical energy into heatconversion of electrical, nuclear, or chemical energy into heat
(or thermal) energy. In heat conduction analysis, such
conversion processes are characterized as heat generation.
• Heat generation is a volumetric phenomenon. That is, it occurs
throughout the body of a medium. Therefore, the rate of heat
generation in a medium is usually specified per unit volumegeneration in a medium is usually specified per unit volume
whose unit is W/m3
The rate of heat generation in a
medium may vary with time as wellmedium may vary with time as well
as position within the medium.
When the variation of heat
generation with position is known,
∫=
V
dVgG && Watt
P.Talukdar/Mech-IITD
g p
the total rate of heat generation in
a medium of volume V can be
determined from
V
8. 1-D Heat Conduction Equationq
Assume the density of the wall is ρ, the specific
heat is C, and the area of the wall normal to the
direction of heat transfer is A.
An energy balance on this thin element during
a small time interval t can be expressed asa small time interval t can be expressed as
EΔ
P.Talukdar/Mech-IITD
t
E
GQQ element
elementxxx
Δ
Δ
=+− Δ+
&&&
9. )TT(x.A.C)TT(mCEEE tttttttttelement −Δρ=−=−=Δ Δ+Δ+Δ+
x.A.gVgG elementelement Δ== &&&
E
GQQ elementΔ
+ &&&
t
GQQ element
elementxxx
Δ
=+− Δ+
)TT(
ACAQQ ttt −
ΔΔ Δ+
&&&
Dividing by
t
)(
x.A.Cx.A.gQQ ttt
xxx
Δ
Δρ=Δ+− Δ+
Δ+
&
TTQQ1 −− &&g y
AΔx gives
t
TT
Cg
x
QQ
A
1 tttxxx
Δ
ρ=+
Δ
− Δ+Δ+
&
Taking the limit as Δx → 0 and Δt → 0 yields and since from Fourier’s Law:
⎟
⎠
⎞
⎜
⎝
⎛
∂
∂
−
∂
∂
=
∂
∂
=
Δ
−Δ+
→Δ x
T
kA
xx
Q
x
QQ xxx
0x
lim
&&&
TT1 ∂⎞⎛ ∂∂
P.Talukdar/Mech-IITD
⎠⎝→Δ 0x
t
T
Cg
x
T
kA
xA
1
∂
∂
ρ=+⎟
⎠
⎞
⎜
⎝
⎛
∂
∂
∂
∂
&
10. Plane wall: A is constant
TT ∂⎞⎛ ∂∂
Variable conductivity:
t
T
Cg
x
T
k
x ∂
∂
ρ=+⎟
⎠
⎞
⎜
⎝
⎛
∂
∂
∂
∂
&
T1gT2
∂∂ &
Constant conductivity:
where the property k/ρC is the thermal
t
T1
k
g
x
T
2
∂
∂
α
=+
∂
∂
diffusivity
P.Talukdar/Mech-IITD
11. Heat Conduction Equation in a
L C li d
C id thi li d i l h ll l t f
Long Cylinder
Consider a thin cylindrical shell element of
thickness r in a long cylinder
The area of the cylinder normal to they
direction of heat transfer at any location is A =
2πrL where r is the value of the radius at that
location. Note that the heat transfer area A
depends on r in this case and thus it varies withdepends on r in this case, and thus it varies with
location.
E lΔ&&&
P.Talukdar/Mech-IITD
t
E
GQQ element
elementrrr
Δ
Δ
=+− Δ+
12. )TT(r.A.C)TT(mCEEE tttttttttelement −Δρ=−=−=Δ Δ+Δ+Δ+
r.A.gVgG elementelement Δ== &&&
)TT( −&&
t
)TT(
r.A.Cr.A.gQQ ttt
rrr
Δ
Δρ=Δ+− Δ+
Δ+
&&&
TTQQ1 &&
dividing by AΔr
gives t
TT
Cg
r
QQ
A
1 tttrrr
Δ
−
ρ=+
Δ
−
− Δ+Δ+
&
⎟
⎞
⎜
⎛ ∂∂∂−Δ+ T
kA
QQQ
li
&&&
⎟
⎠
⎞
⎜
⎝
⎛
∂
∂
−
∂
∂
=
∂
∂
=
Δ
Δ+
→Δ r
T
kA
rr
Q
r
QQ rrr
0r
lim
T
C
T
kA
1 ∂
+⎟
⎞
⎜
⎛ ∂∂
&
P.Talukdar/Mech-IITD
t
Cg
r
kA
rA ∂
ρ=+⎟
⎠
⎞
⎜
⎝
⎛
∂∂
13. Different ExpressionsDifferent Expressions
Variable conductivity:
T
Cg
T
kr
1 ∂
ρ+⎟
⎞
⎜
⎛ ∂∂
&Variable conductivity:
t
Cg
r
.k.r
rr ∂
ρ=+⎟
⎠
⎜
⎝ ∂∂
T1gT1 ∂
⎟
⎞
⎜
⎛ ∂∂ &
Constant Conductivity:
t
T1
k
g
r
T
r
rr
1
∂
∂
α
=+⎟
⎠
⎞
⎜
⎝
⎛
∂
∂
∂
∂
0
gdTd1
⎟
⎞
⎜
⎛ &
0
k
g
rd
r
drr
=+⎟
⎠
⎞
⎜
⎝
⎛
t
T1
r
T
r
rr
1
∂
∂
α
=⎟
⎠
⎞
⎜
⎝
⎛
∂
∂
∂
∂
trrr ∂α⎠⎝ ∂∂
0
rd
dT
r
dr
d
=⎟
⎠
⎞
⎜
⎝
⎛
P.Talukdar/Mech-IITD
14. Heat Conduction Eq in a SphereHeat Conduction Eq. in a Sphere
A = 4πr2
Variable conductivity:
t
T
Cg
r
T
.k.r
rr
1 2
2
∂
∂
ρ=+⎟
⎠
⎞
⎜
⎝
⎛
∂
∂
∂
∂
&
Constant Conductivity:
t
T1
k
g
r
T
r
rr
1 2
2
∂
∂
α
=+⎟
⎠
⎞
⎜
⎝
⎛
∂
∂
∂
∂ &
P.Talukdar/Mech-IITD
Combined One‐Dimensional
Heat Conduction Equation t
T
Cg
r
T
.k.r
rr
1 n
n
∂
∂
ρ=+⎟
⎠
⎞
⎜
⎝
⎛
∂
∂
∂
∂
&
