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FUNDAMENTALS OFFUNDAMENTALS OFFLUID MECHANICSFLUID MECHANICS
Chapter 3 Fluids in Motion Chapter 3 Fluids in Motion  The Bernoulli EquationThe Bernoulli Equation
JyhJyhCherngCherng ShiehShiehDepartment of BioDepartment of BioIndustrial Industrial MechatronicsMechatronics Engineering Engineering
National Taiwan UniversityNational Taiwan University09/28/200909/28/2009

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MAIN TOPICSMAIN TOPICS
NewtonNewtons Second Laws Second LawF=ma Along a StreamlineF=ma Along a StreamlineF=ma Normal to a StreamlineF=ma Normal to a StreamlinePhysical Interpretation Physical Interpretation of of Bernoulli EquationStatic, Stagnation, Dynamic, and Total PressureStatic, Stagnation, Dynamic, and Total PressureApplication of the Bernoulli EquationApplication of the Bernoulli EquationThe Energy Line and the Hydraulic Grade LineThe Energy Line and the Hydraulic Grade LineRestrictions on Use of the Bernoulli EquationRestrictions on Use of the Bernoulli Equation
Bernoulli Equation
Bernoulli equationBernoulli equation

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NewtonNewtons Second Law s Second Law 1/61/6
As a fluid particle moves from one location to another, it As a fluid particle moves from one location to another, it experiences an acceleration or deceleration.experiences an acceleration or deceleration.
According to According to NewtonNewtons second law of motions second law of motion, the net force acting , the net force acting on the fluid particle under consideration must equal its mass tion the fluid particle under consideration must equal its mass times mes its acceleration.its acceleration.
F=maF=ma In this chapter, we consider the motion of In this chapter, we consider the motion of inviscidinviscid fluidsfluids. That is, . That is,
the fluid is assumed to have the fluid is assumed to have zero viscosityzero viscosity. For such case, . For such case, it is it is possible to ignore viscous effects.possible to ignore viscous effects.
The forces acting on the particle ? Coordinates used ?The forces acting on the particle ? Coordinates used ?

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NewtonNewtons Second Law s Second Law 2/62/6
The fluid motion is governed byThe fluid motion is governed byF= Net pressure force + Net gravity forceF= Net pressure force + Net gravity force
To apply NewtonTo apply Newtons second law to a fluid, s second law to a fluid, an appropriate an appropriate coordinate system must be chosen to describe the coordinate system must be chosen to describe the motionmotion. In general, the motion will be three. In general, the motion will be threedimensional dimensional and unsteady so that and unsteady so that three space coordinates and timethree space coordinates and timeare needed to describe it.are needed to describe it.
ForceForce

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NewtonNewtons Second Law s Second Law 3/63/6
The most often used coordinate The most often used coordinate systems are systems are rectangular (x,y,z) rectangular (x,y,z) and cylindrical (r,and cylindrical (r,,z) system.,z) system.

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Streamline?Streamline? Streamline coordinate!Streamline coordinate!
As is done in the study of dynamics, the motion of each As is done in the study of dynamics, the motion of each fluid particle is described in terms of its velocity, V, which fluid particle is described in terms of its velocity, V, which is defined as the time rate of change of the position of the is defined as the time rate of change of the position of the particle.particle.
The particleThe particles velocity is a vector quantity with a s velocity is a vector quantity with a magnitude and direction.magnitude and direction.
As the particle moves about, it follows a particular path, As the particle moves about, it follows a particular path, the shape of which is governed by the velocity of the the shape of which is governed by the velocity of the particle.particle.

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Streamline?Streamline? Streamline coordinate!Streamline coordinate!
The location of the particle along the path is a function of The location of the particle along the path is a function of where the particle started at the initial time and its velocity where the particle started at the initial time and its velocity along the path.along the path.
If it is If it is steady flowsteady flow, each successive particle that passes , each successive particle that passes through a given point will follow the same path.through a given point will follow the same path.

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Streamline?Streamline? Streamline coordinate!Streamline coordinate!
For such cases the path is a fixed line in the For such cases the path is a fixed line in the xxzz plane.plane.Neighboring particles that pass on either side of point (1 Neighboring particles that pass on either side of point (1
following their own paths, which may be of a different following their own paths, which may be of a different shape than the one passing through (1).shape than the one passing through (1).
The entire The entire xxzz plane is filled with such paths.plane is filled with such paths.

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Streamline?Streamline? Streamline coordinate!Streamline coordinate!
For steady flows each particle slides along its path, and its For steady flows each particle slides along its path, and its velocity is everywhere tangent to the path.velocity is everywhere tangent to the path.
The lines that are tangent to the velocity vectors The lines that are tangent to the velocity vectors throughout the flow field are called throughout the flow field are called streamlines.streamlines.

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Streamline?Streamline? Streamline coordinate!Streamline coordinate!
For many situations it is easiest to describe the flow in For many situations it is easiest to describe the flow in terms of the terms of the streamlinestreamline coordinate based on the coordinate based on the streamlines. The particle motion is described in terms of streamlines. The particle motion is described in terms of its distance, its distance, s = s = s(ts(t),), along the streamline from some along the streamline from some convenient origin and the local radius of curvature of the convenient origin and the local radius of curvature of the streamline, streamline, R = R = R(sR(s).).

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NewtonNewtons Second Law s Second Law 4/64/6
In this chapter, the flow is confined to be In this chapter, the flow is confined to be twotwodimensional motion.dimensional motion.
As is done in the study of dynamics, the motion of each As is done in the study of dynamics, the motion of each fluid particle is described in terms of its velocity vector fluid particle is described in terms of its velocity vector VV..
As the particle moves, As the particle moves, it follows a particular path.it follows a particular path.The location of the particle along the path The location of the particle along the path is a function is a function of its initial position and velocity.of its initial position and velocity.
LocationLocation

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NewtonNewtons Second Law s Second Law 5/65/6
For steady flowsFor steady flows, each particle slides along its path, and , each particle slides along its path, and its velocity vector is everywhere tangent to the path. The its velocity vector is everywhere tangent to the path. The lines that are tangent to the velocity vectors throughout the lines that are tangent to the velocity vectors throughout the flow field are called flow field are called streamlinesstreamlines..
For such situation, the particle motion is described in For such situation, the particle motion is described in terms of its distance, s=s(t), along the streamline from terms of its distance, s=s(t), along the streamline from some convenient origin and the local radius of curvature some convenient origin and the local radius of curvature of the streamline, R=R(s).of the streamline, R=R(s).
streamlinestreamline
StreamlineStreamlines=s=s(ts(t))streamlinestreamlineR=R=R(sR(s) )

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NewtonNewtons Second Law s Second Law 6/66/6
The The distance along the streamline is related to the distance along the streamline is related to the particleparticles speeds speed by by VV==ds/dtds/dt, and the radius of curvature is , and the radius of curvature is related to shape of the streamline.related to shape of the streamline.
The acceleration is the time rate of change of the velocity The acceleration is the time rate of change of the velocity of the particleof the particle
The The components of accelerationcomponents of acceleration in the in the s and ns and n directiondirection
nRVs
dsdVVnasa
dtVda
2
ns
RVa
dsdVVa
2
ns CHAPTER 04 CHAPTER 04
s=s=s(ts(t)) VV==ds/dtds/dt
VV==ds/dtds/dt

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StreamlinesStreamlines
Streamlines past an airfoilStreamlines past an airfoil
Flow past a bikerFlow past a biker

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F=ma along a Streamline F=ma along a Streamline 1/41/4
Isolation of a small fluid particle in a flow field.fluid particle in a flow field.

