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    Fluid Mechanics for Chemical

    Engineers

    Old and New

    by James O. Wilkes

    Arthur F. Thurnau Professor

    Emeritus of Chemical Engineering

    University of Michigan

    Wednesday 16 February 2011

    [email protected]

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    Published in 2006

    I: Macroscopic FM II: Microscopic FM

    773 pages

    82 Examples

    (incl. 14 CFD)

    352 Problems

    Two-phase flow

    Microfluidics Computational

    fluid dynamics

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    Two parts, with opportunities

    for questions after each.

    Macroscopic or relatively large-scalephenomena: basic & simple concepts of mass,

    energy, and momentum balances commensuratewith the PE and FE examinations.

    Microscopic or small-scale phenomenastarts

    with the relatively complicated partial differentialmass and momentum equations of fluid motion.Solutions are often best made by computationalfluid dynamics (CFD) software.

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    Part I

    Macroscopic Fluid Mechanics

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    Characteristic of a Fluid

    FluidDeforms continuously when subject to a tangentialor shear force.

    Velocity profile: shows how velocity varies with position;note the no-slip condition at each surface.

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    StressForce Per Unit Area, F/A

    (a)Normal stress = F/A:pressure is the most important case.

    (b) Shear stress = F/A: acts tangentially to an area (that due to

    viscosity is important example).

    (a)

    (b)

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    Viscosity

    ForNewtonian fluids (a broad class), the shear stress = F/A (A =area of plate) is proportional to the velocity gradient du/dy, in

    which the constant is the viscosity (with dimensions M/LT):

    = du

    dy

    = V

    h

    .

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    Conservation Law forX= Mass, Momentum, Energy (Only)

    The diagram shows a system and transports to and from it. Ignoring the

    created and destroyed terms (necessary for reactions but generally not needed in

    fluid mechanics), the basic conservation or balance law is:

    Xin Xout = XSystem

    xin xout=dXSystem

    dt.

    Or, ifx (lower case) denotes a rate of transferof propertyX, then:

    (1)

    (2)

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    Energy Balance (Bernoullis Equation)

    Assumptions:

    Steady flow

    No work effects (no pump or turbine) Frictionless (OK for short runs of straight pipe)

    Incompressible (constant density)

    Under these circumstances, the sum of the kinetic energy, potential, and

    pressure energy remains constant between points 1 and 2:

    u12

    2+gz1 +

    p1

    =u2

    2

    2+gz2 +

    p2

    A related form is also available if there are significant work and frictional

    effectsespecially useful for pumping and piping problems. Eqn. (1) can also

    be divided through by g, so each term has units of length, called either the

    velocity, hydrostatic, or pressure head, withHbeing the constant total head.

    u12

    2g+z1 +

    p1

    g=H=

    u22

    2g+z2 +

    p2

    g

    (1)

    (2)

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    Dynamics of a

    distillationcolumn

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    End of Part I

    Questions?

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    Part II

    Microscopic Fluid Mechanics

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    Representative Computational Fluid

    Mechanics (CFD) Software(Usually based on the finite-element, finite-

    difference, or finite-volume methods)

    Adina

    Ansys COMSOL

    Flow-3D

    Fluent

    FlowLab

    FloTHERM OpenFOAM

    OpenFLOWER

    Etc.

    For a good overview, see:

    http://en.wikipedia.org/wiki/Computational_fluid_dynamics

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    Screw Extruder for Increasing the

    Pressure of a Polymer Before a Die

    h

    r

    Axis ofrotation

    Metering sectionFeed hopper

    Barrel

    Flights

    Exitto die

    Screw

    Primary feedheating region

    W

    L0

    Compressionsection

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    Motion of Barrel as Seen by an Observer

    on ScrewCouette (Relative Motion) +

    Poiseuille (Pressure-Driven) Flow

    x

    W

    h

    Flight axis

    Flight

    Screw

    Barrel

    Vx

    Vy

    V

    Flight

    z y

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    Cross Section between Barrel

    (Moving Left) and Screw (Fixed)

    p= 0

    z

    x

    y= 0x= 0 2

    4

    No slip x= 0.1

    y= 0.005

    1 3No slip No slip = 800 = 500

    Vx= - 0.1 A

    B

    1

    2

    3

    4

    Barrel

    Screw

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    Plots: Arrows, Streamlines, Isobars

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    Horace Lamb (18491934)

    (to the British Association for the

    Advancement of Science, 1932)

    I am an old man now, and when I die and go

    to heaven there are two matters on which I

    hope for enlightenment. One is quantum

    electrodynamics, and the other is the turbulentmotion of fluids. And about the former I am

    rather optimistic.

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    Arrows and Streamlines for Turbulent

    Jets

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    Turbulent Kinematic Viscosity T

    Turbulent Kinetic Energy k

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    Flow of a shear-thinning polymer in a die

    (a) Extrusion from a pipe forming a tube (b) Rotation, also

    exploiting symmetry

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    Velocities

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    A B

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    AB

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    l i bl

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    x

    +

    +

    +

    +

    Sternlayer

    Potential(negative)

    +

    +

    +

    +

    +

    ++

    +

    +

    +

    -potential (negative)

    Diffuse layer

    x= 0

    ySolid

    surface

    Ey

    = 0

    +

    Electric Double Layer

    = dV

    dy

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    x0

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    -potentialThe electric potential rises tozero over a very thin electricdouble layer next to the wall

    Debye length, D

    0

    vy vy

    =yE

    x

    VelocityProfile

    ElectricPotential

    The velocity changes quickly

    from zero at the wall to aconstant value everywhere else

    0

    (constant)

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    Electroosmosis (Multiphysics problem:

    Navier-Stokes + Conductive Media DC )

    Channel Geometry

    H= 0.00005,L = 0.0005 m, = 0.1 V

    Finite-element Mesh

    y

    x

    y= 0x= 0

    2x=L

    y = H

    1

    3

    4A

    B C

    D

    Electric insulation

    Electric insulation

    1 V0 V

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    Velocity Vectors (Arrow Plot)

    Streamlines

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    Electroosmotic Switching1

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    Electroosmotic Switching2

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    End of Part II

    Questions?

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    PostscriptWhats the

    connection

    between thisMemphis juke

    box and fluid

    mechanics?

    Thanks for

    your attention!