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1
ChE234 Thermodynamics
Overview
Module 1: Basic Concepts of
Thermodynamics
Bernard GalloisOffice: Burchard 410
Telephone: 201-216-5041
E-mail: [email protected]
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Office Hours, Burchard 410
Posted on Moodle
Exam Schedule
Posted on Moodle
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Introduction
Goal Today:
What is the course about?
What and how will I learn?
What are the tools, methods and
structured approaches that we will be
using?
Get started
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What Will You Ach ieve in th is
Course?
1. To learn the fundamental concepts ofthermodynamics
2. To develop an intuitive understanding of the subject
matter by emphasizing the physics and physical
arguments3. To master these basic principles and concepts by
applying this knowledge to a wealth of real-world
engineering applications through:
4. Structured and logical problem-solving techniquesthat you will use in homework assignments and
exams
5. Apply thermodynamics principles to the design of
simple devices and chemical processes4
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Major Course Objective:
I think, therefore I am.
Most people would sooner die thanthink; in fact, most do so. BertrandRussell (1872-1970)
Thinkwrongly, if you please, but in allcases thinkfor yourself. G.E. Lessing(1729-1781)
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How do we learn?
In good faith attempts to learn, we
remember: 1
10% of what we read
20% of what we hear 30%of what we read and hear
30% of what we see
70% of what we say
90% of what we teach or do
1Pike, R., 1989, Creative Training Techniques Handbook, Tips, Techniques andHow-tos for Delivering Effective Training; Lakewood Books, Minneapolis, MN,
153p.
1
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Student Evaluation
Weekly Exam (4) 30% (lowest dropped)
Quizzes 20% (lowest dropped)
Weekly Homework (6) 10% (lowest dropped)
Final Exam 40%
There will be NO make-up exams.
Any student who gets 90 percent of the total available pointsbefore the final exam (all exams and quizzes BUT not thehomework)will be excused from the final and will be given agrade of A.
Please consult the Web site for details on student evaluation,excuses, absences, etc
Attendance is mandatory: more than 2 absencesfrom class mean a full letter drop in the final grade.
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Curriculum Performance Criteria
(ABET)*
Please consult the Web site for a fulldescription of the performance criteria.
*Accreditation Board for Engineering and Technology
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Moodle Contents
Overview: student evaluation and policies
regarding excuses, absences, etc.Lecture notes
Solutions of homework problems (posted rightafter they are submitted)
Sample exams and final exam from previoussummer.
Your grades
Assignment every week: Learning objectives: what you should be able to do
Reading assignment Homework assignments. No late homework will be
accepted.
Other information
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Final Comments You have one weekafter you
received a grade on a given exam toget it changed if you consider that amistake was made. Please contactyour instructor at the end of therecitation period.
There will be NO make-up final examand should you miss it, you will need
to take the final exam the next timethe course is offered.
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Questions?
x5041
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Items Highlightedin Light Blue
ThroughoutAre a Must-Know
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Thermodynamics and Energy
Therme=Heat Dynamis=Power
Thermodynamics is a basic engineering science thatdeals with energy in all its forms and itstransformations for the design and operation ofenergy and other systems.
The macroscopic approach is called classicalthermodynamicsand is used to solve engineeringproblems whereas:
Statistical thermodynamics uses a microscopicapproachbased on the average behavior of largegroups of individual particles
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SOME APPLICATIONS AREAS OF
THERMODYNAMICS
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Rationale:
Energy is the single most important
challenge facing humanity today. Nobel
Laureate Rick Smalley, April 2004, Testimony
to U.S. Senate
What should be the centerpiece of a policyof American renewal is blindingly obvious:
making a quest for energy independence the
moon shot of our generation, Thomas L.
Friedman, New York Times, Sept. 23, 2005.
Whatever your major, energy issues may
play a key role in your career.
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JUST A FEW PIECES OF DATA ON
ENERGY, FOR NOW
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Global Energy Consumption
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http://nuclearfissionary.com/2010/04/02/comparing-energy-costs-of-nuclear-coal-gas-wind-and-solar/
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Energy Consumption vs GDP
GJ/capit
a-yr
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What is Energy?
What definitions would you
give? Think about the varioussystems shown on Slide 15
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COW CATCHER: An invention of the Stevens
family
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WHEN DID THERMODYNAMICS
START?
