(18) External Forced Convection Part2

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  • 8/11/2019 (18) External Forced Convection Part2

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    EXTERNAL FORCED CONVECTION

    Associate Professor

    IIT Delhi

    E-mail: [email protected]

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    Flate plate with unheated

    starting length

    Using integral solution methods,

    the local Nusselt numbers for both

    laminar and turbulent flows aree erm ne o e

    31

    3

    31

    5.0

    x

    31

    3

    )0_for(x

    x

    PrRe332.0NuNu == =Laminar flow

    x1x1

    31

    8.0

    P.Talukdar/Mech-IITD 2

    91

    109

    x

    91

    109

    0_orx

    x

    x1

    .

    x1

    Nu

    =

    = =

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    The determination of the average Nusselt number for the heated section

    of a plate requires the integration of the local Nusselt number

    Lx

    43

    h.x

    12

    h =

    =Laminar flow

    L

    1

    109

    x15

    The late is sub ected to uniform Heat Flux condition

    Lx.

    L14

    =

    =

    31

    5.0

    xx PrRe453.0Nu =Laminar flow

    These relations give values that are 36 percent higher for laminar flow and

    318.0

    xx PrRe0308.0Nu =Turbulent flow

    P.Talukdar/Mech-IITD 3

    4 percent higher for turbulent flow relative to the isothermal plate case.

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    Flow over a cylinder and

    sphere

    P.Talukdar/Mech-IITD 5

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    P.Talukdar/Mech-IITD 6

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    Pressure distribution along a

    cylinder Consistentwithboundar la ertheor the ressurethrou h

    theboundary

    layer

    is

    essentially

    constant.

    p=p(x)

    only.

    Thusthepressureintheboundarylayershouldfollowthatof

    e rees ream orpo en a owaroun acy n er

    P.Talukdar/Mech-IITD 7

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    . Astheflow ro ressesalon thefrontsideofthec linder the

    pressurewould

    decrease

    and

    then

    increase

    along

    the

    back

    sideofthecylinder,resultinginanincreaseinfreestream

    thebackside

    P.Talukdar/Mech-IITD 8

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    Sincethe

    ressure

    is

    assumed

    constant

    throu hout

    the

    boundarylayer,wenotethatreverseflowmaybegininthe

    boundarylayernearthesurface;thatis,themomentumof

    overcomethe

    increase

    in

    pressure.

    P.Talukdar/Mech-IITD 9

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    P.Talukdar/Mech-IITD 11

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    coefficientdecreases

    with

    increasing

    Reynolds

    number.Forasphere,itisCD=24/Re.Thereisno

    flowseparationinthisregime.

    Atabout

    Re

    =10,

    separation

    starts

    occurring

    on

    the

    rearofthebodywithvortexsheddingstartingat

    aboutRe= 90.

    Theregion

    of

    separation

    increases

    with

    increasing

    ReynoldsnumberuptoaboutRe= 103.Atthispoint,

    drag.P.Talukdar/Mech-IITD 12

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    Thedragcoefficientcontinuestodecreasewithincreasing

    3

    .

    Adecreaseinthedragcoefficientdoesnotnecessarily

    indicateadecreaseindrag.Thedragforceisproportionalto

    thesquareofthevelocity,andtheincreaseinvelocityat

    higherReynolds

    numbers

    usually

    more

    than

    offsets

    the

    decreaseinthedra coefficient

    P.Talukdar/Mech-IITD 13

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    Inthemoderateran eof103

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    Thereisasuddendropinthedragcoefficientsomewherein

    theran e

    of

    10

    5