Fluid 10

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1 FUNDAMENTALS OF FUNDAMENTALS OF FLUID MECHANICS FLUID MECHANICS Chapter 10 Chapter 10 Flow in Open Channels Flow in Open Channels Jyh Jyh - - Cherng Cherng Shieh Shieh Department of Bio Department of Bio - - Industrial Industrial Mechatronics Mechatronics Engineering Engineering National Taiwan University National Taiwan University

Transcript of Fluid 10

  • 1FUNDAMENTALS OFFUNDAMENTALS OFFLUID MECHANICSFLUID MECHANICS

    Chapter 10Chapter 10Flow in Open ChannelsFlow in Open Channels

    JyhJyh--CherngCherng ShiehShiehDepartment of BioDepartment of Bio--Industrial Industrial MechatronicsMechatronics Engineering Engineering

    National Taiwan UniversityNational Taiwan University

  • 2MAIN TOPICSMAIN TOPICS

    General Characteristics of OpenGeneral Characteristics of Open--Channel FlowChannel FlowSurface WavesSurface WavesEnergy ConsiderationsEnergy ConsiderationsUniform Depth Channel FlowUniform Depth Channel FlowGradually Varies FlowGradually Varies FlowRapidly Varies FlowRapidly Varies Flow

  • 3IntroductionIntroduction

    Open channel flow involves the flows of a liquid in a channel orOpen channel flow involves the flows of a liquid in a channel orconduit that is not completely filled.conduit that is not completely filled.

    There exists a free surface between the flowing fluid (usually wThere exists a free surface between the flowing fluid (usually water) ater) and fluid above it (usually the atmosphere).and fluid above it (usually the atmosphere).

    The main deriving force is the fluid weightThe main deriving force is the fluid weight--gravity forces the fluid gravity forces the fluid to flow downhill.to flow downhill.

    Under steady, fully developed flow conditions, the component if Under steady, fully developed flow conditions, the component if the the weight force in the direction of flow is balanced by the equal aweight force in the direction of flow is balanced by the equal and nd opposite shear force between the fluid and the channel surface.opposite shear force between the fluid and the channel surface.

  • 4Open Channel Flow vs. Pipe FlowOpen Channel Flow vs. Pipe Flow

    There can be no pressure force driving the fluid through the chaThere can be no pressure force driving the fluid through the channel nnel or conduit.or conduit.

    For steady, fully developed channel flow, the pressure distributFor steady, fully developed channel flow, the pressure distribution ion within the fluid is merely hydrostatic.within the fluid is merely hydrostatic.

  • 5Examples of Open Channel FlowExamples of Open Channel Flow

    The natural drainage of water through the numerous creek and rivThe natural drainage of water through the numerous creek and river er systems.systems.

    The flow of rainwater in the gutters of our houses.The flow of rainwater in the gutters of our houses. The flow in canals, drainage ditches, sewers, and gutters along The flow in canals, drainage ditches, sewers, and gutters along roads.roads. The flow of small rivulets, and sheets of water across fields orThe flow of small rivulets, and sheets of water across fields or

    parking lots.parking lots. The flow in the chutes of water rides.The flow in the chutes of water rides.

  • 6Variables in OpenVariables in Open--Channel FlowChannel Flow

    CrossCross--sectional shape.sectional shape. Bends.Bends. Bottom slope variation.Bottom slope variation. Character of its bounding surface.Character of its bounding surface.Most openMost open--channel flow results are based on correlation channel flow results are based on correlation

    obtained from model and fullobtained from model and full--scale experiments.scale experiments. Additional information can be gained from various analytical Additional information can be gained from various analytical

    and numerical efforts.and numerical efforts.

  • 7General Characteristics of General Characteristics of OpenOpen--Channel FlowChannel Flow

  • 8Classification of OpenClassification of Open--Channel FlowChannel Flow

    For openFor open--channel flow, the existence of a free surface allows channel flow, the existence of a free surface allows additional types of flow.additional types of flow.

    The extra freedom that allows the fluid to select its freeThe extra freedom that allows the fluid to select its free--surface surface location and configuration allows important phenomena in openlocation and configuration allows important phenomena in open--channel flow that cannot occur in pipe flow.channel flow that cannot occur in pipe flow.

    The fluid depth, y, varies with time, t, and distance along the The fluid depth, y, varies with time, t, and distance along the channel, x, are used to classify openchannel, x, are used to classify open--channel flow:channel flow:

  • 9Classification Classification -- Type IType I

    Uniform flow (UF): The depth of flow does not vary along the Uniform flow (UF): The depth of flow does not vary along the channel (channel (dy/dxdy/dx=0).=0).

    NonuniformNonuniform flows:flows:Rapidly varying flows (RVF): Rapidly varying flows (RVF):

    The flow depth changes The flow depth changes considerably over a relatively considerably over a relatively short distance dy/dx~1.short distance dy/dx~1.

    Gradually varying flows (GVF): Gradually varying flows (GVF): The flow depth changes slowly The flow depth changes slowly with distance with distance dy/dxdy/dx

  • 10

    Classification Classification -- Type IIType II

    Laminar flow: Re < 500.Laminar flow: Re < 500. Transitional flow: Transitional flow: Turbulent flow: Re > 12,500.Turbulent flow: Re > 12,500.

    = /RVR he V is the average velocity of the fluid.V is the average velocity of the fluid.RRhh is the hydraulic radius of the channel.is the hydraulic radius of the channel.

    Most openMost open--channel flows involve water (which has a fairly small channel flows involve water (which has a fairly small viscosity) and have relatively large characteristic lengths, it viscosity) and have relatively large characteristic lengths, it is is uncommon to have laminar openuncommon to have laminar open--channel flows.channel flows.

  • 11

    Classification Classification -- Type IIIType III

    Critical Flow: Froude number Fr =1.Critical Flow: Froude number Fr =1. SubcriticalSubcritical Flow: Froude number Fr 1.

    lg/VrF =

  • 12

    Surface WaveSurface Wave

  • 13

    Surface WaveSurface Wave

    The distinguishing feature of flows involve a free surface (as iThe distinguishing feature of flows involve a free surface (as in n openopen--channel flows) is the opportunity for the free surface to distorchannel flows) is the opportunity for the free surface to distort t into various shapes.into various shapes.

    The surface of a lake or the ocean is usually distorted into eveThe surface of a lake or the ocean is usually distorted into everr--changing patterns associated with surface waves.changing patterns associated with surface waves.

  • 14

    Kinds of Surface WaveKinds of Surface Wave

    Some of the surface waves are very high, some barely ripple the Some of the surface waves are very high, some barely ripple the surface; some waves are very long, some are short; some are surface; some waves are very long, some are short; some are breaking wave that form white caps, others are quite smooth.breaking wave that form white caps, others are quite smooth.DDsmall amplitude small amplitude DDFiniteFinite--sized solitarysized solitaryDDContinuous sinusoidal shape Continuous sinusoidal shape

  • 15

    small amplitudesmall amplitude Wave Speed Wave Speed 1/51/5

    Consider a single elementary wave of small height, by Consider a single elementary wave of small height, by yy, is , is produced on the surface of a channel by suddenly moving the produced on the surface of a channel by suddenly moving the initially stationary end wall with speed initially stationary end wall with speed VV..