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The Newcomen Engine 1712
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Used to pump water out of mine
shafts
One of the first patents of the
industrial revolution
Very low efficiency
The valves were operated by ahuman operator at about 15
cycles/min
Pink is hot steam, blue is liquid
water
Can you figure out how it worked?
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A much improved Steam Engine of the type one would have
found around 1800+
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Thermodynamic Systems A (thermodynamic) system
is defined as a quantity ofmatter or a region of spacechosen for study
The region outside thesystem is called the
surroundings
The real or imaginarysurface that separates thesystem from the
surroundings is called theboundary
Systems may beopenorclosed
Cl ifi ti f B d i
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Classification of Boundaries
The interactions between a system and its surroundings
are governed by the nature of their common boundary.
Closed system: the boundary is impermeable to mass
flow.
Open system: the boundary allows for mass transport
across it.
The boundary can be rigid, movable or imaginary.
One other set completes the classification: adiabaticand
diathermal boundaries. These boundaries represent
extremes in the rate of heat exchange between the
system and its surroundings. The adiabatic boundary
plays a key role in thermodynamics and we wil return to
it when we introduce the concept of heat
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Adiabatic and Diathermal Boundaries
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Adiabatic and Diathermal BoundariesPlease refer to the next slide
Consider a rigid closed system (a can!) in which a thermometer has
been inserted. Surround this system with a system having a higher
temperature (dip it in hot water)
If the can were made of copper the variation of temperature with
time would look like curve 1 on the next slide.
Curves 2, 3, 4 would result if it was made of steel, glass or asbestos.
If the container was a thermos bottle (a Dewar), the variation oftemperature with time would be quite small (Curve 5)
The adiabatic wall is an idealized concept representing the limiting
case A in the figure. In practice, adiabatic boundaries are
approached in many situations especially those in which events
occur rapidly in relation to the time scale of the experiment.
The diathermal wall is the case diametric to the previous one. The
change in temperature is very rapid in relation to the time scale of
the experiment.
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Based on : J. Tester and M. Modell, Thermodynamics and its Applications 3d
edition, Prentice Hall, p.13
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Types of Boundaries
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Temperature-time behavior for different materials. Limiting
diathermal and adiabatic boundary behavior shown.
From: J. Tester and M. Modell, Thermodynamics and its Applications 3d
edition, Prenitce Hall, p.13
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Questions
You inflate a tire with a bicycle pump, under what
conditions would you consider the wall of the pump
to be diathermal? adiabatic?
(Note: The air inside the pump will heat up as you
compress it)
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The first action in considering a problem is to define
the system and, consequently, the location and the
nature of the boundaries:
Closed or open system (permeable or impermeable
boundary)
Rigid or movable
Diathermal or adiabatic
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Defining the System
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Closed Systems
Mass cannot cross theboundaries of a closedsystem but energy can
The boundary of a closed
system can move Examples includes sealed
tanks and piston/cylinderdevices
Energy in the form of heatand work may cross theboundaries of a closedsystem
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Open System and Control Volume
An open system or
control volume hasmass as well as energycrossing the boundary,often called the controlsurface. The surfacecan be real orimaginary.
Examples includepumps, compressors,turbines, nozzles,valves and heat
exchangers Proper choice of a
control volume cansimplify the analysis ofthe system
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Control Volume: Examples
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Isolated Systems An isolated system is a general system of fixed
mass where no heat or work may cross the
boundary. It is a closed system with no energy crossing the
boundaries.
It is normally a collection of a main system and itssurroundings that are exchanging mass and energy
among themselves and no other system.
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Property
A propertyis a characteristic of a system inequilibrium, independent of the path used toarrive at the systems condition.
A property may be intensive or extensive
Extensive propertiesdepend on the size orextent of the system. e.g. mass, volume,total energy, mass dependent property
Intensive propertiesare independent of thesize of the system. e.g. temperature,pressure, color, age, any mass independentproperty
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Specific Properties
How about these properties?
Density
Specific volume: volume per unit mass Specific energy: energy per unit mass
V
m
1
m
v
V
m
e
E
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STATE AND EQUILIBRIUM
A system is said to be in thermodynamic equilibriumifit maintains
othermal, (uniform temperature)
omechanical(uniform pressure)
ophase(the mass of the two phases, e.g. ice and liquid
water, in equilibrium) and
ochemicalequilibrium
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PROCESS
Any change from one state to another is called a process
During a quasi-equilibrium or quasi-staticprocess thesystem remains practically in equilibrium at all times.
