Chapter 5-Without Moment of Momentum
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Transcript of Chapter 5-Without Moment of Momentum
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Chapter 5: Finite Control
Volume AnalysisConservation of mass The continuity equation
Newtons 2nd Law The linear momentum and moment-of-
momentum equations
First law of thermodynamics The energy equation
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Conservation of Mass
Conservation of mass principle
As applied to a system
Time rate of change of the system mass = 0,
As applied to a coinciding system with a
CVTime rate of change of
the mass of the
coincident system
=
Time rate of change of
the mass of the contents
of the coincident controlvolume
+
Net rate of flow of
mass through the
control surfaces
0
Dt
DMsys
sys CSCV
dAVdt
VdDt
DnV
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Conservation of Mass
(cont.)The control volume expression for
conservation of mass is commonly
known as the cont inui ty equation
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Conservation of Mass
(cont.)
0
dAVdt CSCV nV
For a fixed, non-
deforming CV
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When the flow is steady
When the flow is steady and
incompressible
Conservation of Mass
(cont.)
0inout mm
0inout QQ
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Forsteady flow involving only one
stream of a specific fluid flowing thru a
CV at sections (1) and (2)
Forsteady, incompressible flow
involving only one stream of a specificfluid flowing thru a CV at sections (1)
and (2)
Conservation of Mass
(cont.)
222111 VAVAm
2211 VAVAQ
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The control volume expression for
conservation of mass for a moving,
nondeforming control volume is thesame as that for a stationary control
volume, provided the absolute
velocity is replaced by the relative
velocity.
Conservation of Mass
(cont.)
CVabsolute
CSCV
VWV
dAWVdt
where
0n
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Example 1
The wind blows through a 7 ft X 10 ft garage door opening with a
speed of 5 ft/s as shown. Determine the average speed, V, of the
air through the two 3 ft X 4 ft openings in the windows.
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Example 2
Storm sewer backup causes your basement to flood at the steady
rate of 1 in. of depth per hour. The basement floor area is 1500 ft2.
What capacity (gal/min) pump would you rent to
(a) keep the water accumulated in your basement at a constant
level until the storm sewer is blocked off?
(b) reduce the water accumulation in your basement at a rate of 3
in/hr even while the backup problem exist?
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Newtons 2nd Law
Newtons 2nd Law of motion for a
systemTime rate of change of
the linear momentum ofthe system
= Sum of external forcesacting on the system
sysFVdDtD
sysV
CSCV
dAVdt
nVVV CVcoincidentofcontentsF
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Newtons 2nd Law
Forces involved are the body force andsurface forces.
The only body force we are considering is
the one associated with the action ofgravity, i.e. the weight.
The surface forces are exerted on thecontents of the CV by the material just
outside the CV in contact with the materialjust inside the CV.
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Newtons 2nd Law (cont.)
volumecontroltheofcontentsFnVVV dAVdt CSCV
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Newtons 2nd Law (cont.)
Some notes on the Linear Momentum
Equation
It is directional; it can have components in
x,y,z coordinate directionsMomentum flow out of the control volume
involves a positive
If the CS is selected so that it is perpendicular
to the flow where fluid enters or leaves the CV,the surface force exerted at these locations by
fluid outside the control volume on fluid inside
will be due to pressure.
nV
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Newtons 2nd Law (cont.)
When subsonic flow exits from a controlvolume into the atmosphere, atmosphericpressure prevails at the exit cross section.
Only external forces acting on the contents of
the control volume are considered in the linearmomentum equation
The force required to anchor an object willgenerally exist in response to the surfacepressure and/or shear forces acting on the CS,
to a change in linear momentum flow throughthe CV containing the object, and to theweight of the object and the fluid contained inthe CV.
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Newtons 2nd Law (cont.)
Fluid flows can lead to a reaction
force in the following ways
Linear momentum flow variation indirection and/or magnitude
Fluid pressure forces
Fluid friction forces
Fluid weight
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Example 3
Water enters the horizontal, circular cross section sudden
contraction nozzle at section (1) with a uniformly distributed
velocity of 25 ft/s and a pressure of 75 psi. The water exits from
the nozzle into the atmosphere at section (2) where the uniformly
distributed velocity is 100 ft/s. Determine the axial component of
the anchoring force required to hold the contraction in place.
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Example 4
The thrust developed to propel the jet ski shown is a result of water
pumped through the vehicle and exiting as a high speed water jet.
For the conditions shown in the figure, what flowrate is needed to
produce a 300 lb thrust? Assume the inlet and outlet jets of water
are free jets.
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More Examples
Water flows as two free jets from the tee attached to the pipe as
shown. The exit speed is 15 m/s. If viscous effects and gravity are
negligible, determine the x and y components of the force that the
pipe exerts on the tee.