  • 16

    small amplitude small amplitude WaveWave Speed Speed 2/52/5

    The water in the channel was stationary at the initial time, t=0The water in the channel was stationary at the initial time, t=0.. A stationary observer will observe a single wave move down the A stationary observer will observe a single wave move down the

    channel with a wave speed c, with no fluid motion ahead of the channel with a wave speed c, with no fluid motion ahead of the wave and a fluid velocity of wave and a fluid velocity of VV behind the wave.behind the wave.

    The motion is unsteady.The motion is unsteady. For a observer moving along the channel with speed c, the flow wFor a observer moving along the channel with speed c, the flow will ill

    appear steady.appear steady. To this observer, the fluid velocity will be on theTo this observer, the fluid velocity will be on the observerobservers s

    right and to the left of the observer.right and to the left of the observer.i-cVvv =

    iV)(-cVvv +=

    Momentum Equation + Continuity Equation Momentum Equation + Continuity Equation

  • 17

    small amplitudesmall amplitude Wave Speed Wave Speed 3/53/5

    With the assumption of uniform oneWith the assumption of uniform one--dimensional flow, the dimensional flow, the continuity equation becomescontinuity equation becomes

    Similarly, the momentum equationSimilarly, the momentum equation

    b)yy)(Vc(cyb ++=

    yVy

    yV)yy(c

    =+=

    yy

  • 18

    small amplitudesmall amplitude Wave Speed Wave Speed 4/54/5

    cg

    yV =

    yy)y( 2

  • 19

    small amplitudesmall amplitude Wave Speed Wave Speed 5/55/5

    The single wave on the surface is seen by an observer moving witThe single wave on the surface is seen by an observer moving with h the wave speed, c.the wave speed, c.

    Since the pressure is constant at any point on the free surface,Since the pressure is constant at any point on the free surface, the the Bernoulli equation for this frictionless flow isBernoulli equation for this frictionless flow is

    The continuity equationThe continuity equation

    Combining these two equations and using the fact V=cCombining these two equations and using the fact V=c

    0yg

    VVttanconsyg2

    V2 =+=+

    0yVVyttanconsVy =+=

    gyc =

  • 20

    finitefinite--sized solitarysized solitary Wave SpeedWave Speed

    More advanced analysis and experiments show that the wave speed More advanced analysis and experiments show that the wave speed for finitefor finite--sized solitary wavesized solitary wave

    2/1

    yy1gyc

    += gyyy1gyc

    2/1

    >

    +=

    The larger the amplitude, the faster the wave travel.The larger the amplitude, the faster the wave travel.

  • 21

    ContinuousContinuous sinusoidal shapesinusoidal shape Wave Speed Wave Speed 1/21/2

    A more general description of wave motion can be obtained by A more general description of wave motion can be obtained by considering continuous (not solitary) wave of sinusoidal shape.considering continuous (not solitary) wave of sinusoidal shape.DDBy combining waves of various wavelengths, By combining waves of various wavelengths, , and amplitudes, , and amplitudes,

    y.y.DDThe wave speed varies with both the wavelength and fluid depth The wave speed varies with both the wavelength and fluid depth

    asas2/1

    y2tanh2gc

    =& (4)(4)

  • 22

    ContinuousContinuous sinusoidal shapesinusoidal shape Wave Speed Wave Speed 2/22/22/1

    y2tanh2gc

    =&

    Wave speed as a function of wavelength.Wave speed as a function of wavelength.

    =

    =

    2gc

    1y2tanhy

    gyc

    y2y2tanh0y

    ==

    Deep layerDeep layer

    Shallow layerShallow layer

  • 23

    Froude Number Effects Froude Number Effects 1/31/3

    Consider an elementary wave Consider an elementary wave travellingtravelling on the surface of a fluid.on the surface of a fluid. If the fluid layer is stationary, the wave moves to the right wiIf the fluid layer is stationary, the wave moves to the right with th

    speed c relative to the fluid and stationary observer.speed c relative to the fluid and stationary observer.When the fluid is flowing to the left with velocity V.When the fluid is flowing to the left with velocity V.DDIf Vc, the wave will be washed to the left with a speed of V--c.c.

    c/Vg/VrF == lFroudeFroude NumberNumber

    Is the ratio of the fluid Is the ratio of the fluid velocity to the wave speed.velocity to the wave speed.

  • 24

    Froude Number Effects Froude Number Effects 2/32/3

    When a wave is produced on the surface of a moving stream, as When a wave is produced on the surface of a moving stream, as happens when a rock is thrown into a river.happens when a rock is thrown into a river.DDIf V=0, the wave speeds equally in all directions.If V=0, the wave speeds equally in all directions.DDIf V1, are termed supercritical.

  • 25

    Froude Number Effects Froude Number Effects 3/33/3

    DDIf V=c or Fr=1, the upstream propagating wave remains If V=c or Fr=1, the upstream propagating wave remains stationary and the flow is termed critical.stationary and the flow is termed critical.

  • 26

    Energy ConsiderationsEnergy Considerations

  • 27

    Energy Considerations Energy Considerations 1/31/3

    x and y are taken as the x and y are taken as the distance along the distance along the channel bottom and the channel bottom and the depth normal to the depth normal to the bottom.bottom.

    l21

    0zzS = The slope of the channel bottom or bottom The slope of the channel bottom or bottom

    slope is constant over the segmentslope is constant over the segment

    Very small for most openVery small for most open--channel flows.channel flows.

  • 28

    Energy Considerations Energy Considerations 2/32/3

    With the assumption of a uniform velocity profile across any secWith the assumption of a uniform velocity profile across any section tion of the channel, the oneof the channel, the one--dimensional energy equation becomedimensional energy equation become

    (5)(5)L2222

    1

    211 hz

    g2Vpz

    g2Vp +++=++

    hL is the head loss due to viscous effects between sections (1) and (2).

    (5)(5)

    2211

    o21y/py/p

    Szz==

    = lL

    22

    2o2

    11 hg2

    VyS

    g2V

    y ++=++ l (6)(6)

  • 29

    Energy Considerations Energy Considerations 3/33/3

    (6)(6)

    l/hS Lf =l)of

    21

    22

    21 SS(g2VVyy += (7)(7)

    (7)(7)

    For a horizontal channel bottom (S0=0) and negligible head loss (Sf=0)

    g2VVyy

    21

    22

    21=

  • 30

    Specific Energy Specific Energy 1/41/4

    Define specific energy, EDefine specific energy, E

    g2VyE

    2+=

    l)SS(EE of21 +=(8)(8)

    (9)(9)

    2211 zEzE +=+(9)(9) The sum of the specific energy and The sum of the specific energy and the elevation of the channel bottom the elevation of the channel bottom remains constant.remains constant.This a statement of the Bernoulli This a statement of the Bernoulli equation.equation.

    Head losses are negligible, Head losses are negligible, SSff=0=0

    12o zzS = l

  • 31

    Specific Energy Specific Energy 2/42/4

    If the crossIf the cross--sectional shape is a rectangular of width bsectional shape is a rectangular of width b

    For a given channelFor a given channelb= constantb= constantq = constantq = constantE = E (y) E = E (y) Specific energy diagramSpecific energy diagram

    2

    2

    gy2qyE += (10)(10)

    Where q is the Where q is the flowrateflowrate per unit width, q=Q/b=per unit width, q=Q/b=Vyb/bVyb/b==VyVy

  • 32

    Specific Energy Specific Energy 3/43/4

    2

    2

    gy2qyE +=

    For a given q and E, equation (10) is a For a given q and E, equation (10) is a cubic equation with three solutions , cubic equation with three solutions , yysupsup, , yysubsub, and , and yynegneg..If E >If E >EEminmin, two solutions are positive , two solutions are positive and and yynegneg is negative (has no physical is negative (has no physical meaning and can be ignored).meaning and can be ignored).These two depths are term alternative These two depths are term alternative depths.depths.