15. General Heat Conduction
E iEquation
E lΔ&&&&&&&
P.Talukdar/Mech-IITD
t
E
GQQQQQQ element
elementzzyyxxzyx
Δ
Δ
=+−−−++ Δ+Δ+Δ+
19. Cylindrical and SphericalCylindrical and Spherical
T
Cg
T
k
T
rk
1T
rk
1 ∂
ρ=+⎟
⎞
⎜
⎛ ∂∂
+⎟⎟
⎞
⎜⎜
⎛ ∂∂
+⎟
⎞
⎜
⎛ ∂∂
&
t
Cg
z
.k
z
r.k
rr
r.k
rr 2
∂
ρ=+⎟
⎠
⎜
⎝ ∂∂
+⎟⎟
⎠
⎜⎜
⎝ φ∂φ∂
+⎟
⎠
⎜
⎝ ∂∂
T
Cg
T
sink
1T
k
1T
rk
1 2 ∂
ρ=+⎟
⎞
⎜
⎛ ∂
θ
∂
+⎟⎟
⎞
⎜⎜
⎛ ∂∂
+⎟
⎞
⎜
⎛ ∂∂
&
P.Talukdar/Mech-IITD
t
Cgsin.k
sinr
k
sinrr
r.k
rr 2222
∂
ρ=+⎟
⎠
⎜
⎝ θ∂
θ
θ∂θ
+⎟⎟
⎠
⎜⎜
⎝ φ∂φ∂θ
+⎟
⎠
⎜
⎝ ∂∂
20. Boundary and Initial Conditions
• The temperature distribution in a medium depends on the
conditions at the boundaries of the medium as well as the heat
transfer mechanism inside the medium. To describe a heat
transfer problem completely, two boundary conditions must be
given for each direction of the coordinate system along whichgiven for each direction of the coordinate system along which
heat transfer is significant.
Th f d ifTherefore, we need to specify two
boundary conditions for one-dimensional
problems, four boundary conditions for
two dimensional problems and sixtwo-dimensional problems, and six
boundary conditions for three-dimensional
problems
P.Talukdar/Mech-IITD
21. • A diti hi h i ll ifi d t ti t 0 i ll d• A condition, which is usually specified at time t = 0, is called
the initial condition, which is a mathematical expression for
the temperature distribution of the medium initially.
)z,y,x(f)0,z,y,x(T =
• Note that under steady conditions, the heat conduction
equation does not involve any time derivatives, and thus we do
not need to specify an initial conditionp y
The heat conduction equation is first order in time, and thus the initial
condition cannot involve any derivatives (it is limited to a specified
temperature).
However, the heat conduction equation is second order in space
coordinates, and thus a boundary condition may involve first
d i ti t th b d i ll ifi d l f t t
P.Talukdar/Mech-IITD
derivatives at the boundaries as well as specified values of temperature
22. Specified Temperature Boundary
C di iCondition
The temperature of an exposed surface can
usually be measured directly and easily.
Therefore, one of the easiest ways toy
specify the thermal conditions on a surface
is to specify the temperature. For one-
dimensional heat transfer through a plane
wall of thickness L, for example, the
specified temperature boundary conditions
can be expressed as
1T)t,0(T =
2T)t,L(T =
P.Talukdar/Mech-IITD
2)(
23. Specified Heat Flux Boundary
C di iCondition
The sign of the specified heat flux isThe sign of the specified heat flux is
determined by inspection: positive if
the heat flux is in the positive
direction of the coordinate a is anddirection of the coordinate axis, and
negative if it is in the opposite
direction.
Note that it is extremely important to
have the correct sign for the specifiedhave the correct sign for the specified
heat flux since the wrong sign will
invert the direction of heat transfer
and cause the heat gain to be
P.Talukdar/Mech-IITD
and cause the heat gain to be
interpreted as heat loss
24. For a plate of thickness L subjected to heat flux of 50 W/m2 into theFor a plate of thickness L subjected to heat flux of 50 W/m into the
medium from both sides, for example, the specified heat flux boundary
conditions can be expressed as
50
x
)t,0(T
k =
∂
∂
− 50
x
)t,L(T
k −=
∂
∂
−and
Special Case: Insulated Boundary
0
x
)t,0(T
k =
∂
∂
0
x
)t,0(T
=
∂
∂or
P.Talukdar/Mech-IITD
25. Another Special CaseAnother Special Case
• Thermal SymmetryThermal Symmetry
t,
2
L
T ⎟
⎠
⎞
⎜
⎝
⎛
∂
0
x
2
=
∂
⎠⎝
PTalukdar/Mech-IITD