chap 6 heat loss in fins

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  • 8/11/2019 Chap 6 Heat Loss in Fins

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    6-2 Thin Rectangular Fins

    We will consider only thinrectangular fin.

    The heat transfer through the fincan be treated as one-dimensional, since temperaturegradient exists in the x-directiononly, thus, dT/dx 0.

    Temperature gradient along thewidth, dT/dz , and across thethickness, dT/dy , are negligible.

    L = fins lengthw = fins widtht = fins thickness

    The governing equation for heattransfer trough the fin,

    0=+

    Q

    dxdT

    k dxd

    where Q = internal heat generation (W/m 3).

    6-3 Finite Element ModelingSince heat transfer through the thin fin can be considered one-dimensional, we can model the fin one-dimensional elements.

    Suppose the fin is discretized into three elements, as shown.

    Consider a single element,

    Global coordinate

    Local coordinate

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    Within an element, temperature varies from T 1 at local node 1 to T 2at local node 2.

    To predict the temperature at any point between the two nodes, weneed to establish a temperature function.

    For simplicity, we will assume that the temperature varies withinthe element in a linear fashion. Therefore, we establish a lineartemperature function in the form,

    ( ) [ ]{ }eT N T N T N T =+= 2211

    1 21 1 and

    2 2 N N += =

    6-4 Temperature Function

    where

    are the linear shape functions.

    6-5 Element Conductivity Matrix

    Recall that we use one-dimensional element to model thin fins,which is similar to the case of a plane wall (Chapter 5).

    Therefore the conductivity matrixconductivity matrix for the plane wall element can alsobe used for the fin element, i.e.

    [ ] 2o1 1 W m C1 1e e

    T e

    k k l

    = where k is thermal conductivity of the fin material (W/m. oC) and l e isthe element length.

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    6-6 Element Heat Transfer Matrix

    Recall that in thin fins, heat transfer by convection also takes placetogether with conduction. To include this effect in our analysis, weneed to establish a heat transfer matrixheat transfer matrix, [ hT ].

    It can be shown that,

    [ ] 2o2 1 W

    m C1 23e e

    T

    hl h

    t

    where,h = heat transfer coefficient (W/m 2o C)

    l e = element length (m)t = thickness of the fin (m)

    6-7 Element Heat Rate Vector

    For heat transfer in thin fins, the heat rate is contributed by the heatloss by convection.

    Using the Galerkins approach, it can also be shown that the heatrate vector for a given element is given by,

    { } 21 W

    m1e ehl T r

    t

    where

    T = ambient temperatureh = convective heat transfer coefficient

    t = thickness of the fin

    l e = element length

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    6-8 System of Linear Equations

    For a single fin element, the system of linear equations (SLEs) canbe written in a condensed matrix form as,

    [ ] [ ]( ){ } { }e e e eT T k h T r + =where

    [k T ]e = element conductivity matrix (due to conduction)

    [hT ]e = element heat transfer matrix (due to convection)

    {T }e = nodal temperature vector

    {r }e

    = element heat rate vector

    6-9 Thermal Bondary Conditions

    It is usually assumed that temperature at the base of the fin is thesame as that of the structure, denoted by T o.

    The tip of the fin can be assumed to be adiabatic or insulated,thus, heat flux q = 0 at the tip.

    Therefore, the boundary conditions for fin problems are

    at 0, i.e. specified temperature

    0 at , i.e. specified heat fluxoT T x

    q x L

    = == =

    Global coordinate

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    The heat loss, H e, from each fin element can be estimated usingthe NewtonNewton s laws law of cooling, given by

    ( ) ( ) ( )2e avg s avg e H h T T A h T T w l = = where

    The totaltotal heat loss from the entire fin can be obtained using,

    1

    n

    ee

    H H =

    =

    6-10 Heat Loss Through the Fin

    h = convective heat transfer coefficient,T avg = average temperature within the element,T = ambient temperature,

    A s = surface are of the fin,w = width of the fin,

    le = length of the element.