    (10)(10)

  • 33

    Specific Energy Specific Energy 4/44/4

    Approach y=EApproach y=EVery deep and very slowlyVery deep and very slowly

    E > E > EEminminTwo possible depths of flow, Two possible depths of flow, one one subcriticalsubcritical and the other and the other supercriticalsupercritical

    subsup

    subsup

    VV

    yy

    > y> y11 ).).

  • 37

    Example 10.1 Example 10.1 SolutionSolution2/22/2

    On the other hand, if the gate remains fixed so that the downstrOn the other hand, if the gate remains fixed so that the downstream eam depth remain fixed (ydepth remain fixed (y22 = y= y22 ), the ), the flowrateflowrate will increase as the will increase as the upstream depth increases to y upstream depth increases to y 11 > y> y11..

    q>q0

  • 38

    Example 10.2 Specific Energy diagram Example 10.2 Specific Energy diagram QuantitativeQuantitativezz Water flows up a 0.5Water flows up a 0.5--ftft--tall ramp in a constant width rectangular tall ramp in a constant width rectangular

    channel at a rate of q = 5.75 ftchannel at a rate of q = 5.75 ft22/s as shown in Fig. E10.2a. (For now /s as shown in Fig. E10.2a. (For now disregard the disregard the bumpbump) If the upstream depth is 2.3 ft, determine the ) If the upstream depth is 2.3 ft, determine the elevation of the water surface downstream of the ramp, yelevation of the water surface downstream of the ramp, y22 + z+ z22. . Neglect viscous effects.Neglect viscous effects.

  • 39

    Example 10.2 Example 10.2 SolutionSolution1/41/4

    With SWith S0 0 ll =z=z11--zz22 and and hhLL=0, conservation of energy requires that=0, conservation of energy requires that

    4.64Vy90.1

    zg2

    Vpzg2

    Vp

    22

    2

    2

    222

    1

    211

    +=

    ++=++

    s/ft75.5Vy

    VyVy2

    22

    1122

    ==

    0513.0y90.1y 2232 =+

    (10.2(10.2--1)1)

    The continuity equationThe continuity equation

    (10.2(10.2--2)2) ft466.0yft638.0ft72.1y

    2

    2=

    =

  • 40

    Example 10.2 Example 10.2 SolutionSolution2/42/4

    The corresponding elevations of the free surface are eitherThe corresponding elevations of the free surface are either

    ft14.1ft50.0ft638.0zyft22.2ft50.0ft72.1zy

    22

    22=+=+

    =+=+

    Which of these flows is to be expected?Which of these flows is to be expected?This can be answered by use of the specific energy diagram This can be answered by use of the specific energy diagram obtained from Eq.(10), which for this problem isobtained from Eq.(10), which for this problem is

    2y513.0yE +=

    The diagram is shown in Fig.E10.2(b).The diagram is shown in Fig.E10.2(b).

  • 41

    Example 10.2 Example 10.2 SolutionSolution3/43/4

  • 42

    Example 10.2 Example 10.2 SolutionSolution4/44/4

    The upstream condition corresponds to The upstream condition corresponds to subcriticalsubcritical flow; the flow; the downstream condition is either downstream condition is either subcriticalsubcritical or supercritical, or supercritical, corresponding to points 2 or 2corresponding to points 2 or 2..

    Note that since ENote that since E11=E=E22+(z+(z22--zz11)=E)=E22+0.5 ft, it follows that the +0.5 ft, it follows that the downstream conditions are located to 0.5 ft to the left of the downstream conditions are located to 0.5 ft to the left of the upstream conditions on the diagram.upstream conditions on the diagram.

    .. The surface elevation is.. The surface elevation is

    ft22.2ft50.0ft72.1zy 22 =+=+

  • 43

    Channel Depth Variations Channel Depth Variations 1/31/3

    Consider gradually varying flows.Consider gradually varying flows. For such flows, For such flows, dy/dxdy/dx

  • 44

    Channel Depth Variations Channel Depth Variations 2/32/3

    dxdy

    yV

    dxdy

    yq

    dxdV

    yqV

    2===

    dxdyF

    dxdy

    gyV

    dxdV

    gV 2

    r

    2==

    (12)(12)of

    0L

    SSdxdy

    dxdV

    gV

    Sdxdy

    dxdV

    gV

    dxdh

    =+

    ++=

    For a given For a given flowrateflowrate per unit width, q, in a rectangular channel of per unit width, q, in a rectangular channel of constant width b, we haveconstant width b, we have

    (12)(12) (13)(13)

  • 45

    Channel Depth Variations Channel Depth Variations 3/33/3

    )F1(SS

    dxdy

    2r

    of

    =Sub. (13) into (12)Sub. (13) into (12) (14)(14)

    Depends on the local slope of the channel bottom, the Depends on the local slope of the channel bottom, the slope of the energy line, and the slope of the energy line, and the FroudeFroude number.number.

  • 46

    Uniform Depth Channel FlowUniform Depth Channel Flow

  • 47

    Uniform Depth Channel Flow Uniform Depth Channel Flow 1/31/3

    Many channels are designed to carry fluid at a uniform depth allMany channels are designed to carry fluid at a uniform depth allalong their length.along their length.DDIrrigation canals.Irrigation canals.DDNature channels such as rivers and creeks.Nature channels such as rivers and creeks.

    Uniform depth flow (Uniform depth flow (dy/dxdy/dx=0) can be accomplished by adjusting the =0) can be accomplished by adjusting the bottom slope, Sbottom slope, S00, so that it precisely equal the slope of the energy , so that it precisely equal the slope of the energy line, line, SSff..

    A balance between the potential energy lost by the fluid as it cA balance between the potential energy lost by the fluid as it coasts oasts downhill and the energy that is dissipated by viscous effects (hdownhill and the energy that is dissipated by viscous effects (head ead loss) associated with shear stress throughout the fluid.loss) associated with shear stress throughout the fluid.

  • 48

    Uniform Depth Channel Flow Uniform Depth Channel Flow 2/32/3

    Uniform flow in an open channel.Uniform flow in an open channel.

  • 49

    Uniform Depth Channel Flow Uniform Depth Channel Flow 3/33/3

    Typical velocity and shear stress distributions in an open channTypical velocity and shear stress distributions in an open channel: el: ((aa) velocity distribution throughout the cross section. () velocity distribution throughout the cross section. (bb) shear ) shear stress distribution on the wetted perimeter.stress distribution on the wetted perimeter.

  • 50

    The The ChezyChezy & Manning Equation & Manning Equation 1/61/6

    Control volume for uniform flow in an open channel.Control volume for uniform flow in an open channel.

