Topic 1 Surface Resistance Part II

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    Surface Resistance

    Part II

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    Fully Developed Flow between Parallel

    Plates Using the Navier-Stokes Equations

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    Navier-Stokes Equations without Body Forces

    ( ) ( ) ( )Continuity: 0

    u v w

    t x y z

    + + + =

    ( ) ( ) ( ) ( )2 1x-momentum:

    Re

    xyxx xzuu uv uw p

    t x y z x x y z

    + + + = + + +

    ( ) ( ) ( ) ( )2 1y-momentum:

    Re

    xy yy yzvv uv vw p

    t x y z y x y z

    + + + = + + +

    ( ) ( ) ( ) ( )2 1z-momentum:

    Re

    yzxz zzww uw vw p

    t x y z z x y z

    + + + = + + +

    ( ) ( ) ( ) ( ) ( ) ( ) ( )

    ( ) ( ) ( )

    Energy:

    1

    RePr

    1

    Re

    T T T T

    yx z

    xx xy xz xy yy yz xz yz zz

    E uE vE wE up vp wp

    t x y z x y z

    qq q

    x y z

    u v w u v w u v wx y z

    + + + =

    + + +

    + + + + + + + + +

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    Fully Developed Flow between Parallel Plates Using

    the Navier-Stokes Equations

    The governing equation for laminar flow over a surface can also be

    derived using the Navier-Stokes equations.

    Introduce the new variables xis the coordinate in the direction of

    flo

    w (same as s)and y perpendicular to the plates.

    x

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    Fully Developed Flow between Parallel Plates Using

    the Navier-Stokes Equations

    The flow field is fully developed, so the derivatives

    Also the flow is steady, so

    The components of the gravity force are

    The continuity equation is

    Therefore

    Continuity equation is automatically satisfied!

    0u

    x

    =

    0

    v

    x

    =

    0v

    t

    =

    -direction sinx g

    u

    x

    0

    v

    y

    + =

    0 constant 0v

    v vy

    = = =

    0u

    t

    =

    -direction cosy g

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    Fully Developed Flow between Parallel Plates Using

    the Navier-Stokes Equations

    Momentum equation in the y direction is

    As v is zero everywhere, there is no acceleration of the fluid in

    the y direction and equation reduces to

    By integrating last equation we can get

    where py=0(x) is the pressure distribution along the lower wall.We can see that pressure is decreasing with the elevation in

    the duct.

    We can rewrite this equation as

    where

    v

    t

    vux

    vvy

    2

    2

    p v(y x

    2

    2

    v

    y

    ) g cos

    cosgyp =

    )(cos 0 xpygp y=+=

    )(0 xpzp y==+

    zy =cos

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    Fully Developed Flow between Parallel Plates Using

    the Navier-Stokes Equations

    The gradient of pressure in the x direction is

    Momentum equation in the x direction is

    For steady, fully developed flow all the terms in the left-handside of the equation equal zero and the equation becomes

    As u is a function ofy and is function of x only we can

    rewrite this equation in this form

    As the slope is

    We can rewrite the last equation as

    u

    t

    uu

    x

    +

    v+

    2

    2(

    u p u

    y x x

    = +

    2

    2) sin

    ug

    y

    + +

    dx

    dp

    dx

    dp

    x

    p y==

    =0

    2

    2

    siny

    upg

    x

    p

    =

    xp /

    2

    2

    sindy

    udgdxdp =

    dx

    dz=sin

    2

    2

    )(dy

    udzp

    dx

    d =+

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    Fully Developed Flow between Parallel Plates Using

    the Navier-Stokes Equations

    2

    2

    d d up zdx dy

    )(12

    2

    zpds

    d

    dy

    ud

    +=From SimpleForce Balance

    From N-S

    Equations

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    Surface Resistance

    Solution of Laminar Boundary

    Layer by Blasius

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    Surface Resistance

    Turbulent Velocity Profile

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    Turbulent

    Boundary

    Layer

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    Surface Resistance

    Shear Stress at Turbulent Region

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    Boundary Layer

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    Boundary Layer