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F=ma along a Streamline F=ma along a Streamline 2/42/4
Consider the small fluid particle of fluid particle of size of size of s by s by nn in the plane of the figure and y normal to the figure.
For steady flow, the component of Newtons second law along the streamline direction s
sVVV
sVmVmaF SS
Where represents the sum of the s components of all the force acting on the particle.
SF
ss

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F=ma along a Streamline F=ma along a Streamline 3/43/4
The The gravity force (weight)gravity force (weight) on the particle in the on the particle in the streamline directionstreamline direction
The The net pressure forcenet pressure force on the particle in the streamline on the particle in the streamline directiondirection
sinVsinWWs
Vspynp2ynppynppF SSSps
VspsinFWF psss
sasVV
spsin
Equation of motion Equation of motion along the streamline along the streamline directiondirection
2s
sppS

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F=ma along a Streamline F=ma along a Streamline 4/44/4
A change in fluid particle speed is accomplished by the A change in fluid particle speed is accomplished by the appropriate combination of pressure gradient and particle appropriate combination of pressure gradient and particle weight along the streamline.weight along the streamline.
For fluid For fluid static situationstatic situation, the balance between pressure , the balance between pressure and gravity force is such that and gravity force is such that no change in particle speedno change in particle speedis produced.is produced.
sasVV
spsin
0spsin
IntegrationIntegrationParticle weightParticle weight
pressure gradientpressure gradient
particle weightparticle weightpressure gradientpressure gradient

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IntegrationIntegration....
sasVV
spsin
Rearranged and IntegratedRearranged and Integrated
CgzV21dp
0dzVd21dp
dsdV
21
dsdp
dsdz
2
22
along a streamlinealong a streamlineWhere Where C is a constant of integration C is a constant of integration to be to be determined by the conditions at some point on determined by the conditions at some point on the streamline.the streamline.
In general it is not possible to integrate the pressure term In general it is not possible to integrate the pressure term because the density may not be constant and, therefore, because the density may not be constant and, therefore, cannot be removed from under the integral sign.cannot be removed from under the integral sign.

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Bernoulli Equation Along a StreamlineBernoulli Equation Along a Streamline
For the special case of For the special case of incompressible flowincompressible flow
Restrictions : Steady flow.Restrictions : Steady flow.Incompressible flow.Incompressible flow.Frictionless flow.Frictionless flow.Flow along a streamline.Flow along a streamline.
ttanconsz2
Vp2
BERNOULLI EQUATIONBERNOULLI EQUATION
CgzV21dp 2
The Bernoulli equation is a very The Bernoulli equation is a very powerful tool in fluid mechanics, powerful tool in fluid mechanics, published by Daniel Bernoulli published by Daniel Bernoulli (1700~1782) in 1738.(1700~1782) in 1738.NONO

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Example 3.1 Pressure Variation along A Example 3.1 Pressure Variation along A StreamlineStreamline Consider the Consider the inviscidinviscid, incompressible, steady flow, incompressible, steady flow along the along the
horizontal streamline Ahorizontal streamline AB in front of the sphere of radius a, as B in front of the sphere of radius a, as shown in Figure E3.1a. From a more advanced theory of flow past shown in Figure E3.1a. From a more advanced theory of flow past a a sphere, the fluid velocity along this streamline issphere, the fluid velocity along this streamline is
Determine the pressure variation along the streamline from pDetermine the pressure variation along the streamline from point A oint A far in front of the sphere (far in front of the sphere (xxAA== and Vand VAA= V= V00) to point B on the ) to point B on the sphere (sphere (xxBB==aa and Vand VBB=0)=0)
3
3
0 xa1VV streamlinestreamline
streamlinestreamline
sinsin=0=0 s s xx

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Example 3.1 Example 3.1 SolutionSolution1/21/2
4
3
3
32
04
30
3
3
0 xa
xa1V3
xaV3
xa1V
xVV
sVV
The equation of motion along the streamline (The equation of motion along the streamline (sinsin=0)=0)
The acceleration term
sVV
sp
(1)(1) sasVV
spsin
The pressure gradient along the streamline is
4
3320
3
xx/a1Va3
xp
sp
(2)(2)

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Example 3.1 Example 3.1 SolutionSolution2/22/2
The pressure gradient along the streamline
4
3320
3
xx/a1Va3
xp
sp
(2)(2)
The pressure distribution along the streamline
2)x/a(
xaVp
632
0

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Example 3.2 The Bernoulli EquationExample 3.2 The Bernoulli Equation
Consider the flow of air around a bicyclist moving through stillConsider the flow of air around a bicyclist moving through still air air with with velocity Vvelocity V00, as is shown in Figure E3.2. Determine the , as is shown in Figure E3.2. Determine the difference in the pressure between points (1) and (2).difference in the pressure between points (1) and (2).
point (1)point (1)point (2)point (2)

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Example 3.2 Example 3.2 SolutionSolution
2V
2Vpp
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21
12
The Bernoullis equation applied along the streamline that passes along the streamline that passes through (1) and (2)through (1) and (2)
z1=z2
2
22
21
21
1 z2Vpz
2Vp
(1) is in the free stream VV11=V=V00(2) is at the tip of the bicyclists nose V2=0
Bernoulli equationBernoulli equationpoint (1)point (1)point (2)point (2)streamlinestreamline

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F=ma Normal to a StreamlineF=ma Normal to a Streamline1/21/2
For steady flow, the For steady flow, the component of Newtoncomponent of Newtons s second law in the second law in the normal normal direction ndirection n
RVV
RmVF
22
n
Where represents the Where represents the sum of the n components of all sum of the n components of all the force acting on the particle.the force acting on the particle.
nF
HydrocycloneHydrocyclone separatorseparator

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F=ma Normal to a StreamlineF=ma Normal to a Streamline2/22/2
The The gravity force (weight)gravity force (weight) on the particle in the on the particle in the normal normal directiondirection
The The net pressure forcenet pressure force on the particle in the on the particle in the normal normal directiondirection
cosVcosWWn
Vnpysp2ys)pp(ysppF nnnpn
VRVV
npcosFWF
2
pnnn
RV
npcos
2
Equation of motion Equation of motion normal to the streamlinenormal to the streamlineNormal directionNormal direction
2n
nppn

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IntegrationIntegration....
RV
dndp
dndz 2
RV
npcos
2
RearrangedRearranged
Normal to Normal to the streamlinethe streamline
In general it is not possible to In general it is not possible to integrate the pressure term because integrate the pressure term because the density may not be constant and, the density may not be constant and, therefore, cannot be removed from therefore, cannot be removed from under the integral sign.under the integral sign.
IntegratedIntegrated
A change in the direction of flow of a fluid particle is A change in the direction of flow of a fluid particle is accomplished by the appropriate combination of pressure accomplished by the appropriate combination of pressure gradient and particle weight normal to the streamlinegradient and particle weight normal to the streamline
CgzdnRVdp 2
Without knowing the n dependent Without knowing the n dependent in V=in V=V(s,nV(s,n) and R=) and R=R(s,nR(s,n) this ) this integration cannot be completed.integration cannot be completed.
ParticleParticle weightweight
pressure gradientpressure gradient
V=V=V(s,nV(s,n) ) R=R=R(s,nR(s,n))