  • 51

    The The ChezyChezy & Manning Equation & Manning Equation 2/62/6

    0)VV(QF 12x ==0sinWPFF w21 =+ l (15)(15)

    Under the assumption of steady uniform flow, the x component of Under the assumption of steady uniform flow, the x component of the momentum equationthe momentum equation

    where Fwhere F11 and Fand F22 are the hydrostatic pressure forces across either end are the hydrostatic pressure forces across either end of the control volume.of the control volume.P is wetted perimeter.P is wetted perimeter.

  • 52

    The The ChezyChezy & Manning Equation & Manning Equation 3/63/6

    yy11=y=y22 FF11=F=F22(15)(15)

    PARAW

    PsinW

    0sinWP

    hw

    w

    ====+

    ll

    l

    oho

    w SrRPSA == l

    l(16)(16)

    Wall shear stress is proportional to the dynamic pressureWall shear stress is proportional to the dynamic pressure2

    V2w

    2VK

    2

    w =K is a constant dependent upon the roughness of the pipeK is a constant dependent upon the roughness of the pipe

    (Chapter 8)(Chapter 8)

  • 53

    The The ChezyChezy & Manning Equation & Manning Equation 4/64/6

    (16)(16) (17)(17)

    C is termed the C is termed the ChezyChezy coefficientcoefficient

    Was developed in 1768 by A. Was developed in 1768 by A. ChezyChezy (1718(1718--1798), a French 1798), a French engineer who designed a canal for the Paris water supply.engineer who designed a canal for the Paris water supply.

    oh

    2SrR

    2VK = ohSRCV =

    ChezyChezy equationequation

    (17)(17) 2/1oSV

    hRV

    ReasonableReasonable

    3/2hRV

    Manning EquationManning Equation

  • 54

    The The ChezyChezy & Manning Equation & Manning Equation 5/65/6

    In 1889, R. manning (1816In 1889, R. manning (1816--1897), an Irish engineer, developed the 1897), an Irish engineer, developed the following somewhat modified equation for openfollowing somewhat modified equation for open--channel flow to channel flow to more accurately describe the more accurately describe the RRhh dependence:dependence:

    Manning equationManning equation(18)(18)

    n is the Manning resistance coefficient.n is the Manning resistance coefficient.Its value is dependent on the surface material Its value is dependent on the surface material of the channelof the channels wetted perimeter and is s wetted perimeter and is obtained from experiments.obtained from experiments.It has the units of s/mIt has the units of s/m1/31/3 or s./ftor s./ft1/31/3

    nSRV

    2/1o

    3/2h=

  • 55

    The The ChezyChezy & Manning Equation & Manning Equation 6/66/6

    (19)(19) Where Where =1 if SI units are =1 if SI units are used, used, =1.49 if BG units =1.49 if BG units are used.are used.

    2/1o

    3/2h SRn

    V =(18)(18)

    (20)(20)2/1o3/2

    h SARnQ =

    5/25/3

    2/1o

    3/2

    2/1o

    3/52/1

    o

    3/2P

    kSnQA

    PSA

    nS

    PAA

    nQ

    ==

    =

    The best hydraulic cross section is defined as the section of miThe best hydraulic cross section is defined as the section of minimum nimum area for a given area for a given flowrateflowrate Q, slope, SQ, slope, Soo, and the roughness coefficient, n., and the roughness coefficient, n.

    PAR h = constant

    A channel with minimum A is one with a minimum P.A channel with minimum A is one with a minimum P.

  • 56

    Value of the Manning Coefficient, nValue of the Manning Coefficient, n

  • 57

    Uniform Depth ExamplesUniform Depth Examples

  • 58

    Example 10.3 Uniform Flow, Determine Example 10.3 Uniform Flow, Determine Flow RateFlow Ratezz Water flows in the canal of trapezoidal cross section shown in FWater flows in the canal of trapezoidal cross section shown in Fig. ig.

    E10.3a. The bottom drops 1.4 ft per 1000 ft of length. DetermineE10.3a. The bottom drops 1.4 ft per 1000 ft of length. Determine the the flowrateflowrate if the canal is lined with new smooth concrete. Determine if the canal is lined with new smooth concrete. Determine the Froude number for this flow. the Froude number for this flow.

  • 59

    Example 10.3 Example 10.3 SolutionSolution1/21/2

    (20)(20) =1.49 if BG units are used.=1.49 if BG units are used.

    ft25.3P/ARft6.27)ft40sin/5(2ft12P

    ft8.89ft40tan5ft5)ft5(ft12A

    h

    2

    ===+=

    =

    +=

    2/1o

    3/2h SARn

    Q =

    cfs915n98.10)0014.0()ft25.3)(ft8.89(

    n49.1Q 2/13/22 ===

    From Table 10.1, n=0.012From Table 10.1, n=0.012

    804.0...gyVFrs/ft2.10A/QV =====

  • 60

    Example 10.3 Example 10.3 SolutionSolution2/22/2

  • 61

    Example 10.4 Uniform Flow, Determine Example 10.4 Uniform Flow, Determine Flow DepthFlow Depthzz Water flows in the channel shown in Fig. E10.3 at a rate o Q = 1Water flows in the channel shown in Fig. E10.3 at a rate o Q = 10.0 0.0

    mm33/s. If the canal lining is weedy, determine the depth of the flo/s. If the canal lining is weedy, determine the depth of the flow.w.

  • 62

    Example 10.4 Example 10.4 SolutionSolution

    y=1.50 my=1.50 m

    66.3y11.3y66.3y19.1

    PAR

    66.3y11.340siny266.3P

    y66.3y19.1A

    2

    h

    2

    ++==

    +=

    +=

    +=

    ...03.00.1SAR

    n10Q 2/1o

    3/2h ===

    From Table 10.1, n=0.030From Table 10.1, n=0.030

    0)66.3y11.3(515)y66.3y19.1( 252 =++

  • 63

    Example 10.5 Uniform Flow, Maximum Example 10.5 Uniform Flow, Maximum Flow RateFlow Ratezz Water flows in a round pipe of diameter D at a depth of 0 Water flows in a round pipe of diameter D at a depth of 0 y y D, D,

    as shown in Fig. E10.5a. The pipe is laid on a constant slope ofas shown in Fig. E10.5a. The pipe is laid on a constant slope of SS00, , and the Manning coefficient is n. At what depth does the maximumand the Manning coefficient is n. At what depth does the maximumflowrateflowrate occur? Show that for certain occur? Show that for certain flowrateflowrate there are two depths there are two depths possible with the same possible with the same flowrateflowrate. Explain this behavior.. Explain this behavior.

  • 64

    Example 10.5 Example 10.5 SolutionSolution1/21/2

    (20)(20) =1.49 if BG units are used.=1.49 if BG units are used.

    ===

    =

    4)sin(D

    PAR

    2DP

    )sin(8

    DA

    h

    2

    2/1o

    3/2h SARn

    Q =

    = 3/2

    3/5

    3/2

    3/82/1

    o)sin(

    )4(8DS

    nQ

    This can be written in terms of the flow depth by usingThis can be written in terms of the flow depth by using

    )]2/cos(1[2Dy =

  • 65

    Example 10.5 Example 10.5 SolutionSolution2/22/2

    D938.0ywhenQQ max ==

    A graph of A graph of flowrateflowrate versus flow depth, Q = versus flow depth, Q = Q(yQ(y), has the ), has the characteristic indicated in Fig. E10.5(b).characteristic indicated in Fig. E10.5(b).

