Video Lecture
Transcript of Video Lecture
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Video Lectures for MBA
By:
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Appendices 10.A & 10.B:
An Educational Presentation
Presented By:
Joseph Ash
Jordan BaldwinJustin Hirt
Andrea Lance
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History of Heat Conduction
Jean Baptiste Biot
(1774-1862)
French Physicist
Worked on analysis ofheat conduction
Unsuccessful at dealing
with the problem of
incorporating external
convection effects in heatconduction analysis
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History of Heat Conduction
Jean Baptiste Joseph Fourier
(17681830)
Read Biots work
1807 determined how to solve theproblem
Fouriers Law
Time rate of heat flow (Q) through a
slab is proportional to the gradient of
temperature difference
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History of Heat Conduction
Ernst Schmidt
German scientist
Pioneer in EngineeringThermodynamics
Published paper Graphical DifferenceMethod for Unsteady Heat Conduction
First to measure velocity andtemperature field in free convectionboundary layer and large heat transfercoefficients
Schmidt Number Analogy between heat and mass
transfer that causes a dimensionless
quantity
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Derivation of the Heat
Conduction Equation
A first approximation of the equations
that govern the conduction of heat in asolid rod.
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Consider the following:
A uniform rod is insulated on both lateral
ends.
Heat can now only flow in the axial direction.
It is proven that heat per unit time will pass
from the warmer section to the cooler one.
The amount of heat is proportional to the
area, A, and to the temperature differenceT2-T1, and is inversely proportional to the
separation distance, d.
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The final consideration can be expressed as the
following:
is a proportionality factor called the thermal
conductivity and is determined by material properties
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Assumptions
The bar has a length L so x=0 and x=L
Perfectly insulated
Temperature, u, depends onlyon position, x,
and time, t
Usually valid when the lateral dimensions are
small compared to the total length.
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The differential equation governing
the temperature of the bar is a
physical balance between two rates:
Flux/Flow term
Absorption term
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Flux
The instantaneous rate of heat transfer from left to
right across the cross sections x=x0where x0 is
arbitrary can be defined as:
The negative is needed in order to show a positive
rate from left to right (hot to cold)
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Flux
Similarly, the instantaneous rate of heat transfer
from right to left across the cross section x=x0+x
wherex is small can be defined as:
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Flux
The amount of heat entering the bar in a time span
oft is found by subtracting the previous two
equations and then multiplying the result byt:
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Heat Absorption
The average change in temperature,u, can be
written in terms of the heat introduced, Qt and
the massm of the element as:
where s = specific heat of the material= density
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Heat Absorption
The actual temperature change of the bar is simply
the actual change in temperature at some
intermediate point, so the above equation can also
be written as:
This is the heat absorption equation.
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Heat Equation
Equating the Qt in the flux and absorption
terms, we find the heat absorption equation to
be:
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If we divide the above equation byxt and allow
bothx andt to both go to 0, we will obtain the
heat conductionor diffusion equation:
where
and has the dimensions of length^2/time and calledthe thermal diffusivity
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Boundary Conditions
Certain boundary conditions may apply to the
specific heat conduction problem, for
example:
If one end is maintained at some constanttemperature value, then the boundary condition
for that end is u = T.
If one end is perfectly insulated, then the
boundary condition stipulates ux= 0.
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Generalized Boundary Conditions
Consider the end where x=0 and the rate of flow ofheat is proportional to the temperature at the end ofthe bar. Recall that the rate of flow will be given, from left to right, as
With this said, the rate of heat flow out of the bar from right toleft will be
Therefore, the boundary condition at x=0 iswhere h1is a proportionality constant
if h1=0, then it corresponds to an insulated end
if h1goes to infinity, then the end is held at 0 temp.
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Generalized Boundary Conditions
Similarly, if heat flow occurs at the end x = L, then the
boundary condition is as follows:
where, again, h2is a nonzero proportionality
factor
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Initial Boundary Condition
Finally, the temperature distribution at one
fixed instantusually taken at t = 0, takes the
form:
occurring throughout the bar
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Generalizations
Sometimes, the thermal conductivity, density,
specific heat, or area may change as the axial
position changes. The rate of heat transfer under
such conditions at x=x0is now:
The heat equation then becomes a partial
differential equation in the form:
or
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Generalizations
Other ways for heat to enter or leave a bar must
also be taken into consideration.
Assume G(x,t,u) is a rate per unit per time.
