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    K&C page 77, exercise 3

    y,v

    C (r=1)

    x,u

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    K&C page 77, exercise 3

    x,u

    y,v u= ay = a r sinCirculation:

    = C u d s= 02

    a sin2

    d

    =[ a 12

    x cos x sin x ]0

    2

    = a

    d s r [ i sin j cos ]d

    ds, d

    C (r=1)

    Stokes theorem: surface integral of vorticity = line integral of velocitySometimes one of the two is far easier to calculate!

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    K&C page 77, exercise 3

    x,u

    y,v

    Circulation: = C dA= 12 a = a

    u= ay = a r sinCirculation:

    Vorticity:

    z= a

    = C u d s= 02

    a sin2

    d

    =[ a 12

    x cos x sin x ]0

    2

    = a

    d s r [ i sin j cos ]d

    z= v x

    u y

    ds, d

    C (r=1)

    Stokes theorem: surface integral of vorticity = line integral of velocitySometimes one of the two is far easier to calculate!

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    K&C page 77, exercise 4

    u i

    x j= 1

    2

    u i

    x j

    u j

    xi

    1

    2

    u i

    x j

    u j

    xir ij = ije ij

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    K&C page 77, exercise 4

    e11 = u1

    x1= u

    x= 0

    e 22= u 2 x2

    = v y

    = 0

    Linear strain rates:

    ui x j

    = 12

    ui x j

    u j xi

    12

    ui x j

    u j

    xi

    r ij = ije ij

    Shear strain rates:

    e12 = 12 u1 x2

    u 2 x1

    = 12

    U b

    Vorticity:

    z= r 21= 12 u2 x1

    u1 x2

    = U b

    e 21=12

    U b

    z= r 12=U b

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    K&C page 77, exercise 4

    u i x j

    = 12

    u i x j

    u j xi

    12

    ui x j

    u j xi

    r ij = ije ij

    strain along principal axis (e12

    ); followed by rotation ( z)

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    K&C page 77, exercise 4

    u= Uy /b= y= U

    2

    2bC

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    K&C page 77, exercise 6

    Streamlines:dxu

    = dyv

    1 t x

    dx= 2 t 2y

    dy

    1 t log x =12

    2 t log 2y log f t NB: instant. streamlines, e.g. t = const.; ln f(t) for convenience

    log x1 t =log 2y 1 t /2 log f t We combine last 2 terms in one log, so it becomes a multiplication

    x1 t = f t 2y 1 t /2 This is our answer for the streamlines: x expressed as a function y (or vice versa)

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    K&C page 77, exercise 6

    Pathlines: x t = 0t dx

    dt dt = 0

    t u dt

    dxdt

    = x1 t

    dx x

    = dt 1 t

    log x= log 1 t log f x0

    x= f x0 1 t

    x= x0 1 t

    t = 0 x= x0,so f x0 = x0

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    K&C page 77, exercise 6

    Same for y: y t = 0t dy

    dt dt = 0

    t v dt

    dydt

    = 2y2 t

    dy y

    = 2dt2 t

    log y= 2log 2 t 2log g y0

    y= g y02 2 t 2

    y= y02 /4 2 t 2

    t = 0 y= y0, so g y02= 1 /4 y0

    2

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    K&C page 77, exercise 6

    y= y02 /4 2 t 2

    x= x0 1 t

    The pathline for a particle that is at x0,y

    0at t=0 is given by:

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    K&C page 135, exercise 6

    const. acceleration a

    Steady, so no viscous deformation;only hydrostatic forces; Navier-Stokesequation reduce to:

    0= 1 p x

    a

    g x

    x

    = tan

    0= 1 p z

    gcompareclassichydrostatics:

    tan = ag

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    K&C page 335, exercise 1

    xy

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    K&C page 335, exercise 1

    D u D t

    = 1 P g 2 u

    0= g sin 2 u

    y2

    Fully developed, steady, no driving pressure

    0= g sin y u

    yC 1

    0= g2

    sin y2 u C 1 y C 2

    u= g y2

    2sin C 1 y C 2

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    K&C page 335, exercise 1

    D u D t

    = 1 P g 2 u

    0= g sin 2 u

    y2

    Fully developed, steady, no driving pressure

    0= g sin y u

    yC 1

    0= g2

    sin y2 u C 1 y C 2

    u= g y2

    2sin C 1 y C 2

    No slip: u = 0 at y = h

    0= g h2

    2sin h2 C 2

    Stress-free at surface:

    du /dy = 0 at y= 0

    C 1= 0

    C 2=g h 2

    2sin

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    K&C page 335, exercise 1

    u=g y2

    2 sin C 1 y C 2 C 1= 0 C 2= g h2

    2 sin

    u= g y2

    2sin g h

    2

    2sin

    u= g

    2sin h2 y2 QED

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    K&C page 335, exercise 1

    u= g2

    sin h2 y2

    Q= 0h

    udy = 0h g

    2sin h2 y2 dy =[ g sin

    2h2 y y

    3

    3]0

    h

    = g sin h3

    3

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    K&C page 335, exercise 1

    u= g2

    sin h2 y2

    W = u y y= h

    W =h g sin = gh sin NB : / =

    u y = g 2ysin2 = g y sin

    NB: shear stress is related to column of water that drives the flow

    y = h

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    K&C page 335, exercise 1

    u= g2

    sin h2 y2

    W = u y y= h

    W =h g sin = gh sin NB : / =

    u y = g 2ysin2 = g y sin

    NB: shear stress is related to column of water that drives the flow

    Question: would this also hold for rivers?

    y = h

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    Outer flow is irrotational,So no net viscous forces:Inviscid Bernoulli

    Show ( x u =0)or recognize inviscid vortex

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    Pressure in outer flow:(Bernoulli, compare withfar away u=0, p = p 0)

    p F(z) =p 0 + g(h-z) u 2

    The stress is continuous atsurface, so pressure fromboth sides should be equal(no pressure drop):

    p F = p c

    p 0+ g(h-z)=p 0+ cg(h-z) u2

    Solving for u 2 gives answer

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    Compare the two expressions:

    u =2 r

    u2= 2g ' h z

    2 r

    2

    = 2g ' h z

    outside

    surface

    R z 2=2

    8 2 g ' 1

    h z

    Surface r=R, solve:

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    Velocity scale: V =h

    Froude influence of hydrostatic pressureversus flow-induced pressure (e.g. Y>>1, hardlyany influence of gravity)

    u2

    V 2= u

    2

    2 /h2= 2 g ' h z2 /h2

    u ' = 2Y

    1 z , with Y =2

    g ' h 3

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    SEE KUNDU:Stokes' second problem

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    Surface tension creates a pressuredifference; Pressure differenceused to fill plenum cannot be higherthan the pressure due to surfacetension; so: calculate surfacetension, compare with Poiseuille

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