    The maximum The maximum flowrateflowrate occurs when y=0.938D, or occurs when y=0.938D, or =303=303

  • 66

    Example 10.6 Uniform Flow, Effect of Example 10.6 Uniform Flow, Effect of Bottom SlopeBottom Slopezz Water flows in a rectangular channel of width b = 10 m that has Water flows in a rectangular channel of width b = 10 m that has a a

    Manning coefficient of n = 0.025. Plot a graph of Manning coefficient of n = 0.025. Plot a graph of flowrateflowrate, Q, as a , Q, as a function of slope Sfunction of slope S00, indicating lines of constant depth and lines of , indicating lines of constant depth and lines of constant Froude number.constant Froude number.

  • 67

    Example 10.6 Example 10.6 SolutionSolution1/21/2

    (19)(19)

    )y2b(by

    PARy10byA h +====

    2/1o

    3/22/1

    o3/2

    h Sy210y10

    025.00.1SR

    nV

    +==

    3/42

    o

    2/1o

    3/22/1

    y5y5yFr00613.0S

    Sy210

    y10025.00.1Fr)gy(

    +=

    +=

    (10.6(10.6--1)1)

    (10.6(10.6--2)2)

  • 68

    Example 10.6 Example 10.6 SolutionSolution2/22/2

    For given value of Fr, we pick For given value of Fr, we pick various value of y, determine the various value of y, determine the corresponding value of Scorresponding value of Soo from from EqEq(10.6(10.6--2)2), and then calculate Q=VA, , and then calculate Q=VA, with V from either with V from either EqEq (10.6(10.6--1)1) or or V=(gy)V=(gy)1/21/2FrFr. .

    The results are indicated in The results are indicated in Fig. E10.6Fig. E10.6

  • 69

    Example 10.7 Uniform Flow, Variable Example 10.7 Uniform Flow, Variable RoughnessRoughnesszz Water flows along the drainage canal having the properties shownWater flows along the drainage canal having the properties shown in in

    Fig. E10.7a. If the bottom slope is SFig. E10.7a. If the bottom slope is S0 0 = 1 ft/500 ft=0.002, estimate = 1 ft/500 ft=0.002, estimate the the flowrateflowrate when the depth is y = 0.8 ft + 0.6 ft = 1.4 ft.when the depth is y = 0.8 ft + 0.6 ft = 1.4 ft.

  • 70

    Example 10.7 Example 10.7 SolutionSolution

    2/1o

    3/2hi

    ii SRAn

    49.1Qi

    =

    321 QQQQ ++=

    s/ft8.16...Q 3==

  • 71

    Example 10.8 Uniform Flow, Best Example 10.8 Uniform Flow, Best Hydraulic Cross SectionHydraulic Cross Sectionzz Water flows uniformly in a Water flows uniformly in a

    rectangular channel of width rectangular channel of width b and depth y. Determine the b and depth y. Determine the aspect ratio, aspect ratio, b/yb/y, for the best , for the best hydraulic cross section.hydraulic cross section.

  • 72

    Example 10.8 Example 10.8 SolutionSolution1/31/3

    (20)(20) =1.49 if BG units are used.=1.49 if BG units are used.

    )Ay2(Ay

    )y2b(A

    )y2b(by

    PAR

    y2bPbyA

    2h +=+=+==+==

    2/1o

    3/2h SARn

    Q =

    2/1o

    3/2

    2 S)Ay2(AyA

    nQ

    +=

    2/3

    2/1o

    22/5

    SnQK)Ay2(KyA

    =+=

    constantconstant

  • 73

    Example 10.8 Example 10.8 SolutionSolution2/32/3

    The best hydraulic section is the one that gives the minimum A The best hydraulic section is the one that gives the minimum A for all y. That is, for all y. That is, dA/dydA/dy = 0.= 0.

    ky4A

    dydAy4KAy

    dydAA

    250

    dydA

    2/5

    2/52/3

    =

    +=+=

    2y/b =The rectangular with the best hydraulic cross section twice The rectangular with the best hydraulic cross section twice as wide as it is deep, oras wide as it is deep, or

    byy2 2 =

  • 74

    Example 10.8 Example 10.8 SolutionSolution3/33/3

    The best hydraulic cross section for other shapesThe best hydraulic cross section for other shapes

  • 75

    Gradually Varied FlowGradually Varied Flow

    1dxdy

  • 76

    Gradually Varied Flow Gradually Varied Flow 1/21/2

    Open channel flows are classified as uniform depth, gradually Open channel flows are classified as uniform depth, gradually varying or rapidly varying.varying or rapidly varying.

    If the channel bottom slope is equal to the slope of the energy If the channel bottom slope is equal to the slope of the energy line, line, SSoo==SSff, the flow depth is constant, , the flow depth is constant, dy/dxdy/dx=0.=0.DDThe loss in potential energy of the fluid as it flows downhill iThe loss in potential energy of the fluid as it flows downhill is s

    exactly balanced by the dissipation of energy through viscous exactly balanced by the dissipation of energy through viscous effects.effects.

    If the bottom slope and the energy line slope are not equal, theIf the bottom slope and the energy line slope are not equal, the flow flow depth will vary along the channel.depth will vary along the channel.

  • 77

    Gradually Varied Flow Gradually Varied Flow 2/22/2

    )F1(SS

    dxdy

    2r

    of

    = (14)(14)

    The sign of The sign of dy/dxdy/dx, that is, whether the flow depth , that is, whether the flow depth increase or decrease with distance along the channel increase or decrease with distance along the channel depend on depend on SSff --SSoo ad 1ad 1--FrFr22

  • 78

    Classification of Surface Shapes Classification of Surface Shapes 1/31/3

    The character of a gradually varying flow is often classified inThe character of a gradually varying flow is often classified in terms terms of the actual channel slope, Sof the actual channel slope, Soo, compared with the slope required to , compared with the slope required to produce uniform critical flow, Sproduce uniform critical flow, Sococ..

    The character of a gradually varying flow depends on whether theThe character of a gradually varying flow depends on whether thefluid depth is less than or greater than the uniform normal deptfluid depth is less than or greater than the uniform normal depth, h, yynn..

    12 possible surface configurations12 possible surface configurations

  • 79

    Classification of Surface Shapes Classification of Surface Shapes 2/32/3

    FrFryyccFr>1 : y1 : y

  • 80

    Examples of Gradually Varies Flows Examples of Gradually Varies Flows 1/51/5

    Typical surface configurations for nonuniform depth flow with a mild slope. S0 < S0c.

    DropDrop--down profiledown profile

    Backwater curveBackwater curve

  • 81

    Examples of Gradually Varies Flows Examples of Gradually Varies Flows 2/52/5

    Typical surface configurations for Typical surface configurations for nonuniformnonuniform depth flow with a depth flow with a critical slope. Scritical slope. S00 = = SS0c0c..

  • 82

    Examples of Gradually Varies Flows Examples of Gradually Varies Flows 3/53/5

    Typical surface Typical surface configurations for configurations for nonuniformnonuniform depth depth flow with a steep flow with a steep slope. Sslope. S00 > > SS0c0c..

  • 83

    Examples of Gradually Varies Flows Examples of Gradually Varies Flows 4/54/5

    Typical surface configurations for Typical surface configurations for nonuniformnonuniform depth flow with a depth flow with a horizontal slope. Shorizontal slope. S00 =0.=0.