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Bernoulli Equation Normal to a StreamlineBernoulli Equation Normal to a Streamline
For the special case of For the special case of incompressible flowincompressible flow
Restrictions : Steady flow.Restrictions : Steady flow.Incompressible flow.Incompressible flow.Frictionless flow. Frictionless flow. NO shear forceNO shear forceFlow normal to a streamline.Flow normal to a streamline.
CzdnRVp
2
BERNOULLI EQUATIONBERNOULLI EQUATION
CgzdnRVdp 2

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If gravity is neglectedFree vortex
A larger speed or density or smaller radius of curvature of A larger speed or density or smaller radius of curvature of the motion required a larger force unbalance to produce the the motion required a larger force unbalance to produce the motion.motion.
If gravity is neglected or if the flow is in a horizontalIf gravity is neglected or if the flow is in a horizontal
RV
dndp
dndz 2
RV
dndp 2
Pressure increases with distance away from the center Pressure increases with distance away from the center of curvature. Thus, the pressure outside a tornado is of curvature. Thus, the pressure outside a tornado is larger than it is near the center of the tornado.larger than it is near the center of the tornado.

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Aircraft wing tip vortexAircraft wing tip vortex

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Example 3.3 Pressure Variation Normal to Example 3.3 Pressure Variation Normal to a Streamlinea Streamline Shown in Figure E3.3a and E3.3b are two flow fields with circulaShown in Figure E3.3a and E3.3b are two flow fields with circular r
streamlines. The streamlines. The velocity distributionsvelocity distributions are are
)b(r
C)r(V)a(rC)r(V 21
Assuming the flows are steady, inviscid, and incompressible with streamlines in the horizontal plane (dz/dn=0).
RV
npcos
2

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Example 3.3 Example 3.3 SolutionSolution
020221 prrC21p
rV
rp 2
For flow in the horizontal plane (dz/dn=0). The streamlines are circles /n=/rThe radius of curvature R=r
For case (a) this gives
rCrp 2
1
3
22
rC
rp
For case (b) this gives
0220
22 pr
1r1C
21p
RV
dndp
dndz 2

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Physical InterpreterPhysical Interpreter1/21/2
Under the basic assumptions: Under the basic assumptions: the flow is steady and the fluid is the flow is steady and the fluid is inviscidinviscid and incompressible.and incompressible.
Application of F=ma and integration of equation of motion along Application of F=ma and integration of equation of motion along and normal to the streamline result inand normal to the streamline result in
To To produce an acceleration, there must be an unbalance of produce an acceleration, there must be an unbalance of the resultant forcethe resultant force, , of which only pressure and gravity were of which only pressure and gravity were considered to be importantconsidered to be important. Thus, there are three process . Thus, there are three process involved in the flow involved in the flow mass times acceleration (the mass times acceleration (the VV22/2 term), /2 term), pressure (the p term), and weight (the pressure (the p term), and weight (the z term).z term).
CzdnRVp
2
Cz2Vp
2
ppz z
RVa
dsdVVa
2
ns

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Physical InterpreterPhysical Interpreter2/22/2
The Bernoulli equation is a mathematical statement of The Bernoulli equation is a mathematical statement of The The work done on a particle of all force acting on the particle is ework done on a particle of all force acting on the particle is equal qual to the change of the kinetic energy of the particleto the change of the kinetic energy of the particle..Work done by force : Work done by force : FFdd..Work done by weight: Work done by weight: z z Work done by pressure force: pWork done by pressure force: p
Kinetic energy: Kinetic energy: VV22/2/2
CdnRVzp
2
C2Vzp
2
Based onBased on

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HeadHead
An alternative but equivalent form of the Bernoulli An alternative but equivalent form of the Bernoulli equation is obtained by dividing each term by equation is obtained by dividing each term by
czg2
VP 2
Pressure HeadPressure Head
Velocity HeadVelocity Head
Elevation HeadElevation Head
The Bernoulli Equation can be written in The Bernoulli Equation can be written in terms of heights called headsterms of heights called heads
streamlinestreamline

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Example 3.4 Kinetic, Potential, and Example 3.4 Kinetic, Potential, and Pressure EnergyPressure Energy Consider the flow of water from the syringe Consider the flow of water from the syringe
shown in Figure E3.4. A force applied to the shown in Figure E3.4. A force applied to the plunger will produce a pressure greater than plunger will produce a pressure greater than atmospheric at point (1) within the syringe. atmospheric at point (1) within the syringe. The water flows from the needle, point (2), The water flows from the needle, point (2), with relatively high velocity and coasts up to with relatively high velocity and coasts up to point (3) at the top of its trajectory. Discuss point (3) at the top of its trajectory. Discuss the energy of the fluid at point (1), (2), and (3) the energy of the fluid at point (1), (2), and (3) by using the Bernoulli equation. by using the Bernoulli equation.
point (1) (2) (3)point (1) (2) (3)

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Example 3.4 Solution
The sum of the three types of energy (kinetic, potential, and prThe sum of the three types of energy (kinetic, potential, and pressure) essure) or heads (velocity, elevation, and pressure) must remain constanor heads (velocity, elevation, and pressure) must remain constant. t.
The pressure gradient between (1) and (2) The pressure gradient between (1) and (2) produces an acceleration to eject the water produces an acceleration to eject the water form the needle. Gravity acting on the form the needle. Gravity acting on the particle between (2) and (3) produces a particle between (2) and (3) produces a deceleration to cause the water to come to deceleration to cause the water to come to a momentary stop at the top of its flight.a momentary stop at the top of its flight.
streamlinethealongttanconszV21p 2
The motion results in a change in the magnitude of each type of energy as the fluid flows from one location to another.

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Example 3.5 Pressure Variation in a Example 3.5 Pressure Variation in a Flowing StreamFlowing Stream Consider the Consider the inviscidinviscid, incompressible, steady flow shown in Figure , incompressible, steady flow shown in Figure
E3.5. From section A to B the streamlines are straight, while frE3.5. From section A to B the streamlines are straight, while from C om C to D they follow circular paths. to D they follow circular paths. Describe the pressure variation Describe the pressure variation between points (1) and (2)and points(3) and (4)between points (1) and (2)and points(3) and (4)
point (1)(2)point (1)(2) point(3)(4)point(3)(4)

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Example 3.5 Example 3.5 SolutionSolution1/21/2
1221221 rhp)zz(rpp
ttanconsrzp
R= , , for the portion from for the portion from A to BA to B
Using p2=0,z1=0,and z2=h21
Since the radius of curvature of the streamline is infinite, the pressure variation in the vertical direction is the same as if the fluids were stationary.
Point (1)~(2)

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4
3
z
z
2
343 dzRVrhp
With pp44=0 and z=0 and z44zz33=h=h4433 ,this becomes
334z
z
2
4 rzprz)dz(RVp
4
3
Example 3.5 Example 3.5 SolutionSolution2/22/2
Point (3)~(4)
For the portion from For the portion from C to DC to D