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More ExamplesA circular plate having a diameter of 300 mm is held perpendicular to
an axisymmetric horizontal jet of air having a velocity of 40 m/s
and a diameter of 80 mm as shown. A hole at the center of the
plate results in a discharge jet of air having a velocity of 40 m/s
and a diameter of 20 mm. Determine the horizontal component of
force required to hold the plate stationary.
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More ExamplesA vertical circular cross section jet of air strikes a conical deflector
as shown. A vertical anchoring force of 0.1N is required to hold
the deflector in the place. Determine the mass (kg) of the
deflector. The magnitude of the velocity of the air remains
constant.
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More ExamplesAir flows into the atmosphere from a nozzle and strikes a vertical
plate as shown. A horizontal force of 9 N is required to hold the
plate in place. Determine the reading on the pressure gage.
Assume the flow to be incompressible and frictionless.
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More ExamplesAir discharges from a 2-in.-diameter nozzle and strikes a curvedvane, which is in a vertical plane as shown. A stagnation tube
connected to a water U-tube manometer is located in the free air
jet. Determine the horizontal component of the force that the air jet
exerts on the vane. Neglect the weight of the air and all friction.
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First Law of
ThermodynamicsTime rate of increase of
the total stored energy
of the system=
Net time rate of energy
addition by heat
transfer into the system+
Net time rate of
energy addition
by work transfer
into the system
gzV
ue 2
2
innetQ
innetW
Represents the ways in
which energy isexchanged between the
CV contents and
surroundings because of a
temperature difference
Also known as power.+ when work is done
on the contents of the
CV by surroundings and
vice versa
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First Law of
Thermodynamics (cont.)
outin
QQQ innet
outin WWW innet
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Work transfer
In many instances, work is transferred by amoving shaft
Work can also occur at the CS when a forceassociated with the fluid normal stress acts
over a distance
Work transfer can also occur due to tangentialstress but is usually negligible
First Law of
Thermodynamics (cont.)
shaftrotatingforntdisplacemeofrateXforce
shaftshaft
TW
W
CS dApW nVstressnormal
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First Law of
Thermodynamics (cont.)
innetshaftinnet
2
2WQdAgz
VpudVe
t CSCV
nV
From normalstress From
moving
shaft
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If there is only one steady stream
entering and leaving the CV, and if all
the properties are assumed to be
uniformly distributed over the flow
cross-sectional areas involved
First Law of
Thermodynamics (cont.)
innet
shaftinnet
22
2WQzzgVVppuum inoutinout
inout
inout
Valid for compressible and incompressible flow
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C i f th E
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Comparison of the Energy
Eqn with the Bernoulli
EquationFor steady, incompressible flow with zero
shaft power and negligible viscous forces
effects, the energy equation becomes theBernoulli Equation
For steady, incompressible flow with
friction,
inin
inoutout
out zV
pzV
p
22
22
0lossinnet quu inout
Loss of useful or available
energy that occurs in an
incompressible fluid flow
due to friction
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First Law of
Thermodynamics (cont.)Other related equations
Used for one dimensional steady-in-the-mean, incompressible flow withfriction and shaft work. Also knownas the Mechanical Energy Equat ionor the Extended Bernoul l i Equat ion
loss22 innetshaft
22
wgzVp
gz
Vpin
ininout
outout
minnetshaft
innetshaft
Ww
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First Law of
Thermodynamics (cont.)For non-uniform velocity distribution
(velocity profile at any cross section
where flow crosses the control surface is
not uniform),
where is the kinetic energy coefficient andis the average velocity.
loss22 innet
shaft
22
wgzVp
gzVp
inininin
outoutoutout
V
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Example 6
Air flows past an object in a pipe of 2-m diameter and exits as a free
jet as shown. The velocity and pressure upstream are uniform at
10 m/s and 50 N/m2, respectively. At the pipe exit, the velocity is
nonuniform as indicated. The shear stress along the pipe wall is
negligible.
(a) Determine the head loss associated with a particle as it flowsfrom the uniform velocity upstream of the object to the location in
the wake at the exit plane of the pipe.
(b) Determine the force that the air puts on the object.
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Example 7
What is the maximum possible power output of the hydroelectric
turbine shown in the figure.
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Example 8
Water is to be moved from one large reservoir to another at a higher
elevation. The loss in available energy associated with 2.5 ft3/s
being pumped from sections (1) to (2) is 61V2/2 where V is the
average velocity of water in the 8-in inside diameter piping
involved. Determine the amount of shaft power required.
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More Examples
Water flows steadily down the inclined pipe as shown. Determine thefollowing:
(a) The difference in pressure, p1-p2
(b) The loss between sections (1) and (2)
(c) The net axial force exerted by the pipe wall on the flowing water
between sections (1) and (2)
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More Examples
Water flows by gravity from one lake to another as shown at a steady
rate of 100 gpm. What is the loss in available energy associated
with this flow? If this same amount of loss is associated with
pumping the fluid from the lower lake to the higher one at the
same flowrate, estimate the amount of pumping power required.