Can you think of a real engineering process that is quasi-
static? Would that be useful?
We will often assume that processes we analyze are quasi-equilibrium
processes because they are easy to analyze (the equations of state apply)
and work-producing devices deliver the most work when they operate on a
quasi-equilibrium process.
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EXAMPLE: CONSTANT PRESSURE
PROCESS
In most of the processes
that we will study, one
thermodynamic property
is held constant. Isobaric: constant P
Isothermal: constant T
Isochoric: constant V
Isentropic: constant S
(S is entropy, Chapter 6)
At equilibrium, the force
exerted by the water on the
lower face of the piston is
equal to the combined
weight of the brick andpiston (a constant). The
pressure in the tank is thus
a constant even when the
water is heated.
P b t ill t t d b di
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Processes are best illustrated by a diagram,
a useful approach when solving problems
Using English sentences you
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Using English sentences, you
must be able to define:
Closed system Open system
Isolated system
Control volume
Control surface
Intensive property
Extensive property
State and equilibrium
Quasi-static or equilibrium process
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The Steady-Flow Process
During a steady-flowprocess, fluid propertiesmay change with positionbut not with time.
Steady-flow conditionsessentially prevail in manyengineering devices.
Therefore, the volume, themass and the energycontent of the controlvolume remain constantduring the entire process.
STATE POSTULATE
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STATE POSTULATE
The state of a system is described by its properties. By
experience, not all properties need to be known to specify the
state of the system. In fact, the number of properties required
to fix the state of simple, homogeneous system is given by the
state postulate.
In a simple compressiblesystem, there are no electrical,
magnetic, gravitational, motion or surface tension effects. An
additional property need to be specified for each effect that issignificant.
In ahomogeneoussubstance, the thermodynamic properties
are uniform throughout.
Two properties are independent if one can be varied while the
other is held constant.
The thermodynamic state of a simplecompressible system is completely specified by
two independent intensive properties.
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CYCLES
A system is said to have
undergone a cycle if itreturns to its initial state at
the end of the process.
The illustration shows a
cycle consisting of twoprocesses.
Along process A, both P and
V change from state 1 to
state 2.
To complete the cycle, P and
V change from state 2 to
state 1 in process B.
Keep in mind that all other
thermodynamic properties
must also change so that the
pressure is a function ofvolume as described in these
two processes.
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UNITS
In this course, we shall use S.I. (Systeme
International) units exclusively. The seven fundamental units: Length: meter m
Mass: kilogram kg
Time: second s Temperature: kelvin K
Amount of light: candela cd
Electric current: ampere A
Amount of matter: mole mol All other units are derived from the
fundamental units
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MORE ON UNITS
Velocity: length/time m/s
Acceleration: velocity/time m/s2
Force: mass x acceleration kg m/s2
Pressure: force/area kgm-1/s2
Work (energy): force x distance kgm2/s2
Power: work/time kgm2
s
Quantity Derived from: Dimensions Unit
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Quantity Derived from: Dimensions Unit
Area L2 m2
Volume L3 m3
Density Mass/volume ML-3 kg/m3Specific volume Volume/mass M-1L3 m3/kg
Velocity Length/time LT-1 m/s
Acceleration Velocity/time LT-2 m/s2
Force Mass x acceler. MLT-2 N (newton)
Pressure Force/area ML-1T-2 N/m2
Work or energy Force x length M L2 T-2 J (joule)
Power Energy/time M L2 T-3 W (watt)Entropy Energy/temp. M L2 T-2K-1 J/K
Specific entropy
Specific energy
Entropy/mass
Energy/mass
L2 T-2K-1
L2 T-2
J/kgK
J/kg
Temperature and the Zeroth Law of
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Temperature and the Zeroth Law of
Thermodynamics What is temperature?
Temperature measurements are based onpredictable and reliable changes in the properties ofmaterials as they are heated or cooled: expansion/contraction of metals or other substances,resistance of platinum, change in color, etc
At thermal equilibrium, two bodies have equaltemperatures.
The zeroth law of thermodynamicsstates that whentwo bodies are in thermal equilibrium with a third
body, they are also in equilibrium with each other If the third body is a thermometer: two bodies are in
thermal equilibrium if both have the sametemperature reading even if they are not in contact
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The Ideal Gas Temperature Scale
We need to have a temperature scale that is
independent of the properties of any substance: athermodynamic temperature scale, or a kelvin scale
The ideal gas temperature scaleis such a scale.
