similitude in hydrosimilitude in hydrodynamicsdynamics

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    Similitude in Hydrodynamic

    Problems

    Department of Ocean EngineeringIndian Institute of Technology Madras

    Chennai 600 036

    Prof.V.G.Idichandy

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    Introduction

    Hydrodynamic problems need to be separately treated.

    Difficult to achieve complete similitude

    There are many more problems that require solution using

    an empirical approaches based on experimental data. Background for deriving appropriate scaling relationship

    for hydrodynamic model tests.

    Complete similarity models are models in which the values

    of all relevant dimension less parameters in the prototypeare maintained in the model.

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    Geometric similarity

    Geometrically similar models are undistorted models

    Horizontal and vertical scales are the same

    The model is a true geometric reproduction.

    Definite objectives can be achieved by departing formgeometric similarity.

    Such models are called distorted models.

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    Kinematic similarity

    In hydrodynamic model kinematic similarity is achieved

    when the ratio between the components of all vertical

    motions for the prototype and the model are the same forall particles at all times.

    In a geometrically similar model, the kinematic similarity

    gives particles paths that are geometrically similar toprototype.

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    Kinematically similar wave motion

    What is the scaling criteria necessary for kinematically

    similar wave motion for gravity waves whose length is

    given by

    L is the wave lengthg acceleration due to gravity

    T wave period

    h water depth

    2 2tanh

    2

    gT hL

    L

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    Kinematically similar wave motion

    2h/L is dimension lessThis ratio for model and prototype should be an invariant

    for geometrically similar model.

    2h/L is the same, then the hyperbolic tangent will also bethe same.

    The scale relationship between L and T is found from theprototype to model ratio of wave length.

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    Kinematically similar wave

    motion

    2

    2

    2

    2

    2

    tanh(2 / )2

    tanh(2 /2

    p p

    m

    m

    p p p

    m m m

    e g T

    gTh L

    L

    L gT h L

    L g T

    L g T

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    Kinematically similar wave motion

    g= 1

    Therefore the kinematic similarity of wave motions can

    be achieved by making

    T l

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    Dynamic Similarity

    Kinematic similarity is achieved without considering any

    other properties of the fluid

    But this is not so for dynamic similarity.

    Dynamic similarity between two geometrically and

    kinematically similar system requires that the ratio's of all

    vectorial forces in the two systems be the same.

    In other words, there must be constant prototype to model

    ratio's of all masses and forces acting on the system.

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    Dynamic Similarity

    For fluid mechanics problems Newton's second law can be written as,

    Fi= Fg+ F+ F + Fe+ Fpr

    Where Fi inertial force, mass x accelaeration

    Fg gravitational force

    F viscous forceF surface tension forceFe elastic compression force

    pr pressure force

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    Dynamic Similarity

    Forces being vectors both magnitude and directionmust be represented.

    Overall dynamic similarity requires that the ratio of

    the inertial forces between prototype and model be

    equal to the ratio of the sum of all the active forces

    expressed as,

    g e pri p p

    i g e pr m m

    F F F F FF

    F F F F F F

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    Dynamic Similarity

    Perfect similitude requires in addition to the above that all

    force ratios between the prototype and model be equal or,

    or in terms of scale ratios,

    g pri ep p p p p p

    i eg prm m m mm m

    F FF F F F

    F F F FF F

    i g e pr F F F F F F

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    Dynamic Similarity

    No fluid is known that will satisfy all force ratio

    requirements, if the model is smaller than the prototype.

    So an important task in scale model design is to relate

    the important force ratios and to provide justification for

    neglecting the others

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    Practical aspects

    Dynamic similarity is practically unachievable forscale models other than for scale factor 1

    For model tests the similarity requirements have

    to be violated

    In model tests, it should be possible to justifydepartures and where required apply theoretical

    corrections

    It should also be possible to predict which of theforces are important for a given situation.

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    Practical aspects

    Almost any major problem can besimplified into the interplay of two majorforces.

    Inertia forces are always present in flowproblems. So inertia needs to be balancedby one or more of the other forces.

    The first step is to express each of theforces in terms of their physical units.

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    Practical aspects

    3 22 2

    3

    2

    e

    L acceleration L

    accleration due to gravity = L g

    Velocity VF cos area = V Ldistance L

    F unit surface tension length = L

    F modules of elastic

    i

    g

    VF mass V

    L

    F mass

    Vis ity L

    2

    2

    ity area = E L

    unit pressure area = p LprF

    The ratio of the inertial force to any other force

    provides the relative influence of the two forces in

    hydrodynamic problems. Each force ratio leads

    similitude criterion as given below.

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    Froude Criterion

    It is the parameter that express the relative

    influence of inertial and gravitational

    forces,expressed as the square root of theratio of forces

    2 2

    r3Froude Number ( F )

    L V V

    L g Lg

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    Froude Criterion

    The Froude criterion for modeling

    inertial forces are balanced primarily by gravitational forces,which is true in most cases involving free surface.