  • 84

    Examples of Gradually Varies Flows Examples of Gradually Varies Flows 5/55/5

    Typical surface configurations for Typical surface configurations for nonuniformnonuniform depth flow with a depth flow with a adverse slope. Sadverse slope. S00

  • 85

    Classification of Surface Shapes Classification of Surface Shapes 3/33/3

    The free surface is relatively free to conform to the shape thatThe free surface is relatively free to conform to the shape thatsatisfies the governing mass, momentum, and energy equations.satisfies the governing mass, momentum, and energy equations.

    The actual shape of the surface is often very important in the dThe actual shape of the surface is often very important in the design esign of openof open--channel devices or in the prediction of flood levels in channel devices or in the prediction of flood levels in natural channels.natural channels.

    The surface shape, y=The surface shape, y=y(xy(x), can be calculated by solving ), can be calculated by solving the governing differential equation obtained from a the governing differential equation obtained from a combination of the Manning equation (20) and the combination of the Manning equation (20) and the energy equation (14).energy equation (14).

    Numerical techniques have been developed and Numerical techniques have been developed and used to predict openused to predict open--channel surface shapes.channel surface shapes.

  • 86

    Rapidly Varied FlowRapidly Varied Flow

    1~dxdy

  • 87

    Rapidly Varied FlowRapidly Varied Flow

    Rapidly varied flow: flow depth changes occur over a relatively Rapidly varied flow: flow depth changes occur over a relatively short distance.short distance.DDQuite complex and difficult to analyze in a precise fashion.Quite complex and difficult to analyze in a precise fashion.DDMany approximate results can be obtained by using a simple Many approximate results can be obtained by using a simple

    oneone--dimensional model along with appropriate experimentally dimensional model along with appropriate experimentally determined coefficients when necessary.determined coefficients when necessary.

  • 88

    Occurrence of Rapidly Varied Flow Occurrence of Rapidly Varied Flow 1/21/2

    Flow depth changes significantly un a short distance: The flow Flow depth changes significantly un a short distance: The flow changes from a relatively shallow, high speed condition into a changes from a relatively shallow, high speed condition into a relatively deep, low speed condition within a horizontal distancrelatively deep, low speed condition within a horizontal distance of e of just a few channel depths.just a few channel depths.

    Hydraulic Jump

  • 89

    Occurrence of Rapidly Varied Flow Occurrence of Rapidly Varied Flow 2/22/2

    Sudden change in the channel geometry such as the flow in an Sudden change in the channel geometry such as the flow in an expansion or contraction section of a channel.expansion or contraction section of a channel.

    Rapidly varied flow may occur in a Rapidly varied flow may occur in a channel transition section.channel transition section.

  • 90

    Example of Rapidly Varied Flow Example of Rapidly Varied Flow 1/21/2

    The scouring of a river bottom in the neighborhood of a bridge pThe scouring of a river bottom in the neighborhood of a bridge pier.ier.

    The complex threeThe complex three--dimensional flow structure around a bridge pier.dimensional flow structure around a bridge pier.

    Responsible for Responsible for the erosion near the erosion near the foot of the the foot of the bridge pier.bridge pier.

  • 91

    Example of Rapidly Varied Flow Example of Rapidly Varied Flow 2/22/2

    Many openMany open--channel channel flowflow--measuring devicesmeasuring devices are based on are based on principles associated with rapidly varied flows.principles associated with rapidly varied flows.

    DDBroadBroad--crested weirs.crested weirs.DDSharpSharp--crested weirs.crested weirs.DDCritical flow flumes.Critical flow flumes.DDSluice gates.Sluice gates.

  • 92

    Hydraulic JumpHydraulic Jump

  • 93

    The Hydraulic Jump The Hydraulic Jump 1/61/6

    Under certain conditions it is possible that the fluid depth wilUnder certain conditions it is possible that the fluid depth will l change very rapidly over a short length of the channel without achange very rapidly over a short length of the channel without any ny change in the channel configuration.change in the channel configuration.DDSuch changes in depth can be approximated as a discontinuity in Such changes in depth can be approximated as a discontinuity in

    the free surface elevation (the free surface elevation (dy/dxdy/dx==).).DDThis near discontinuity is called a This near discontinuity is called a hydraulic jumphydraulic jump....

  • 94

    The Hydraulic Jump The Hydraulic Jump 2/62/6

    A simplest type of hydraulic jump in a horizontal, rectangular cA simplest type of hydraulic jump in a horizontal, rectangular channel.hannel.

    Assume that the flow at sections (1) and (2) is nearly uniform, Assume that the flow at sections (1) and (2) is nearly uniform, steady, steady, and oneand one--dimensional.dimensional.

  • 95

    The Hydraulic Jump The Hydraulic Jump 3/63/6

    The x component of the momentum equationThe x component of the momentum equation)VV(byV)VV(QFF 1211221 ==

    2/byApF 2111c1 ==2/byApF 2222c2 ==

    (21)(21))VV(gyV

    2y

    2y

    211

    22

    21 =

    The conservation of mass equationThe conservation of mass equation (22)(22)QbVybVy 2211 ==The energy equationThe energy equation L

    22

    2

    21

    1 hg2Vy

    g2Vy ++=+ (23)(23)

    The head loss is due to the violent turbulent mixing and dissipaThe head loss is due to the violent turbulent mixing and dissipation.tion.

  • 96

    The Hydraulic Jump The Hydraulic Jump 4/64/6

    (21)+(22)+(23)(21)+(22)+(23) Nonlinear equationsNonlinear equations

    One solution is yOne solution is y11=y=y22, V, V11=V=V22, , hhLL=0=0Other solutions?Other solutions?

    (21)+(22)(21)+(22)

    0F2yy

    yy 2

    1r1

    22

    1

    2 =

    +

    += 21r1

    2 F81121

    yy

    1

    11

    gyVFr =

    ++= 21r1

    2 F81121

    yy

    )yy(gy

    yVVy

    yVgyV

    2y

    2y

    212

    121

    12

    111122

    21 =

    =

    SolutionsSolutions (24)(24)

  • 97

    The Hydraulic Jump The Hydraulic Jump 5/65/6

    (23)(23)

    +=

    2

    2

    121r

    1

    2

    1

    Lyy1

    2F

    yy1

    yh

    (25)(25)

    (24)+(25)(24)+(25) Depth ratio and dimensionless head loss across a Depth ratio and dimensionless head loss across a hydraulic jump as a function of upstream hydraulic jump as a function of upstream FroudeFroudenumber.number.

  • 98

    The Hydraulic Jump The Hydraulic Jump 6/66/6

    The head loss is negative if FrThe head loss is negative if Fr11

  • 99

    Classification of Hydraulic Jump Classification of Hydraulic Jump 1/21/2

    The actual structure of a hydraulic jump is a complex function oThe actual structure of a hydraulic jump is a complex function of Frf Fr11, , even though the depth ratio and head loss are given quite accuraeven though the depth ratio and head loss are given quite accurately tely by a simple oneby a simple one--dimensional flow analysis.dimensional flow analysis.

    A detailed investigation of the flow indicates that there are A detailed investigation of the flow indicates that there are essentially five type of surface and jump conditions.essentially five type of surface and jump conditions.