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Static, Stagnation, Dynamic, and Static, Stagnation, Dynamic, and Total PressureTotal Pressure1/51/5Each term in the Bernoulli equation can be interpreted as a Each term in the Bernoulli equation can be interpreted as a
form of pressure.form of pressure.
pp is the actual thermodynamic pressure of the fluid as it is the actual thermodynamic pressure of the fluid as it flows. To measure this pressure, one must move along flows. To measure this pressure, one must move along with the fluid, thus being with the fluid, thus being staticstatic relative to the moving relative to the moving fluid. Hence, it is termed the fluid. Hence, it is termed the static pressurestatic pressure seen by the seen by the fluid particle as it movesfluid particle as it moves. .
C2
Vzp2
Each term can be interpreted as a form of pressure
ppstaticstaticstatic pressurestatic pressure

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Static, Stagnation, Dynamic, and Static, Stagnation, Dynamic, and Total PressureTotal Pressure2/52/5The static pressureThe static pressure is measured in a flowing fluid using a is measured in a flowing fluid using a
wall pressure wall pressure taptap, or a static pressure probe., or a static pressure probe.hhhphp 34133131 The static pressureThe static pressure
zz is termed the is termed the hydrostatic hydrostatic pressurepressure. It is not actually a . It is not actually a pressure but does represent the pressure but does represent the change in pressure possible due change in pressure possible due to potential energy variations of to potential energy variations of the fluid as a result of elevation the fluid as a result of elevation changes.changes.
wall wall pressurepressuretaptapstatic static pressurepressure
zz

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Static, Stagnation, Dynamic, and Static, Stagnation, Dynamic, and Total PressureTotal Pressure3/53/5VV22/2/2 is termed the is termed the dynamic pressuredynamic pressure. It can be interpreted . It can be interpreted
as the pressure at the end of a small tube inserted into the as the pressure at the end of a small tube inserted into the flow and pointing upstream. flow and pointing upstream. After the initial transient After the initial transient motion has died out, the liquid will fill the tube to a height motion has died out, the liquid will fill the tube to a height of H.of H.
The fluid in the tube, including that at its tip (2), will be The fluid in the tube, including that at its tip (2), will be stationary. That is, Vstationary. That is, V22=0, or point (2) is a stagnation point.=0, or point (2) is a stagnation point.
2112 V2
1pp Stagnation pressure
Static pressure Dynamic pressureDynamic pressure
VV22/2/222HH
1122
sstagnationtagnation pressurepressure

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Stagnation pointStagnation point
Stagnation point flowStagnation point flow

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Static, Stagnation, Dynamic, and Static, Stagnation, Dynamic, and Total PressureTotal Pressure4/54/5There is a stagnation point on any stationary body that is There is a stagnation point on any stationary body that is
placed into a flowing fluid. Some of the fluid flows placed into a flowing fluid. Some of the fluid flows overoverand some and some underunder the object.the object.
The dividing line is termed the The dividing line is termed the stagnation streamlinestagnation streamline and and terminates at the stagnation point on the body.terminates at the stagnation point on the body.
Neglecting the elevation Neglecting the elevation effects, effects, the stagnation the stagnation pressure is the largest pressure is the largest pressure obtainable along a pressure obtainable along a given streamlinegiven streamline..
stagnation pointstagnation point
stagnation pointstagnation point
stagnation pointstagnation point

47
Static, Stagnation, Dynamic, and Static, Stagnation, Dynamic, and Total PressureTotal Pressure5/55/5The The sum of the static pressure, dynamic pressure, and sum of the static pressure, dynamic pressure, and
hydrostatic pressure is termed the total pressurehydrostatic pressure is termed the total pressure..The Bernoulli equation is a statement that the total The Bernoulli equation is a statement that the total
pressure remains constant along a streamline.pressure remains constant along a streamline.
ttanconspz2
Vp T2
Total pressureTotal pressurestreamlinestreamline
TTootaltal pressurepressure

48
The The PitotPitotstatic Tube static Tube 1/51/5
/)pp(2V
2/Vpp
pppzz
2/Vppp
43
243
14
41
232
Knowledge of the values of the static and Knowledge of the values of the static and stagnation pressure in a fluid implies that the stagnation pressure in a fluid implies that the fluid speed can be calculated.fluid speed can be calculated.
This is This is the principle on which the the principle on which the PitotPitotstatic tube is based.static tube is based.
Static pressureStatic pressure
Stagnation pressureStagnation pressure
PitotPitotstatic static stubesstubes measure measure fluid velocity by converting fluid velocity by converting velocity into pressure.velocity into pressure.
streamlinestreamlinetotal pressuretotal pressure
staticstaticstagnation stagnation pressurepressure

49
Airplane Airplane PitotPitotstatic probestatic probe
Airspeed indicatorAirspeed indicator

50
The The PitotPitotstatic Tube static Tube 2/52/5

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The The PitotPitotstatic Tube static Tube 3/53/5
The use of The use of pitotpitotstatic tube depends on the ability to static tube depends on the ability to measure the static and stagnation pressure.measure the static and stagnation pressure.
An accurate measurement of static pressure requires that An accurate measurement of static pressure requires that none of the fluidnone of the fluids kinetic energy be converted into a s kinetic energy be converted into a pressure rise at the point of measurement.pressure rise at the point of measurement.
This requires a smooth hole with no burrs or imperfections.This requires a smooth hole with no burrs or imperfections.
Incorrect and correct design of static pressure taps.Incorrect and correct design of static pressure taps.
TapsTaps

52
The The PitotPitotstatic Tube static Tube 4/54/5
Typical pressure distribution along a Typical pressure distribution along a PitotPitotstatic tube.static tube.
The pressure along the surface of an object varies from the The pressure along the surface of an object varies from the stagnation pressure at its stagnation point to value that stagnation pressure at its stagnation point to value that may be less than free stream static pressure.may be less than free stream static pressure.
It is important that the pressure taps be properly located to It is important that the pressure taps be properly located to ensure that the pressure measured is actually the static ensure that the pressure measured is actually the static pressure.pressure.tapstapsstatic pressurestatic pressure

53
The The PitotPitotstatic Tube static Tube 5/55/5
Three pressure taps are drilled into a small circular Three pressure taps are drilled into a small circular cylinder, fitted with small tubes, and connected to three cylinder, fitted with small tubes, and connected to three pressure transducers. pressure transducers. The cylinder is rotated until the The cylinder is rotated until the pressures in the two side holes are equalpressures in the two side holes are equal, thus indicating , thus indicating that the center hole points directly upstream.that the center hole points directly upstream.
21
12
31
PP2V
PP
Directionalfinding Pitotstatic tube.
If =0PP11=P=P33
PitotPitotstatic tubestatic tube

54
Example 3.6 Example 3.6 PitotPitotStatic TubeStatic Tube
An airplane flies 100mi/hr at an elevation of 10,000 ft in a An airplane flies 100mi/hr at an elevation of 10,000 ft in a standard atmosphere as shown in Figure E3.6. Determine standard atmosphere as shown in Figure E3.6. Determine the pressure at point (1) far ahead of the airplane, point (2), the pressure at point (1) far ahead of the airplane, point (2), and the pressure difference indicated by a and the pressure difference indicated by a PitotPitotstatic static probe attached to the fuselage. probe attached to the fuselage.
PitotPitotstatic tubestatic tube