    Majority of problems in hydrodynamics are scaled accordingto Froude model law and therefore it is the most important

    model law .

    p m

    V V

    Lg Lg

    p p p

    m m m

    V g L

    V g L

    1

    1v

    g

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    Reynolds Criterion

    When viscous forces dominate, the important parameter is

    the ratio of inertial to viscous forces

    Reynolds used this number to distinguish between laminar

    and turbulent flows.

    Reynolds similitude is achieved when,

    2 2

    e L V Reynolds Number (R )

    L VV L

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    Reynolds Criterion

    Reynolds law is intended for flows where viscous forces

    dominate.

    Examples are laminar boundary layer, forces on cylinder for

    low values of Re

    Lv

    1

    p m

    p p p p

    m m m m

    v L p

    LV

    V L

    V L

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    Weber Criterion

    Relative importance of surface tension is given by inertia to surface tension forces

    Weber model criteria is used when surface tension forces dominates

    Surface tension effects are seldom encountered in ocean engineering problems in

    prototype. In very small models surface tension may play some role.

    2 2 2int forces vL Weber Number

    surface tension forces

    ertial V V L

    L

    2

    1p v L

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    Cauchy Criterion

    An index of the relative importance of inertial forces to

    compressive forces

    This is of importance where inertial forces are large enough to cause

    changes in fluid compressibility. Cauchy number is related to Machnumber (v/c) because the speed of sound c in a fluid is given by

    2 2 2

    2

    inertial forcesCauchy number

    elastic forces

    L V V

    E L E

    E 2

    2 V

    Ea aM C

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    Cauchy Criterion

    Mach number is used in studies of air flow having high

    velocities. Cauchy modeling criterion is,

    This criterion has little application in Ocean engineering

    problems because the fluid is considered incompressible.

    There could application in breaking waves.

    2

    1v

    E

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    Euler Criterion

    When the pressure forces are dominant Euler

    criterion is used

    Euler model criterion is

    2

    2 2 2

    Pressure force P L

    intertial force L

    P

    V V

    2

    v

    1

    p

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    Strouhal Number

    Inertial forces in fluid can be caused by two types of accelerations. Convective

    accelerations are due to different fluid velocities at different locations in the flow field

    and they are represented mathematically as,

    Temporal accelerations are changes in flow velocity at a point that occur in time. They

    represent the unsteadiness of the flow and can be expressed mathematically as,

    /u u x

    /u t 3

    22

    Tenporal inertial force = L

    Connective inertial force = L

    V

    t

    V

    L

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    Strouhal Number

    The relative importance of temporal inertia force to connectiveinertial force is given as

    which is represented as Strouhal Number .

    This dimensional parameter is important in unsteady, oscillatory flows.Where the period of oscillation is given by variable it. Often StrouhalNumber is expressed as (L/V) or (fL/V)

    2

    22

    L

    L

    V

    Lt

    V VT

    L

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    Strouhal Number

    For Strouhal Criteria in the model

    which states that the velocity scalar ratio is equal to the length scale ratio divided by

    time scale ratio. In unsteadyoscillating flows it is important to maintain similarity of

    Strouhal Numbers

    1

    p m

    p p p

    m m m

    L

    v t

    L L

    Vt Vt

    L V t

    L V t

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    Importance of Froude Scaling

    Practically most of the ocean engineering problems and fluid flowproblems, where the forces due to surface tension, pressure andelastic compressionare relatively small and can be safely neglected.

    This leaves an appropriate hydrodynamic scaling law to an evaluationof whether gravity or viscousforces are dominant.

    Therefore either Froude or Reynolds similarity combined with

    geometric and Kinematic similarity provides the condition forhydrodynamic similitude in almost all ocean related problems.

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    Importance of Froude Scaling

    Reynolds similitude is seldom

    involved for most models as gravity

    forces dominate in free surface flowsand consequently most models are

    designed for Froude criteria.

    However, the viscous effects must bereducedotherwise dissimilar viscous

    forces will constitute scale effect.

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    Scaling of A Froude Model

    In the study of wave mechanics three non-

    dimensional parameters are most

    important. They are Froude, Reynolds andStrouhal. Keulegan-Carpenter number also

    becomes important in showing the

    dependence of inertia and dragcoefficients.

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    Scaling of A Froude Model

    Except Cm and Cdall terms follow Froude scaling.

    The hydrodynamic coefficients Cd& Cmare non-

    dimensional and are function of Keulegan-

    Carpenter number KC defined as (uT/D).According to Froude's law the velocity and wave

    period scale are square root of the scale factor

    while linear dimension scale linearly

    p m

    KC KC

    3

    2

    ewhere as R ep mR

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    Scaling of A Froude Model

    For current drag, the drag force is proportional to the

    square of the velocity. Experiments have shown that flow

    characteristics in the boundary layer are most likely to be laminar

    at Re < 106 but turbulent for Re > 106. In most model of Froude

    scale boundary layer is laminar whereas for prototype it is

    turbulent. Thus two scaling laws have to be applied which is ,not

    possible. It is convenient to employ Froude scaling in a laboratary

    and apply correction for violating Reynolds number.

    Once the flow is turbulent the drag coefficient is only

    weakly dependent as Re. As a result in many experiments, the

    laminar flow is deliberately tripped by some kind of roughness

    near the bow of the structure.