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Gv 3 Newtonian Compressible Flows

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    MEE206Fluid Mechanics

    G. Vinayagamurthy Dr. Engg.School of Mechanical and Building Sciences

    VIT University Chennai

    Lecture - 5

    Newtonian and Non-Newtonian Fluids

    Compressibility

    Incompressible and Compressible flows

    VINAYAGAMURTHY, SMBS, VIT CHENNAI

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    Viscosity

    where is called absolute or dynamic viscosity. Dimensionsand units for are and , respectively. [In

    the absolute metric system basic unit of co-efficient of viscosity

    is called poise. 1 poise =

    The viscosity is measure of the fluidity of the fluid which is not captured simply by

    density or specific weight. A fluid can not resist a shear and under shear begins to flow.

    The shearing stress and shearing strain can be related with a relationship of the followingform for common fluids such as water, air, oil, and gasoline:

    dy

    du

    No SlipCondition

    VINAY

    AGAMURTHY, SMBS, VIT CHENNAI

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    For Non-Newtonian fluid: . Examples are sugar solution andpolymers. Therefore,General expression for shear stress

    where, m is the flow consistency and n is the flow behaviour index.

    Also known as powerLaw model

    also known as apparent viscosityVINAYAGAMURTHY, SMBS, VIT CHENNAI

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    Viscosity: Measurements

    A Capillary Tube Viscosimeter is one method of measuring the viscosity of the fluid.

    Viscosity Varies from Fluid to Fluid and is dependent on temperature, thus

    temperature is measured as well.

    Units of Viscosity are Ns/m2or lbs/ft2

    VINAYAGAMURTHY, SMBS, VIT CHENNAI

    http://localhost/var/www/apps/conversion/tmp/scratch_1/1-6.jpghttp://localhost/var/www/apps/conversion/tmp/scratch_1/V1_3.movhttp://localhost/var/www/apps/conversion/tmp/scratch_1/1-6.jpghttp://localhost/var/www/apps/conversion/tmp/scratch_1/1-6.jpghttp://localhost/var/www/apps/conversion/tmp/scratch_1/1-6.jpghttp://localhost/var/www/apps/conversion/tmp/scratch_1/1-6.jpghttp://localhost/var/www/apps/conversion/tmp/scratch_1/1-6.jpg
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    Viscosity

    VINAYAGAMURTHY, SMBS, VIT CHENNAI

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    Newtonian Fluids

    VINAYAGAMURTHY, SMBS, VIT CHENNAI

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    VINAYAGAMURTHY, SMBS, VIT CHENNAI

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    Non-Newtonian Fluids

    VINAYAGAMURTHY, SMBS, VIT CHENNAI

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    Non-Newtonian Fluids

    VINAYAGAMURTHY, SMBS, VIT CHENNAI

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    No slip condition

    No-slip conditionfor viscous fluids states that ata solid boundary, the fluid will have zero velocity

    relative to the boundary.

    No Slip

    Condition

    VINAYAGAMURTHY, SMBS, VIT CHENNAI

    http://localhost/var/www/apps/conversion/tmp/scratch_1/V1_2.movhttp://localhost/var/www/apps/conversion/tmp/scratch_1/V1_2.movhttp://localhost/var/www/apps/conversion/tmp/scratch_1/V1_2.movhttp://localhost/var/www/apps/conversion/tmp/scratch_1/V1_2.mov
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    Compressibility

    Compressibility of any substance is the measure of its change in

    volume under the action of external forces. The normal compressive stress on any fluid element at rest is

    known as hydrostatic pressure p and arises as a result of

    innumerable molecular collisions in the entire fluid.

    The degree of compressibility of a substance is characterized by the

    bulk modulus of elasticity E defined as

    VINAYAGAMURTHY, SMBS, VIT CHENNAI

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    E for liquids are very high as compared with those of gases (except at very high

    pressures). Therefore, liquids are usually termed as incompressible fluids though, in

    fact, no substance is theoretically incompressible with a value ofE as

    For example, the bulk modulus of elasticity for water and air at atmospheric

    pressure are approximately 2 x 106kN/m 2and 101 kN/m 2respectively. It indicates

    that air is about 20,000 times more compressible than water. Hence water can be

    treated as incompressible.VINAYAGAMURTHY, SMBS, VIT CHENNAI

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    For gases another characteristic parameter, known as compressibility

    K, is usually defined , it is the reciprocal of E

    K is often expressed in terms of specific volume

    VINAYAGAMURTHY, SMBS, VIT CHENNAI

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    Incompressible and a Compressible

    Flow

    In order to know, if it is necessary to take into account the compressibility ofgases in fluid flow problems, we need to consider whether the change in pressure

    brought about by the fluid motion causes large change in volume or density.

    By Bernoulli's equation

    p + (1/2)V2= constant (V being the velocity of flow), change in pressure, p, in

    a flow field, is of the order of (1/2)V2 (dynamic head).

    Invoking this relationship into

    So if / is very small, the flow of gases can be

    treated as incompressible with a good degree of

    approximation.VINAYAGAMURTHY, SMBS, VIT CHENNAI

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    where, Ma is the ratio of the velocity of flow to the acoustic velocity in theflowing medium at the condition and is known as Mach number.

    So we can conclude that the compressibility of gas in a flow can be neglected

    if /is considerably smaller than unity, i.e. (1/2)Ma2

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    Compressibility of Fluids: Speed of Sound

    vE

    cord

    dp

    c

    kpc

    A consequence of the compressibility of fluids is that small disturbances introduced ata point propagate at a finite velocity. Pressure disturbances in the fluid propagate as

    sound, and their velocity is known as the speed of sound or the acoustic velocity, c.

    Isentropic Process (frictionless, no heat exchange because):

    Ideal Gas and Isentropic Process:

    kRTc

    VINAYAGAMURTHY, SMBS, VIT CHENNAI

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    Compressibility of Fluids: Compression of Gases

    RTp Ideal Gas Law:

    P is pressure, is the density, R is the gas constant, and T is Temperature

    COMPRESSIBILITYOFFLUIDS: SPEEDOFSOUNDSpeed of Sound in Air at 60 F 1117 ft/s or 300 m/s

    Speed of Sound in Water at 60 F 4860 ft/s or 1450 m/s

    If a fluid is truly incompressible, the speed of sound is infinite, however, all

    fluids compress slightly.

    Ideal Gas and Isentropic Process:

    smc

    KkgKJc

    kRTc

    /6.296

    219*)/9.286(*40.1

    Example: A jet aircraft flies at a speed of 250 m/s at an altitude of 10,700 m,

    where the temperature is -54 C. Determine the ratio of the speed of the aircraft,

    V, to the speed of sound, c at the specified altitude. Assume k = 1.40

    VINAYAGAMURTHY, SMBS, VIT CHENNAI

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    84.0

    /6.296

    /250

    Ratio

    sm

    smRatio

    c

    VRatio

    Compressibility of Fluids: Speed of Sound

    Example(Continued):

    The above ratio is known as the Mach Number, Ma

    For Ma < 1 Subsonic Flow

    For Ma > 1 Supersonic Flow

    For Ma > 1 we see shock waves and sonic booms:

    1) Wind Tunnel Visualization known as Schlieren method

    2) Condensation instigated from jet speed allowing us to see a

    shock wave

    VINAYAGAMURTHY, SMBS, VIT CHENNAI

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    VINAYAGAMURTHY, SMBS, VIT CHENNAI


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