55
Example 3.6 Example 3.6 Solution Solution 1/21/2
2Vpp
21
12
psia11.10)abs(ft/lb1456p 21
The static pressure and density at the altitude
If the flow is steady, inviscid, and incompressible and elevation changes are neglected. The Bernoulli equation
3ft/slug001756.0
With V1=100mi/hr=146.6ft/s and V2=0
)abs(ft/lb)9.181456(
2/)s/ft7.146)(ft/slugs001756.0(ft/lb1456p2
222322
10,000ft10,000ft

56
psi1313.0ft/lb9.18p 22
In terms of gage pressure
psi1313.02Vpp
21
12
The pressure difference indicated by the Pitotstatic tube
Example 3.6 Example 3.6 Solution Solution 2/22/2

57
Application of Bernoulli Equation Application of Bernoulli Equation 1/21/2
The Bernoulli equation can be appliedThe Bernoulli equation can be applied between any two between any two points on a streamline providedpoints on a streamline provided that the other that the other three three restrictionsrestrictions are satisfied. The result isare satisfied. The result is
2
22
21
21
1 z2Vpz
2Vp
Restrictions : Steady flow.Restrictions : Steady flow.Incompressible flow.Incompressible flow.Frictionless flow.Frictionless flow.Flow along a streamline.Flow along a streamline.
Bernoulli equationBernoulli equation
streamlinestreamline
Bernoulli equationBernoulli equation

58
Application of Bernoulli Equation Application of Bernoulli Equation 2/22/2
Free jet.Free jet.Confined flow.Confined flow.FlowrateFlowrate measurementmeasurement
Bernoulli equationBernoulli equation

59
Free Jets Free Jets 1/31/3
Application of the Bernoulli equation between points (1) Application of the Bernoulli equation between points (1) and (2) on the streamlineand (2) on the streamline
gh2h2V
2Vh
2
At point (5)
)Hh(g2V
2
22
21
21
1 z2Vpz
2Vp
pp11=p=p22=0=0 zz11=h=hzz22=0=0VV11=0=0
pp11=p=p55=0=0 zz11==h+Hh+Hzz22=0=0VV11=0=0

60
Free JetsFree Jets
Flow from a tankFlow from a tank

61
Free Jets Free Jets 2/32/3
For the For the horizontal nozzlehorizontal nozzle, the , the velocity at the centerline, Vvelocity at the centerline, V22, , will be greater than that at the will be greater than that at the top Vtop V11..
In general, d

62
Free Jets Free Jets 3/33/3
Typical Typical flow patterns and flow patterns and contraction coefficientscontraction coefficients for for various round exit various round exit configuration.configuration.
The diameter of a fluid jet is The diameter of a fluid jet is often smaller than that of the often smaller than that of the hole from which it flows.hole from which it flows.
Define Cc = contraction coefficient Define Cc = contraction coefficient
h
jc A
AC
AjAj=area of the jet at the vena =area of the jet at the vena contractacontractaAh=area of the holeAh=area of the hole
2
22
21
21
1 z2Vpz
2Vp
flow patternflow pattern

63
Example 3.7 Flow From a TankExample 3.7 Flow From a Tank GravityGravity
A stream of water of diameter d = 0.1m flows steadily from a tanA stream of water of diameter d = 0.1m flows steadily from a tank k of Diameter D = 1.0m as shown in Figure E3.7a. of Diameter D = 1.0m as shown in Figure E3.7a. Determine the Determine the flowrateflowrate, Q,, Q, needed from the inflow pipe if needed from the inflow pipe if the water depth remains the water depth remains constantconstant, h = 2.0m., h = 2.0m.
flowrateflowrate QQ

64
Example 3.7 Example 3.7 SolutionSolution1/21/2
22
221
2
11 zV21pzV
21p
22
21 V2
1ghV21
The Bernoulli equation applied between points The Bernoulli equation applied between points (1) and (2)(1) and (2) isis
(1)(1)
With With pp11 = p= p22 = 0, z= 0, z11 = h, and z= h, and z22 = 0= 0
(2)(2)
For steady and incompressible flow, For steady and incompressible flow, conservation of mass requiresconservation of mass requiresQQ11 = Q= Q22, where Q = AV. Thus, A, where Q = AV. Thus, A11VV11 =A=A22VV2 2 , or , or
22
12 Vd
4VD
4
2
22
21
21
1 z2Vpz
2Vp
22
1 V)Dd(V (3)
Bernoulli equationBernoulli equationpoint(1)point(1)(2)(2)
Point(1)Point(1)(2)(2)

65
Example 3.7 Example 3.7 SolutionSolution2/22/2
s/m26.6)m1/m1.0(1
)m0.2)(s/m81.9(2)D/d(1
gh2V4
2
42
Combining Equation 2 and 3
Thus,
s/m0492.0)s/m26.6()m1.0(4
VAVAQ 322211
VV110 (Q) vs. V0 (Q) vs. V110 (Q0 (Q00))
4
4
2
2
0 )/(11
2])/(1/[2
DdghDdgh
VV
QQ
D

66
Example 3.8 Flow from a TankExample 3.8 Flow from a TankPressurePressure
Air flows steadily from a tank, through a hose of diameter Air flows steadily from a tank, through a hose of diameter D=0.03m and exits to the atmosphere from a nozzle of D=0.03m and exits to the atmosphere from a nozzle of diameter d=0.01m as shown in Figure E3.8. diameter d=0.01m as shown in Figure E3.8. The pressure The pressure in the tank remains constant at 3.0kPa (gage)in the tank remains constant at 3.0kPa (gage) and the and the atmospheric conditions are standard temperature and atmospheric conditions are standard temperature and pressure. pressure. Determine the Determine the flowrateflowrate and the pressure in and the pressure in the hose.the hose.
flowrateflowrate Point(2)Point(2)

67
Example 3.8 Example 3.8 SolutionSolution1/21/2
32332
2221
211 zV2
1pzV21pzV
21p
2212
13 V2
1ppandp2V
For steady, For steady, inviscidinviscid, and incompressible flow, the Bernoulli equation , and incompressible flow, the Bernoulli equation along the streamlinealong the streamline
With zWith z11 =z=z22 = z= z33 , V, V11 = 0, and p= 0, and p33=0=0
(1)(1)
The density of the air in the tank is obtained from the perfect The density of the air in the tank is obtained from the perfect gas law gas law
33
2
1
m/kg26.1K)27315)(Kkg/mN9.286(
kN/N10]m/kN)1010.3[(RTp
Bernoulli equationBernoulli equationpoint(1)(2)point(1)(2)(3)(3)
Point(1)Point(1)(2)(2)((33))

68
Example 3.8 Example 3.8 SolutionSolution2/22/2
s/m00542.0Vd4
VAQ 332
33
s/m0.69m/kg26.1
)m/N100.3(2p2V 323
13
Thus, Thus,
oror
The pressure within the hose can be obtained from The pressure within the hose can be obtained from EqEq. 1. 1and the continuity equationand the continuity equation
s/m67.7A/VAV,HenceVAVA 23323322
22
23232212
m/N2963m/N)1.373000(
)s/m67.7)(m/kg26.1(21m/N100.3V
21pp