At low pressures, T is proportional to P : T= a +bP
a and b can be determined experimentally with a gasthermometer by using only two reproducible points(ice and steam point of water, freezing point of puresubstances) to determine the two unknowns a and b.
The unknown temperature T of a given medium can
then be determined by interpolation. In the Celsius scale, the freezing and boiling points
are assigned values of 0 and 100 respectively.
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The Absolute Gas Temperature Scale
When using different types
of gases at low pressures,plots of P as a function of T
extrapolate to -273.15 oC, the
lowest attainable
temperature, also called
absolute zero.
In the absolute gas
temperature scale, T = bP
and the temperature only
needs to be specified at a
single point to define the
absolute gas temperature
scale
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Temperature Scales
T(R) = T(oF) + 459.67
T(R) = 1.8 T(K)The Celsius scale is defined interms of a single point, thetriple point of water (0.01oC)and the absolute temperature
scale. The ice point remains0oC (273.15 K) and the boilingpoint remains 100oC (373.15K)at one atmosphere pressure.(The normal temperature of the humanbody is 37.1oC or 98.8oF)
T(K) = T(o
C) + 273.151 K = 1 oCT(oF) = 1.8 T(oC) + 32
N molecules Kinetic Theor of Ideal Gas
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The temperature of an ideal monatomic gas is a measure related to
the average kinetic energy of its atoms as they move. In this
animation, the size of helium atoms relative to their spacing is
shown to scale under 1950 atmospheres of pressure. These room-
temperature atoms have a certain, average speed (slowed down
here two trillion fold).
N molecules
Cubic box of side l
Volume V = l3
Constant temperature
Spherical elastic particles inconstant random motion
Elastic collisions with the walls and
between particles.
The interactions among molecules
are negligible. They exert no forces
on one another except during
collisions.
The total volume of the individual
gas molecules added up is negligible
compared to the volume of the
container.
Kinetic Theory of Ideal Gas
53
Pressure = Force exerted by molecules on a
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y
surface per unit area
A gas molecule collides with the wall of the
container perpendicular to the xaxis and bouncesoff in the opposite direction with the same speed (an
elastic collision). The momentum lost by the particle
and gained by the wall is:
The particle impacts the wall once every 2l /vxtime
units and produces a momentum change on the wall
once every 2l /vxtime units.
The force on the wall due to the particle is given by
2x i f xp p p mv
22
2 /
x x
x
mv mvpF
t l v l
54
Pressure cont.
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Pressure cont.
The force exerted by N particles of mass m can be written as:
The pressure is given by
The total mass of gas is Nmand the density is Nm/V, the
density
so that
The pressure is proportional to the density of the gas and the
root mean square velocity.
2
rmstotal mNvF
l
2 23
2
1
since
wall rms rmsF mNv mNv
P V lA l l V
21
3 rmsP v
55
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Units of Pressure
The SI unit is the pascal equal to onenewton per square meter. 1 Pa = 1 N/m2
It is a small unit so that kilopascals kPa=
103Paand megapascals Mpa= 106Paareused commonly.
Other units widely used include:
1 bar = 105
Pa1 atm = 101,325 Pa = 101.325 kPa =1.01235 bar = 760 torr
Gage pressure vacuum pressure atmospheric
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Gage pressure, vacuum pressure, atmospheric
pressure, absolute pressure
Pgage
= Pabs
Patm
Pvac= Patm- Pabs
What is the origin of atmospheric pressure? The weight of the column of
air above us!
The pressure is the same at all points on a
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The pressure is the same at all points on a
horizontal plane in a given fluid regardless of
geometry, provided that the points are
interconnected by the same fluid.
Forces Exerted on a Fluid Column
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Forces Exerted on a Fluid ColumnConsider an element of fluid of height h and
area A and the free body diagram.
The pressure P1exerted on the top face of the
element = F1x area
The pressure P2exerted on the bottom face of
the element = F2x area
From the free body diagram:
F2= F1+ mg
P2A = P1A + mg but m =density x volume = AhFrom which we deduce
P2P1= gh
As we move down in a fluid , the pressureincreases (diving in the ocean).
As we move up in a fluid, the pressure
decreases (climbing a mountain).
F2
F1
h
mg
The Manometer
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e a o ete
The manometer is used tomeasure small andmoderate pressuredifferences.