  • 100

    Classification of Hydraulic Jump Classification of Hydraulic Jump 2/22/2

  • 101

    Hydraulic Jump Variations Hydraulic Jump Variations 1/21/2

    Hydraulic jumps can occur in a variety o channel flow Hydraulic jumps can occur in a variety o channel flow configurations, not just in horizontal, rectangular channels as configurations, not just in horizontal, rectangular channels as discussed above.discussed above.

    Other common types of hydraulic jumps include those that occur iOther common types of hydraulic jumps include those that occur in n sloping channels and the submerged hydraulic jumps that can occusloping channels and the submerged hydraulic jumps that can occur r just downstream of a sluice gate.just downstream of a sluice gate.

  • 102

    Hydraulic Jump Variations Hydraulic Jump Variations 2/22/2

    Hydraulic jump variations:Hydraulic jump variations:((aa) jump caused by a change ) jump caused by a change in channel slope, in channel slope, ((bb) submerged jump) submerged jump

  • 103

    Example 10.9 Hydraulic JumpExample 10.9 Hydraulic Jump

    zz Water on the horizontal apron of the 100Water on the horizontal apron of the 100--ftft--wide spillway shown in wide spillway shown in Fig. E10.9a has a depth o 0.60 ft and a velocity of 18 ft/s. DetFig. E10.9a has a depth o 0.60 ft and a velocity of 18 ft/s. Determine ermine the depth, ythe depth, y22, after the jump, the Froude numbers before and after , after the jump, the Froude numbers before and after the jump, Frthe jump, Fr11 and Frand Fr22, and the power dissipated, P, and the power dissipated, Pdd, with the jump., with the jump.

  • 104

    Example 10.9 Example 10.9 SolutionSolution1/31/3

    10.4)ft60.0)(s/ft2.32(

    s/ft18gyVFr

    21

    11 ===

    32.5...F81121

    yy 2

    1r1

    2 ==

    ++=

    Conditions across the jump are determined by the upstream Conditions across the jump are determined by the upstream FroudeFroude numbernumber

    (24)(24)

    ft19.3)ft60.0(32.5y2 ==Since QSince Q11=Q=Q22, or V, or V22=(y=(y11VV11)/y)/y22=3.39ft/s=3.39ft/s

  • 105

    Example 10.9 Example 10.9 SolutionSolution2/32/3

    334.0)ft19.3)(s/ft2.32(

    s/ft39.3gyVFr

    21

    22 ===

    L11Ld hVbyQhP ==

    The poser dissipated, Pd, by viscous effects within the jump canThe poser dissipated, Pd, by viscous effects within the jump canbe determined from the head lossbe determined from the head loss

    ft26.2...g2

    Vyg2

    Vyh22

    2

    21

    1L ==

    +

    +=(23)(23)

    hp277s/lbft1052.1...hVbyQhP 5L11Ld ====

  • 106

    Example 10.9 Example 10.9 SolutionSolution3/33/3

    22

    2

    21121

    y81.1y

    gy2qyE

    s/ft8.10VybQqqq

    +=+=

    =====

    Various upstream depthVarious upstream depth

  • 107

    Weirs and GateWeirs and Gate

  • 108

    WeirWeir

    A weir is an obstruction on a channel bottom over which the fluiA weir is an obstruction on a channel bottom over which the fluid d must flow.must flow.

    Weir provides a convenient method of determining the Weir provides a convenient method of determining the flowrateflowrate in in an open channel in terms of a single depth measurement.an open channel in terms of a single depth measurement.

  • 109

    SharpSharp--Crested Weir Crested Weir 1/41/4

    A sharpA sharp--Crested weir is essentially a verticalCrested weir is essentially a vertical--edged flat plate placed edged flat plate placed across the channel.across the channel.

    The fluid must flow across the sharp edge and drop into the poolThe fluid must flow across the sharp edge and drop into the pooldownstream of the weir plate.downstream of the weir plate.

  • 110

    SharpSharp--Crested Weir Crested Weir -- Geometry Geometry 2/42/4

    SharpSharp--crested weir plate geometry: (a) rectangular, (b) triangular, (ccrested weir plate geometry: (a) rectangular, (b) triangular, (c) ) trapezoidal. trapezoidal.

  • 111

    SharpSharp--Crested Weir Crested Weir FlowrateFlowrate 3/43/4

    Assume that the velocity profile upstream of the weir plate Assume that the velocity profile upstream of the weir plate is uniform and that the pressure within the is uniform and that the pressure within the nappenappe is is atmosphere.atmosphere.

    Assume that the Assume that the fluid flows fluid flows horizontally over the horizontally over the weir plate with a weir plate with a nonuniformnonuniform velocity velocity profile.profile.

  • 112

    SharpSharp--Crested Weir Crested Weir FlowrateFlowrate 4/44/4

    With PWith PBB=0, the Bernoulli equation for flow along the arbitrary =0, the Bernoulli equation for flow along the arbitrary streamline Astreamline A--B indicated can be written asB indicated can be written as

    g2VpH

    g2Vpz

    21

    w

    21A

    A ++=++

    +=

    g2Vhg2u

    21

    2

    g2u)hPH(z

    g2Vp 22

    wA

    21A ++=++ (26)(26)

    Since the total head for any particle along the vertical sectionSince the total head for any particle along the vertical section (1) is (1) is the samethe same

    (26)(26) ==== Hh 0h 22 dhudAuQ l (27)(27)

  • 113

    Rectangular Weir Rectangular Weir FlowrateFlowrate 1/21/2

    For a rectangular weir, For a rectangular weir, ll=b=b

    (28)(28)

    (28)(28) (29)(29)

    +=

    +=

    2/321

    2/321

    H

    0

    2/121

    g2V

    g2VHbg2

    32dh

    g2Vhbg2Q

    Hg2

    V21

  • 114

    Rectangular Weir Rectangular Weir FlowrateFlowrate 2/22/2

    CCwrwr is the rectangular weir coefficient. is the rectangular weir coefficient. CCwrwr is function of Reynolds number (viscous effects), Weber is function of Reynolds number (viscous effects), Weber number (surface tension effects), H/number (surface tension effects), H/PPww (geometry effects).(geometry effects).

    In most practical situations, the Reynolds and Weber number In most practical situations, the Reynolds and Weber number effects are negligible, and the following correction can be usedeffects are negligible, and the following correction can be used..

    (31)(31)

    +=

    wwr P

    H075.0611.0C

  • 115

    Triangular Weir Triangular Weir FlowrateFlowrate 1/21/2

    An experimentally determined An experimentally determined triangular weir coefficient, Ctriangular weir coefficient, Cwtwt, is , is used to account for the real world effects neglected in the analused to account for the real world effects neglected in the analysis ysis so thatso that

    (32)(32)

    For a triangular weirFor a triangular weir

    2/5Hg22

    tan158Q =

    2tan)hH(2=l

    Hg2

    V21

  • 116

    Triangular Weir Triangular Weir FlowrateFlowrate 2/22/2

    Weir coefficient for Weir coefficient for triangular sharptriangular sharp--crested crested weirsweirs

  • 117

    About About NappeNappe

    Flow conditions over a weir without a free Flow conditions over a weir without a free nappenappe: (: (aa) plunging ) plunging nappenappe, , ((bb) submerged ) submerged nappenappe..

    FlowrateFlowrate over a weir depends on whether the over a weir depends on whether the napplenapple is free or is free or submerged.submerged.