69
Example 3.9 Flow in a Variable Area PipeExample 3.9 Flow in a Variable Area Pipe
Water flows through a pipe reducer as is shown in Figure E3.9. TWater flows through a pipe reducer as is shown in Figure E3.9. The he static pressures at (1) and (2) are measured by the inverted Ustatic pressures at (1) and (2) are measured by the inverted Utube tube manometer containing oil of specific gravity, SG, less than one.manometer containing oil of specific gravity, SG, less than one.Determine the manometer reading, h.Determine the manometer reading, h.
reading hreading h

70
Example 3.9 Example 3.9 SolutionSolution1/21/2
2211 VAVAQ
For steady, For steady, inviscidinviscid, incompressible flow, the Bernoulli equation along , incompressible flow, the Bernoulli equation along the streamlinethe streamline
The continuity equationThe continuity equation
Combining these two equations Combining these two equations
(1)(1)
22221
211 zpV2
1pzpV21p
])A/A(1[pV21)zz(pp 212
221221

71
Example 3.9 Example 3.9 SolutionSolution2/22/2
h)SG1()zz(pp 1221
2121 phSGh)zz(p
2
1
222 A
A1pV21h)SG1(
This pressure difference is measured by the manometer and determThis pressure difference is measured by the manometer and determine ine by using the pressureby using the pressuredepth ideas developed in depth ideas developed in Chapter 2Chapter 2..
oror(2)(2)
SG1g2)A/A(1A/Qh
2122
2
Since VSince V22=Q/A=Q/A22
 +
be independent of be independent of
Point(1)(2)Point(1)(2)

72
Confined Flows Confined Flows 1/41/4
When the fluid is physically constrained within a device, When the fluid is physically constrained within a device, its pressure cannot be prescribed a priori as was done for its pressure cannot be prescribed a priori as was done for the free jet.the free jet.
Such casesSuch cases include include nozzle and pipesnozzle and pipes of of various diametervarious diameterfor which the fluid velocity changes because the flow area for which the fluid velocity changes because the flow area is different from one section to another.is different from one section to another.
For such situations, it is necessary to use the concept of For such situations, it is necessary to use the concept of conservation of mass (the continuity equation) along with conservation of mass (the continuity equation) along with the Bernoulli equation.the Bernoulli equation.
Tools: Bernoulli equation + Continuity equation
devicedevicenozzlenozzlepipepipe

73
Confined Flows Confined Flows 2/42/4
Consider a fluid flowing through a fixed volume that has Consider a fluid flowing through a fixed volume that has one inlet and one outlet.one inlet and one outlet.
Conservation of mass requiresConservation of mass requiresFor For incompressible flowincompressible flow, the continuity equation is, the continuity equation is
222111 VAVA
212211 QQVAVA

74
Confined Flows Confined Flows 3/43/4
If the fluid velocity is increased, If the fluid velocity is increased, the pressure will decrease.the pressure will decrease.
This pressure decrease can be This pressure decrease can be large enough so that the large enough so that the pressure in the liquid is reduced pressure in the liquid is reduced to its to its vapor pressure.vapor pressure.
Pressure variation and cavitationin a variable area pipe.
vapor pressurevapor pressure
VenturiVenturi channelchannel

75
Confined Flows Confined Flows 4/4 example of 4/4 example of cavitationcavitation
A example of A example of cavitationcavitation can be demonstrated with a can be demonstrated with a garden hose.garden hose. If the hose is If the hose is kinked,kinked, a restriction in the a restriction in the flow area will result.flow area will result.
The water The water velocityvelocity through the restriction will be through the restriction will be relatively large.relatively large.
With a sufficient amount of restriction the sound of the With a sufficient amount of restriction the sound of the flowing water will change flowing water will change a definite a definite hissinghissing sound will sound will be produced.be produced.
The sound is a result of The sound is a result of cavitationcavitation..

76
Damage from Damage from CavitationCavitation
Cavitation from propeller
bubblebubble

77
Example 3.10 Siphon and Example 3.10 Siphon and CavitationCavitation
Water at 60Water at 60 is siphoned from a large tank through a constant is siphoned from a large tank through a constant diameter hose as shown in Figure E3.10. Determine the maximum diameter hose as shown in Figure E3.10. Determine the maximum height of the hill, H, over which the water can be siphoned withheight of the hill, H, over which the water can be siphoned without out cavitationcavitation occurring. The end of the siphon is 5 ft below the bottom occurring. The end of the siphon is 5 ft below the bottom of the tank. Atmospheric pressure is 14.7 of the tank. Atmospheric pressure is 14.7 psiapsia..
The value of H is a function of both the The value of H is a function of both the specific weight of the fluid, specific weight of the fluid, , and its , and its vapor pressure, vapor pressure, ppvv..
Max. HMax. Hcavitationcavitation

78
Example 3.10 Example 3.10 SolutionSolution1/21/2
32332
2221
211 zV2
1pzV21pzV
21p
For ready, For ready, inviscidinviscid, and incompressible flow, the Bernoulli equation , and incompressible flow, the Bernoulli equation along the streamline from along the streamline from (1) to (2) to (3)(1) to (2) to (3)
With With zz1 1 = 15 ft, z= 15 ft, z22 = H, and z= H, and z33 = = 5 ft. Also, V5 ft. Also, V11 = 0 (large tank), p= 0 (large tank), p11 = 0 = 0 (open tank), p(open tank), p33 = 0 (free jet), and from the continuity equation A= 0 (free jet), and from the continuity equation A22VV22 = = AA33VV33, or because the hose is constant diameter V, or because the hose is constant diameter V22 = V= V33.. The speed of The speed of the fluid in the hose is determined from the fluid in the hose is determined from EqEq. 1 to be. 1 to be
(1)(1)
22
313 Vs/ft9.35ft)]5(15)[s/ft2.32(2)zz(g2V (1)(3)(1)(3)
(1)(2)(1)(2)

79
Example 3.10 Example 3.10 SolutionSolution2/22/2
22212
221
2112 V2
1)zz(zV21zV
21pp
233222 )s/ft9.35)(ft/slugs94.1(21ft)H15)(ft/lb4.62()ft/.in144)(.in/lb4.14(
Use of Use of EqEq. 1 . 1 between point (1) and (2) then gives the pressure pbetween point (1) and (2) then gives the pressure p22 at the at the toptop of the hill asof the hill as
The The vapor pressure of water at 60vapor pressure of water at 60 is 0.256 is 0.256 psiapsia. . Hence, for incipient Hence, for incipient cavitationcavitation the lowest pressure in the system will be p = 0.256 the lowest pressure in the system will be p = 0.256 psiapsia..UUsing gage pressure: sing gage pressure: pp11 = 0, p= 0, p22=0.256 =0.256 14.7 = 14.7 = 14.4 14.4 psipsi
(2)(2)
ftH 2.28

80
FlowrateFlowrate Measurement Measurement inin pipes 1/5pipes 1/5
Various flow meters are Various flow meters are governed by the governed by the Bernoulli Bernoulli and continuity equationsand continuity equations..
2211
222
211
VAVAQ
V21pV
21p
])A/A(1[)pp(2AQ 212
212
The theoretical The theoretical flowrateflowrate
Typical devices for measuring Typical devices for measuring flowrateflowrate in pipesin pipes
Flow metersFlow meters