Source G(x,t,u) is added to the bar
G(x,t,u) is positive, non-zero, linear, and u does not depend on t
G(x,t,u) must be added to the left side of the heat equation
yielding the following differential equation
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Generalizations
Similarly,
Sink
G(x,t,u) is subtracted from the bar
G(x,t,u) is positive, non-zero, linear, and u does notdepend on t
G(x,t,u) then under this sink condition takes the
form:
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Generalizations
Putting the source and sink equations together
in the heat equation yields
which is commonly called the generalized
heat conduction equation
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Multi-dimensional space
Now consider a bar in which the temperature is
a function of more than just the axial x-
direction. Then the heat conduction equation
can then be written: 2-D:
3-D:
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Example 1: Section 10.6, Problem 9
Let an aluminum rod of length 20 cm be initially
at the uniform temperature 25C. Suppose that
at time t=0, the end x=0 is cooled to 0C while
the end x=20 is heated to 60C, and both arethereafter maintained at those temperatures.
Find the temperature distribution in
the rod at any time t
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Example 1: Section 10.6, Problem 9
Find the temperature distribution, u(x,t)
2uxx=ut, 0
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Example 1: Section 10.6, Problem 9
Using Equations 16 and 17 found on page 614, we
find that
where
1112 sin,
2
222
n
L
tn
nL
xn
ecTL
x
TTtxu
L
n dxL
xn
TL
x
TTxfLc 0 112 sin
2
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Example 1: Section 10.6, Problem 9
Evaluating cn, we find that
n
nc
n
nnnnc
dxxnx
c
n
n
L
n
50cos70
5sin12cos71020
sin0
20
06025
20
2
2
0
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Example 1: Section 10.6, Problem 9
Now we can solve for u(x,t)
1
400
86.0
1
20
86.0
20sin
50cos703,
20
sin50cos70
0
20
060,
2
2
222
n
tn
n
tn
xne
n
nxtxu
xne
n
nxtxu
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Example 1: Section 10.6, Problem 9
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Derivation of the Wave Equation
Applicable for:
One space dimension, transverse vibrations on elastic string
Endpoints atx= 0 andx= L along thex-axis
Set in motion at t= 0 and then left undisturbed
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Schematic of String in Tension
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Equation Derivation
Since there is no acceleration in the horizontal direction
However the vertical components must satisfy
where is the coordinate to the center of mass and the
weight is neglected
Replacing Twith Vthe and rearranging the equation becomes
0cos),()cos(),( txTtxxT
),(sin),()sin(),( txxutxTtxxT tt x
),(),(),(
txux
txVtxxVtt
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Derivation continued
Letting , the equation becomes
To express this in terms of only terms of uwe note that
The resulting equation in terms of uis
and since H(t)is not dependant onxthe resulting equation is
0x
),(),( txutxV ttx
),()(tan)(),( txutHtHtxV x
ttxx uHu )(
ttxx uHu
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DerivationContinued
For small motions of the string, it is approximated that
using the substitution that
the wave equation takes its customary form of
TTH cos
/2 Ta
ttxx
uua 2
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Wave Equation Generalizations
The telegraph equation
where cand kare nonnegative constants
cut arises from a viscous damping force
kuarises from an elastic restoring forceF(x,t)arises from an external force
The differences between this telegraph equation and the customary
wave equation are due to the consideration of internal elastic
forces. This equation also governs flow of voltage or current in a
transmission line, where the coefficients are related to the electrical
parameters in the line.
),(2 txFuakucuuxxttt
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Wave Equations in Additional Dimensions
For a vibrating system with more than on significant space
coordinate it may be necessary to consider the wave equation in
more than one dimension.
For two dimensions the wave equation becomes
For three dimensions the wave equation becomes
ttyyxx uuua )(2
ttzzyyxx uuuua )(2
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Example 2: Section 10.7, Problem 6
Consider an elastic string of length L whose ends
are held fixed. The string is set in motion from
its equilibrium position with an initial velocity
g(x). Let L=10 and a=1. Find the stringdisplacement for any time t.
,4
,1
,4
L
xL
L
x
xg
LxL
Lx
L
Lx
4
34
3
4
40
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Example 2: Section 10.7, Problem 6
From equations 35 and 36 on page 631, we find
that
where
1
sinsin,n
n L
atn
L
xnktxu
L
n dxL
xnxgLkL
an
0 sin2
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Example 2: Section 10.7, Problem 6
Solving for kn, we find:
4sin
4
3sin
8
sin4
sin4
3sin
42
sin4
sinsin42
3
2
4
0
4
3
4 4
3
nn
na
Lk
nnn
n
L
ank
dx
L
xn
L
xLdx
L
xndx
L
xn
L
x
L
k
L
an
n
n
L L
L
L
Ln
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Example 2: Section 10.7, Problem 6
Now we can solve for u(x,t)
1 33
133
1
3
10sin
10sin
4sin
4
3sin
180,
sinsin4
sin4
3sin
18,
sinsin4
sin4
3sin
8,
n
n
n
tnxnnn
ntxu
L
atn
L
xnnn
n
Ltxu
L
atn
L
xnnn
na
Ltxu
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