    Example 6-1

    A metallic fin, 0.1 cm thick,10 cm long, 1 m width and with thermalconductivity k = 360 W/m oC, extends from a plane wall whosetemperature is 235 oC. Determine the temperature distribution withinthe fin and amount of heat loss from the fin to the ambient air, whichis at 20 oC. Take h = 9 W/m 2oC.

    SolutionWe will model the fin using three one-dimensional elements andassume that the tip of the fin is insulated.

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    [ ]( ) [ ]( ) [ ]( )1 2 3 21 13601 13.33 10T T T

    k k k = = =

    [ ]

    =

    1100

    1210

    0121

    0011

    1033.3360

    2T K

    1. Element conductivity matrices

    Since the fin is made up of homogeneous material and that allelements have the same length, the element conductivity matrixfor the elements will be the same, i.e.

    2. Assemble global conductivity matrix

    1 2 3 4 Global nodes

    [ ]( ) [ ]( ) [ ]( )

    ===

    21

    12

    001.031033.39 2321

    T T T hhh

    [ ]

    =

    2100

    1410

    0141

    0012

    001.031033.39 2

    T H

    3. Element heat transfer matrices

    Since all elements have the same length and thickness, theelement heat transfer matrix for the elements will be the same,

    4. Assemble global heat transfer matrix

    1 2 3 4 Global nodes

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    { }( ) { }( ) { }( ) ===

    1

    1

    001.0201033.39 2321 r r r

    { } =

    12

    2

    1

    001.0

    201033.39 2 R

    5. Element heat rate vector

    Since all elements have the same length and thickness, theelement heat rate vector for the elements will be the same, i.e.

    6. Assemble global heat rate vector

    1

    2

    34

    Global nodes

    7. Write the system of linear equations

    1

    2 22

    3

    4

    2

    1 1 0 0 2 1 0 0

    1 2 1 0 1 4 1 0360 9 3.33 100 1 2 1 0 1 4 13.33 10 3 0.001

    0 0 1 1 0 0 1 2

    1

    29 3.33 10 2020.001

    1

    T

    T T

    T

    +

    =

    [ ] [ ]( ){ } { }T T K H T R+ =We get,

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    8. Impose the thermal boundary conditions.

    1

    22

    23

    4

    2

    1 1 0 0 2 1 0 0

    1 2 1 0 1 4 1 0360 9 3.33 100 1 2 1 0 1 4 13.33 10 3 0.001

    0 0 1 1 0 0 1 2

    1

    29 3.33 10 2020.001

    1

    T

    T

    T

    T

    +

    =

    We have T 1 = 235 C. Using the Gauss eliminationGauss elimination method, wedelete the 1 st row and column of the SLEs, and modify the rightside term accordingly.

    22

    32

    4

    2

    2

    2 1 0 4 1 0360 9 3.33 10

    1 2 1 1 4 13.33 10 3 0.0010 1 1 0 1 2

    29 3.33 10 20

    20.001

    1

    1360 235

    03.33 10

    0

    T

    T

    T

    +

    =

    2

    19 3.33 10 235

    03 0.001

    0

    9. Write the reduced system of linear equations

    After imposing the boundary condition, the system of linearequations are reduced to,

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    2o

    3

    4

    211.7

    197.0 C

    192.2

    T

    T

    T

    =

    21

    22

    23

    235 211.79 20 2 1 3.33 10 121.9 W

    2

    211.7 1979 20 2 1 3.33 10 110.5 W2

    197 192.29 20 2 1 3.33 10 104.7 W

    2

    H

    H

    H

    + = =

    + = = + = =

    10. Solve the reduced SLEs

    Solving the reduced SLEs yields

    11. Heat loss from each element

    12. Total heat loss

    The total heat loss from the fin is given by

    1 2 3

    121.9 110.5 104.7

    337.1 W

    H H H H

    H

    H

    = + += + +

    =

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    End of Chapter 6