Lecture Week 4 1

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    ME 3345 Heat Transfer

    Objective:

    Introduction To Steady State 2-D Heat Transfer

    Numerical Solutions to Multidimensional Heat

    Transfer

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    2

    2

    1T T

    tx

    2-D and Transient Heat Conduction Equations

    How can we solve this equation, given 4 B.C.s?

    How can we solve this equation, given

    2 B.C.s and the initial condition?

    ( , )T x y

    ( , )T x t

    Partial differential equations

    Parabolic equation

    LaPlace Equation (special form of Poisson Equations)

    Chapter 4

    Chapter 5

    2 2

    2 2 0

    T T

    x y

    T2

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    1. Exact solutions or analytical solutions

    - can only be obtained for limited cases with regular B.C.s

    - complicated functions and series are involved

    - serve as a tool to verify numerical solutions

    - excellent sources of analytical solutions in many found in

    many texts: (e.g., Carslaw and Jaeger, Conduction of

    Heat in Solids, 1959)

    2. Graphical methods- physically intuitive and tedious

    - limited use for simple geometries only

    - Not good for high accuracy calculations

    3. Numerical methods

    - powerful

    - easy to get wrong results: be careful

    - 1 & 2 are often used to ensure that the numerical

    solutions are correct

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    Main points: Isotherms and Heat Flow Lines

    FLUX PLOT

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    Main points: Symmetry lines

    Lines of symmetry are adiabatic.

    Symmetry lines are also heat flow lines.

    We need only to study 1/8 of the whole

    structure to save time.

    Long square duct

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    2 2

    2 2

    1

    1

    1

    2

    0

    (0, )

    ( , )

    ( , 0)

    ( , )

    T T

    x y

    T y T

    T L y T

    T x T

    T x W T T1

    T2

    T1 T1

    L

    W

    x

    y

    2 2

    2 2 0

    (0, ) 0

    ( , ) 0

    ( , 0) 0

    ( , ) 1

    x y

    y

    L y

    x

    x W

    1

    2 1

    LetT T

    T T

    2-D steady-state:

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    Separation of Variables

    Assume ( , ) ( ) * ( )x y f x g y

    Hope to obtain equations for ( ) and ( ) separately.f x g y

    Find all solutions and the one that meets all the B.C.s.

    The Fourier series is often involved.

    Let ( , ) ( )* ( )x y X x Y y

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    1

    ( , ) sin sinhnn

    n x n yx y C

    L L

    You can verify that it satisfies the partial different equation

    as well as three of the B.C.s. For it to be the solution, wemust have

    Solving for Cn, we obtain:

    1

    ( , ) 1 sin sinhnn

    n x n W x W C

    L L

    The solution to the differential equation for this problem is

    in the form of:

    1

    2 1 cos( , ) sin sinh sinh

    n

    n n x n y n W x y

    L Ln L

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    Introduction to Finite Difference Method

    Several different numerical methods have been developed.

    Finite difference method is more intuitive and easy to apply.

    Other methods include

    Finite element method

    Finite volume method

    Boundary element method, etc.

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    Numerical method -- continued

    Discretization: a nodal network, called mesh orgrid. We canrefine the mesh but we cannot obtain continuous solutions.

    Nodal points or simply nodes, nodal property such as nodal

    temperature - it is the temperature of the node but it also

    represents the temperature around the node (average).

    Basic principle: Through approximation, convert the

    differential equations to a set of algebraic equations that can be

    solved numerically.

    A coarse mesh A fine mesh

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    ,m nT = average temperature around nodeP(m, n).

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    Discretization of a Continuous Function

    1

    1/ 2

    m m

    m

    T TdT

    dx x

    1

    1/ 2

    m m

    m

    T TdTdx x

    21/ 2 1/ 2 1 1

    2 2

    2

    ( )

    m m m m m

    m

    T T

    x x T T Td T

    xdx x

    T

    x

    m

    m+1

    m+1/2m 1m 1/2

    xx

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    2 2

    2 2 0

    T T

    x y

    21, 1, ,

    2 22

    ( )

    m n m n m n

    m

    T T TTx x

    2, 1 , 1 ,

    2 2

    2

    ( )

    m n m n m n

    m

    T T TT

    y y

    2-D Steady State

    If , then we obtainx y

    1, 1, , 1 , 1 ,4 0m n m n m n m n m nT T T T T

    Finite difference equation for (m, n)

    UseNlinear algebraic equations to solveNunknowns.

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    The Energy Balance Method

    m,n

    m,n 1

    m,n+1

    m+1,nm 1, n

    x

    y

    y

    x

    m,n m+1,n

    x

    y

    m,n m+1,n

    qin

    1yk

    xqin = (Tm+1,nTm,n)

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    m,n

    m,n 1

    m,n+1

    m+1,nm 1, n

    x

    y

    y

    x

    2-D Steady State with Heat Generation

    0in gE E

    1, , 1, ,

    , 1 , , 1 ,

    ( ) ( )

    ( ) ( )

    0

    m n m n m n m n

    m n m n m n m n

    y y

    k T T k T T x x

    x xk T T k T T

    y y

    q x y

    m,n

    m+1,n

    1ykx

    1xk

    y

    m,n+1

    m 1, n

    m,n 1

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    21, 1, , 1 , 1 ,

    ( )4 0m n m n m n m n m nq xT T T T T

    k

    If ,x y

    Corner Nodes and others -- Read pp. 200 - 205

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    What do we end up with is a set of linear algebraic equations.

    Assume there areNunknown nodal temperatures.

    11 1 12 2 1 1

    21 1 22 2 2 2

    1 1 2 2

    .........

    .........

    ........

    .........

    N N

    N N

    N N NN N N

    a T a T a T C

    a T a T a T C

    a T a T a T C

    1

    , 1, 2,...,N ij j ij

    a T C i N

    1 1[ ] [ ] [ ]N N N NA T C

    11 12 1 1 1

    21 22 2 2 2

    1 2

    ... ...

    ... ...

    . .... ... ... . .

    ... ...

    N

    N

    N N NN N N

    a a a T C

    a a a T C

    a a a T C

    1[ ] [ ] [ ]T A C

    Matrix inversion solution:

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    1. Energy balance

    2. Grid-Independent Study

    3. Compare with exact solution if available

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