81
Example 3.11 Example 3.11 VenturiVenturi MeterMeter
Kerosene (SG = 0.85) flows through the Kerosene (SG = 0.85) flows through the VenturiVenturi meter shown in meter shown in Figure E3.11 with Figure E3.11 with flowratesflowrates between 0.005 and 0.050 mbetween 0.005 and 0.050 m33/s. /s. Determine the range in pressure difference, Determine the range in pressure difference, pp11 pp22, needed to , needed to measure these measure these flowratesflowrates..
Known Q, Determine pKnown Q, Determine p11pp22
point(1)(2)point(1)(2)

82
Example 3.11 Example 3.11 SolutionSolution1/21/2
33O2H kg/m850)kg/m1000(85.0SG
22
2
A2])A/A(1[Q
pp2
12
21
For steady, For steady, inviscidinviscid, and incompressible flow, the relationship between , and incompressible flow, the relationship between flowrateflowrate and pressure and pressure
The density of the flowing fluidThe density of the flowing fluid
The area ratioThe area ratio
36.0)m10.0/m006.0()D/D(/AA 221212
])A/A(1[)pp(2AQ 212
212
EqEq. 3.20. 3.20

83
Example 3.11 Example 3.11 SolutionSolution2/22/2
The pressure difference for the The pressure difference for the smallest smallest flowrateflowrate isis
The pressure difference for the The pressure difference for the largest largest flowrateflowrate isis
22
22
21 ])m06.0)(4/[(2)36.01()850)(05.0(pp
kPa116N/m1016.1 25
kPa16.1N/m1160])m06.0)(4/[(2
)36.01()kg/m850()/sm005.0(pp2
22
2323
21
kPa116ppkPa16.1 21

84
FlowrateFlowrate Measurement Measurement sluice gate 2/5sluice gate 2/5
The sluice gate is often used to regulate and measure the The sluice gate is often used to regulate and measure the flowrateflowrate in in an open channel.an open channel.
The The flowrateflowrate, Q, , Q, is function of the water depth upstream, zis function of the water depth upstream, z11, the , the width of the gate, b, and the gate opening, a.width of the gate, b, and the gate opening, a.
212
212 )z/z(1
)zz(g2bzQ
With pWith p11=p=p22=0, the =0, the flowrateflowrate
22221111
22221
211
zbVVAzbVVAQ
zV21pzV
21p

85
FlowrateFlowrate Measurement Measurement sluice gate 3/5sluice gate 3/5
In the limit of In the limit of zz11>>z>>z22, this result simply becomes , this result simply becomes
This limiting result represents the fact that if the depth This limiting result represents the fact that if the depth ratio, zratio, z11/z/z22, is large, , is large, the kinetic energy of the fluid the kinetic energy of the fluid upstream of the gate is negligibleupstream of the gate is negligible and the fluid velocity and the fluid velocity after it has fallen a distance (zafter it has fallen a distance (z11zz22)~z)~z11 is approximately is approximately
ZZ2 2 ?? ?? QQ
12 gz2bzQ
12 gz2V
zz11zz22
z2

86
FlowrateFlowrate Measurement Measurement sluice gate 4/5sluice gate 4/5
As we discussed relative to flow from an orifice, As we discussed relative to flow from an orifice, the fluid the fluid cannot turn a sharp 90cannot turn a sharp 90 corner. A vena corner. A vena contractacontracta results results with a contraction coefficient, with a contraction coefficient, CCcc=z=z22/a, less than 1/a, less than 1..
Typically CTypically Ccc~0.61 over the depth ratio range of 0

87
Example 3.12 Sluice Gate
Water flows under the sluice gate in Figure E3.12a. Water flows under the sluice gate in Figure E3.12a. DertermineDertermine the the approximate approximate flowrateflowrate per unit width of the channel.per unit width of the channel.

88
Example 3.12 Example 3.12 SolutionSolution1/21/2
s/m61.4)m0.5/m488.0(1
)m488.0m0.5)(s/m81.9(2)m488.0(bQ 2
2
2
212
212 )z/z(1
)zz(g2zbQ
For steady, inviscid, incompreesible flow, the flowerate per uniFor steady, inviscid, incompreesible flow, the flowerate per unit widtht width
With zWith z11=5.0m and a=0.80m, so the ratio a/z=5.0m and a=0.80m, so the ratio a/z11=0.16

89
Example 3.12 Example 3.12 SolutionSolution1/21/2
If we consider zIf we consider z11>>z>>z22 and neglect the kinetic energy of the upstream and neglect the kinetic energy of the upstream fluidfluid, we would have, we would have
s/m83.4m0.5s/m81.92m488.0gz2zbQ 22
12

90
FlowrateFlowrate Measurement Measurement weirweir 5/55/5
For a typical rectangular, sharpFor a typical rectangular, sharpcrested, the crested, the flowrateflowrate over the top of over the top of the weir plate is dependent on the weir plate is dependent on the weir height, Pthe weir height, Pww, the width of the , the width of the channel, b, and the head, H,channel, b, and the head, H, of the water above the top of the weir.of the water above the top of the weir.
2/3111 Hg2bCgH2HbCAVCQ The The flowrateflowrate
Where CWhere C11 is a constant to be determined.is a constant to be determined.

91
Example 3.13 WeirExample 3.13 Weir
Water flows over a triangular weir, as is shown in Figure E3.13.Water flows over a triangular weir, as is shown in Figure E3.13.Based on a simple analysis using the Bernoulli equation, determiBased on a simple analysis using the Bernoulli equation, determine ne the dependence of the dependence of flowrateflowrate on the depth H. on the depth H. If the If the flowrateflowrate is Qis Q00when H=Hwhen H=H00, estimate the , estimate the flowrateflowrate when the depth is increased to when the depth is increased to H=3HH=3H00.. HH33

92
Example 3.13 Example 3.13 SolutionSolution
gH2
For steady , For steady , inviscidinviscid , and incompressible flow, the average speed , and incompressible flow, the average speed of the fluid over the triangular notch in the weir plate is of the fluid over the triangular notch in the weir plate is proportional toproportional toThe flow area for a depth of H is H[H tan(The flow area for a depth of H is H[H tan( /2)]/2)]The The flowrateflowrate
where Cwhere C11 is an unknown constant to be determined experimentally.is an unknown constant to be determined experimentally.
2/51
211 Hg22
tanC)gH2(2
tanHCVACQ
An increase in the depth by a factor of the three ( from HAn increase in the depth by a factor of the three ( from H00 to 3Hto 3H00 ) ) results in an increase of the results in an increase of the flowrateflowrate by a factor ofby a factor of
6.15Hg22/tanCH3g22/tanC
QQ
2/501
2/501
H
H3
0
0

93
EL & HGL EL & HGL 1/41/4
For For steady, steady, inviscidinviscid, incompressible flow, incompressible flow , the total energy , the total energy remains constant along a streamline.remains constant along a streamline.
g/p
g2/V 2
zH
The head due to local static pressure (pressure energy)The head due to local static pressure (pressure energy)
The head due to local dynamic pressure (kinetic energy)The head due to local dynamic pressure (kinetic energy)
The elevation head ( potential energy )The elevation head ( potential energy )
The total head for the flowThe total head for the flow
Httanconszg2
VP 2
HEADHEAD
streamlinestreamlinetotal headtotal head

