ME2342_Sec3_Kinematics

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    P. S. Krueger ME/CEE 2342 3 - 1

    ME/CEE 2342:

    Paul S. Krueger

    Associate Professor

    Department of Mechanical Engineering

    Southern Methodist UniversityDallas, TX 75275

    [email protected]

    (214) 768-1296Office: 301G Embrey

    Fluid Mechanics

    Section 3 Fluid Kinematics (Motion)

    [Chapter 4 in the text book]

    mailto:[email protected]:[email protected]
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    Example: Flow Out of a Pipe

    Two Options:1) Track the velocity of each individual fluid particle.

    2) Observe the velocity of the fluid particles moving through

    each point in space

    Eulerian and Lagrangian Flow Descriptions

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    Option 1 is called the Lagrangian description of the flow.

    This method provides the velocity of each particle i in the

    flow for all time:

    where

    ( )

    Option 2 is called the Eulerian description of the flow. In

    this case the velocity is given at each point in the flow for all

    time and is represented as a velocity field:( ) ( ) ( )zyxu ,,,,,,,,,,,, tzyxwtzyxtzyxutzyx ++= v

    222wuV ++= vu = flow speed

    Both descriptions provide the same information in different

    ways. For fluid mechanics, the Eulerian description isusually more convenient

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    Streamlines, Streaklines, and Pathlines

    To assist visualization or interpretation of complex flows, we

    often construct/insert lines in the flow that represent fluid

    motion. Three common types are

    x

    y

    Streamlines and Vector Field

    -2 -1.5 -1 -0.5 0 0.5 1 1.5 20

    0.5

    1

    1.5

    2

    2.5

    3

    3.5

    4

    -1.8 -1.6 -1.4 -1.2 -1 -0.8 -0.6 -0.4 -0.2

    0.2

    0.4

    0.6

    0.8

    1

    1.2

    1.4

    1.6

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    2

    2.2

    1) Streamlines. Streamlines are lines that are everywhere

    tangentto the velocity field.

    Stagnation Point Flow:

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    2) Pathlines. Pathlines follow the path of individual fluid

    particles. Conceptually these can be generated by

    placing a dot of dye in a liquid flow and tracing its path asit moves.

    Example: Bubbles follow pathlines

    [Source: Cengel and Cimbala (2010), Fig. 4-21]

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    3) Streaklines. Streaklines are the path traced out by

    particles injected into the flow at a fixed point.

    Conceptually, we can create streaklines by using adropper to put drops of dye into the flow at a fixed point

    and then connecting the dots to form a streakline.

    Example: Smoke visualization of flow over a wing

    [Source: Bertin, Aerodynamics for Engineers, Prentice Hall (2002)]

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    For a general flow, all three flow lines may give different but

    complimentary pictures of the flow (see Example 4-5 in the

    textbook).

    Forsteady flows (flows that do not change in time), each

    fluid particle follows the one preceding it, so streamlines,

    streaklines, and pathlines are identical for steady flows.

    We will deal primarily with steady flows and focus on

    streamlines. For a 2D flow:

    By definition of streamlines, the coordinates (xs, ys) of all

    streamlines must obey

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    Examples:

    1) Linear Flow

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    Separate variables and integrate:

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    2) Stagnation Point Flow

    ( )yxu 0 yxLU =

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    Sketch of a few streamlines:

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    The Acceleration Field and Material

    Derivative

    Given the velocity field, we can find the acceleration of the

    fluid particles at each point in space by taking the total

    derivative:

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    In component form

    Short hand:

    ( )uuuu

    a +

    ==

    tDt

    D

    where

    ( )( ) ( ) ( )

    zyx

    +

    +

    = zyx

    D()/Dt is called the material derivative and refers to the rate

    of change of a quantity () for a fluid particle at (x, y, z) at

    instant t. We applied it to u to obtain a, but it can be appliedto any fluid property (temperature, density,).

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    Note: The fluid velocity can be changed by either of two

    effects:

    1) Unsteady effects: rate of change at a fixed location

    2) Convective effects: Change caused by moving to a

    location where flow properties are different

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    Example: Converging Nozzle

    Find the acceleration field.

    x-component:

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    y and z-components:

    Note: ax 0 even though flow through the nozzle is steady.

    This occurs because flow speed increases in x (u/x 0).As you move from A to B to C, u increases and so the

    acceleration is non-zero.