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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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    THE END

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