94
EL & HGL EL & HGL 2/42/4
Energy Line (EL) : represents the total head height.Energy Line (EL) : represents the total head height.
Hydraulic Grade Line (HGL) height: Hydraulic Grade Line (HGL) height: represents the sum of the represents the sum of the elevation and static pressure heads.elevation and static pressure heads.
The difference in heights between the The difference in heights between the EL and the HGLEL and the HGL represents represents the dynamic ( velocity ) headthe dynamic ( velocity ) head
zg2
VP 2
zP
g2/V2
streamlinestreamlinetotal headtotal head
streamlinestreamline
ELELHGLHGLsstreamlinetreamline

95
EL & HGL EL & HGL 3/43/4
Httanconszg2
VP 2

96
EL & HGL EL & HGL 4/44/4
Httanconszg2
VP 2
Httanconszg2
VP 2

97
Example 3.14 Example 3.14 Energy Line and Hydraulic Grade LineEnergy Line and Hydraulic Grade Line
Water is siphoned from the tank shown in Figure E3.14 through a Water is siphoned from the tank shown in Figure E3.14 through a hose of constant diameter. A small hole is found in the hose at hose of constant diameter. A small hole is found in the hose at location (1) as indicate. When the siphon is used, will water lelocation (1) as indicate. When the siphon is used, will water leak out ak out of the hose, or will air leak into the hose, thereby possibly caof the hose, or will air leak into the hose, thereby possibly causing using the siphon to malfunction?the siphon to malfunction?

98
Example 3.14Example 3.14 SolutionSolution1/21/2
Whether air will leak into or water will leak out of the hose dWhether air will leak into or water will leak out of the hose depends epends on on whether the pressure within the hose at (1) is less than or whether the pressure within the hose at (1) is less than or greater than atmosphericgreater than atmospheric. Which happens can be easily determined . Which happens can be easily determined by using the energy line and hydraulic grade line concepts. Withby using the energy line and hydraulic grade line concepts. With the the assumption of steady, incompressible, assumption of steady, incompressible, inviscidinviscid flow it follows that the flow it follows that the total head is constanttotal head is constantthus, the energy line is horizontal.thus, the energy line is horizontal.
Since the hose diameter is constant, it follows from the continuSince the hose diameter is constant, it follows from the continuity ity equation (AV=constant) that the water velocity in the hose is coequation (AV=constant) that the water velocity in the hose is constant nstant throughout. Thus throughout. Thus the hydraulic grade line is constant distance, Vthe hydraulic grade line is constant distance, V22/2g, /2g, below the energy linebelow the energy line as shown in Figure E3.14. as shown in Figure E3.14.

99
Example 3.14Example 3.14 SolutionSolution2/22/2
Since the pressure at the end of the hose is atmospheric, it folSince the pressure at the end of the hose is atmospheric, it follows that lows that the hydraulic grade line is at the same elevation as the end of the hydraulic grade line is at the same elevation as the end of the hose the hose outlet. outlet. The fluid within the hose at any point above the hydraulic gradeThe fluid within the hose at any point above the hydraulic gradeline will be at less than atmospheric pressure.line will be at less than atmospheric pressure.
Thus, Thus, air will leak into the hose through the hole at point (1). air will leak into the hose through the hole at point (1).

100
Restrictions on Use of the Bernoulli Restrictions on Use of the Bernoulli Equation Equation compressibility effects 1/4compressibility effects 1/4
The assumption of incompressibility is reasonable for The assumption of incompressibility is reasonable for most liquid flows.most liquid flows.
In certain instances, the assumption introduce considerable In certain instances, the assumption introduce considerable errors for gases.errors for gases.
To account for compressibility effectsTo account for compressibility effects
CgzV21dp 2

101
Restrictions on Use of the Bernoulli Restrictions on Use of the Bernoulli Equation Equation compressibility effects 2/4compressibility effects 2/4
For isothermal flow of perfect gas
For isentropic flow of perfect gas the density and pressure For isentropic flow of perfect gas the density and pressure are related by are related by P / P / kk =Ct, where k = Specific heat ratio=Ct, where k = Specific heat ratio
22
2
11
21 z
g2V
PPln
gRTz
g2V
ttanconsgzV21dPPC 2k
1k1
ttanconsgzV21dpRT 2
2
22
2
21
21
1
1 gz2
VP1k
kgz2
VP1k
k

102
Restrictions on Use of the Bernoulli Restrictions on Use of the Bernoulli Equation Equation compressibility effects 3/4compressibility effects 3/4
To find the pressure ratio as a function of Mach number
1111a1 kRT/Vc/VM The upstream Mach number
Speed of sound
1M2
1k1p
pp 1kk
21a
1
12Compressible flow
Incompressible flow21a
1
12 M2k
ppp

103
Restrictions on Use of the Bernoulli Restrictions on Use of the Bernoulli Equation Equation compressibility effects 4/4compressibility effects 4/4
21a
1
12 M2k
ppp
1M2
1k1p
pp 1kk
21a
1
12

104
Example 3.15 Compressible Flow Example 3.15 Compressible Flow Mach Mach NumberNumber A Boeing 777 flies at Mach 0.82 at an altitude of 10 km in a A Boeing 777 flies at Mach 0.82 at an altitude of 10 km in a
standard atmosphere. Determine the stagnation pressure on the standard atmosphere. Determine the stagnation pressure on the leading edge of its wing if the flow is incompressible; and if tleading edge of its wing if the flow is incompressible; and if the he flow is incompressible isentropic.flow is incompressible isentropic.
kPa5.12...pp
471.0...M2k
ppp
12
21a
1
12
For incompressible flowFor incompressible flow For compressible isentropic flowFor compressible isentropic flow
kPa7.14....pp
55.0...1M2
1k1p
pp
12
1kk
21a
1
12

105
Restrictions on Use of the Bernoulli Restrictions on Use of the Bernoulli Equation Equation unsteady effectsunsteady effects
For unsteady flow V = V ( s , t )For unsteady flow V = V ( s , t )
To account for unsteady effects To account for unsteady effects
sVV
tVaS
0dzVd21dpds
tV 2
Along a streamline
+ Incompressible condition+ Incompressible condition
2222
S
S12
11 zV21pds
tVzV
21p 2
1
Oscillations Oscillations in a Uin a Utubetube

106
Example 3.16 Unsteady Flow Example 3.16 Unsteady Flow UUTubeTube
An incompressible, An incompressible, inviscidinviscid liquid liquid is placed in a vertical, constant is placed in a vertical, constant diameter Udiameter Utube as indicated in tube as indicated in Figure E3.16. When released from Figure E3.16. When released from the the nonequilibriumnonequilibrium position shown, position shown, the liquid column will oscillate at a the liquid column will oscillate at a specific frequency. Determine this specific frequency. Determine this frequency.frequency.

107
Example 3.16Example 3.16 SolutionSolutionLet points (1) and (2) be at the airwater interface of the two columns of the tube and z=0 correspond to the equilibrium position of the interface.Hence z = 0 , p1 =p2 = 0, z1 = 0, z2 =  z , V1 = V2 = V z = z ( t )
dtdVds
dtdVds
tV 2
1
2
1
S
S
S
S
The total length of the liquid colum
/g20zg2dt
zd
gdtdzV
zdtdVz
2
2
Liquid oscillationLiquid oscillation