    FlowrateFlowrate will be different for these situations will be different for these situations than that give by than that give by EqEq. (30) and (32).. (30) and (32).

  • 118

    BroadBroad--Crested Weir Crested Weir 1/31/3

    A broadA broad--crested weir is a structure in an open channel that has a crested weir is a structure in an open channel that has a horizontal crest above which the fluid pressure may be considerehorizontal crest above which the fluid pressure may be considered d hydrostatic.hydrostatic.

  • 119

    BroadBroad--Crested Weir Crested Weir 2/32/3

    Generally, these weirs are restricted to the range 0.08 < H/Generally, these weirs are restricted to the range 0.08 < H/LLww < 0.50.< 0.50. For long weir block (H/For long weir block (H/LLww < 0.08), head losses across the weir < 0.08), head losses across the weir

    cannot be neglected.cannot be neglected. For short weir block (H/For short weir block (H/LLww > 0.50), the streamlines of the flow over > 0.50), the streamlines of the flow over

    the weir are not horizontal.the weir are not horizontal.Apply the Bernoulli equationApply the Bernoulli equation

    g2VPy

    g2VPH

    2c

    wc

    21

    w ++=++

    g2V

    g2VVyH

    2c

    21

    2c

    c ==

    If the upstream velocity head is negligibleIf the upstream velocity head is negligible

  • 120

    BroadBroad--Crested Weir Crested Weir 3/33/3

    H32y

    2yyH ccc ==

    cc2 gyVV ==SinceSince

    2/32/3

    2/3ccc22 H3

    2gbygbVbyVbyQ

    ====The The flowrateflowrate isis

    Again an empirical Again an empirical broadbroad--crested weir coefficient, crested weir coefficient, CCwbwb, is used to , is used to account for the real world effects neglected in the analysis so account for the real world effects neglected in the analysis so thatthat

    2/32/3

    wb H32gbCQ

    = 2/1w

    wb

    PH1

    65.0C

    +

    =(33)(33) (34)(34)

  • 121

    Example 10.10 SharpExample 10.10 Sharp--Crested and broadCrested and broad--Crested WeirsCrested Weirszz Water flows in a rectangular channel of width b = 2 m with Water flows in a rectangular channel of width b = 2 m with flowrateflowrate

    between between QQminmin = 0.02 m= 0.02 m33/s and /s and QQmaxmax = 0.60 m= 0.60 m33/s. This /s. This flowrateflowrate is to is to be measured by using (a) a rectangular sharpbe measured by using (a) a rectangular sharp--crested weir, (b) a crested weir, (b) a triangular sharptriangular sharp--crested weir with crested weir with =90=90, or (c) a broad, or (c) a broad--crested crested weir. In all cases the bottom of the flow area over the weir is weir. In all cases the bottom of the flow area over the weir is a a distance Pdistance Pww = 1 m above the channel bottom. Plot a graph of Q= = 1 m above the channel bottom. Plot a graph of Q= Q(H) for each weir and comment on which weir would be best for Q(H) for each weir and comment on which weir would be best for this application.this application.

  • 122

    Example 10.10 Example 10.10 SolutionSolution1/31/3

    For the rectangular weir with For the rectangular weir with PPww=1.=1.

    2/3

    2/332

    w

    2/332

    wr

    H)H075.0611.0(91.5Q

    bHg2PH075.0611.0bHg2CQ

    +=

    +==(30)+(31)(30)+(31)

    For the triangular weirFor the triangular weir

    (32)(32) 2/5wt2/5

    wt HC36.2Hg22tan

    158CQ ==

  • 123

    Example 10.10 Example 10.10 SolutionSolution2/32/3

    For the broadFor the broad--crested weircrested weir

    (33)+(34)(33)+(34) 2/32/3

    2/1

    w

    2/32/3

    wb H32gb

    PH1

    65.0H32gbCQ

    +

    =

    =

    2/32/1 H)H1(

    22.2Q +=

  • 124

    Example 10.10 Example 10.10 SolutionSolution3/33/3

  • 125

    Underflow Gates Underflow Gates 1/41/4

    A variety of underflow gate structure is available for A variety of underflow gate structure is available for flowrateflowratecontrol at the crest of an overflow spillway, or at the entrancecontrol at the crest of an overflow spillway, or at the entrance of an of an irrigation canal or river from a lake.irrigation canal or river from a lake.

    Three variations of underflow gates: (Three variations of underflow gates: (aa) vertical gate, () vertical gate, (bb) radial gate, () radial gate, (cc) drum gate.) drum gate.

  • 126

    Underflow Gates Underflow Gates 2/42/4

    The flow under the gate is said to be free outflow when the fluiThe flow under the gate is said to be free outflow when the fluid d issues as a jet of supercritical flow with a free surface open tissues as a jet of supercritical flow with a free surface open to the o the atmosphere.atmosphere.

    In such cases it is customary to write this In such cases it is customary to write this flowrateflowrate asas

    1d gy2aCq = (35)(35)Where q is the Where q is the flowrateflowrate per unit width.per unit width.

    The discharge coefficient, The discharge coefficient, CCdd, is a function of contraction coefficient, , is a function of contraction coefficient, CCcc = y= y22/a, and the depth ration y/a, and the depth ration y11/a./a.

  • 127

    Underflow Gates Underflow Gates 3/43/4

    Typical discharge coefficients for underflow gatesTypical discharge coefficients for underflow gates

  • 128

    Underflow Gates Underflow Gates 4/44/4

    Drowned outflow from a sluice gate.Drowned outflow from a sluice gate.

    The depth downstream of the gate is controlled by some downstreaThe depth downstream of the gate is controlled by some downstream m obstacle and the jet of water issuing from under the gate is oveobstacle and the jet of water issuing from under the gate is overlaid rlaid by a mass of water that is quite turbulent.by a mass of water that is quite turbulent.

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    Example 10.11 Sluice gateExample 10.11 Sluice gate

    zz Water flows under the sluice gate shown in Fig. E10.11. The Water flows under the sluice gate shown in Fig. E10.11. The channel width is b = 20 ft, the upstream depth is ychannel width is b = 20 ft, the upstream depth is y11= 6 ft, and the = 6 ft, and the gate is a = 1.0 ft off the channel bottom. Plot a graph of gate is a = 1.0 ft off the channel bottom. Plot a graph of flowrateflowrate, Q, , Q, as a function of yas a function of y33..

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    Example 10.11 Example 10.11 SolutionSolution1/21/2

    (35)(35) cfsC393gy2baCbqq d1d ===

    (Figure 10.29)(Figure 10.29)

    cfs220cfs)56.0(393Q ==

    Along the vertical line yAlong the vertical line y11/a=6./a=6.For yFor y33=6 ft, =6 ft, CCdd=0=0

    The value of The value of CCdd increases as yincreases as y33/a decreases, reading a maximum of/a decreases, reading a maximum ofCCdd=0.56 when y=0.56 when y33/a=3.2. Thus with y/a=3.2. Thus with y33=3.2a=3.2ft=3.2a=3.2ft

    For yFor y33 < 3.2 ft the < 3.2 ft the flowrateflowrate is independent of yis independent of y33, and the outflow , and the outflow is a free outflow.is a free outflow.

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    Example 10.11 Example 10.11 SolutionSolution2/22/2

    The The flowrateflowrate forfor3.2ft 3.2ft yy3 3 6ft6ft