How small is small:~ 103kg/m3 , g ~10 m/s2 h ~
0.1 m
P ~ 0.1x104Pa ~ 0.01 atm~0.01 bar
Pressure due to a columnof water 10 m high:
P = 103 x10x10 ~105Pa
Patm
Pascals experiment: by
running a long pipe up amountain and into a barrel ,he was able to burst thebarrel!
P1= P2 (same level in connected fluid)P2 = Patm+ gh
Barometer and the Atmospheric
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Barometer and the Atmospheric
Pressure:
The Basic Barometer
A force balance in the verticaldirection yields:
Patm= gh
Standard atmosphere:
13 595 kg/m3
(at 0o
C)g = 9.807 m/s2(standard g)
h = 0.760 m (760 mm)
Patm= 101.325 kPa
Patm= 760 mm Hg
Patm= 29.92 inHg
Patm= 760 torr
Vacuum
Note: atmospheric pressure decreases with
altitude; why?
Engineering Units To Know
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g g
Energy: kJ and kWh
1 kWh = 1000Wx3600s = 3.6x106
J= 3.6x103kJ
Pressure
1 MPa = 1000 kPa 1 bar =100,000 Pa =100 kPa
1 atm = 760 mmHg = 101.325 kPa
Volume 1 L = 1000cm3= 0.001 m3
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Work
Energy Transfer by Work
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Energy Transfer by Work
Mechanical work, W, is performed
whenever a force, F, acts through adistance, dl:
W = Fdl
The work done during a process betweentwo states, 1 and 2, is denoted W12 orsimply W
Work done per unit mass w = W/m (J/kg) The work done per unit time is called
power and is denoted (.
W
Some Important Caveats
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Some Important Caveats
Work is a boundary phenomenon.
Systems possess energy, but not work.
Work is associated with a process, not a
state.
Work is a path function: its magnitude
depends on the path followed during a
process.
Path Functions and Point Functions
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Path Functions and Point Functions
Path functions have inexact
differentials denoted by d.A differential amount ofwork or heat is representedby dW or dQ not dW or dQ.
Properties are pointfunctions and they haveexact differentialsrepresented by the symbold as in dV. They dependon the initial and finalstates only and not on thepath taken to go fromstate1 to state 2.
The volume change during
process 1-2 is V2
V1
=
V
irrespective of path.
The total work during the
process, W12(not W and not
W2W1) depends on the path
taken.
Mechanical Forms of Work
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For a work interaction to exist between a system
and its surroundings:
There must be a force acting on the boundary.
The boundary must move.
If the force is constant: W= Fs (kJ)
If the force is not constant:
The integral assumes that we know the relationbetween F and s
2
1
( )W F s ds
Potential Energy and Kinetic Energy
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Potential Energy and Kinetic Energy
Gravitational Workis the work done by oragainst gravity. The force acting on a body is F = mg. The work is
given by:Wg= mg( z2z1)
where z1z2is the vertical distance traveled.
This is simply the change in potential energy.
Accelerational workis associated with a change in velocity of asystem.F = ma = m dV d t V = ds /dt ds = V d t
A simple integration yields:
Wa
= m(V2
2V1
2)
This is simply the change in kinetic energy.
Example: Conservation of Energy
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a p e Co se at o o e gy
The energy of a falling object is
conserved:Wg= mg( z2z1)
Wa= m(V22V1
2)
Wg +Wa = 0
mg( z2z1) + m(V22V1
2) = 0
Potential energy is transformed into kinetic
energy.
Shaft Work
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Shaft Work
Very often, the torquet (and hence the
force F) applied to a shaft is constant. Wecalculate the work done in this case
A force F acting through a moment armr
generates a torque given by T Fr
This force acts through a distance s which
is related to the radius r by s = (2pr)n,
where n s the number of revolutions
(2 ) 2T
W Fs rn nT r
p p
Spring Work, Elastic
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p g ,
For linear elastic springs, the displacement x isproportional to the force: F = - kx
The displacement is measured from theequilibrium position (x = 0 when F= 0)
The work done is
Where x1and x2are the initial and final
displacements of the spring measured from theundisturbed (equilibrium) position.
2
1
2 2
2 11 ( )2
x
x
W Fdx k x x
Electrical Work
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Electrical Work
V
We = VN
Power = VI
= RI2
= V2/R
I
When N coulombs of electrical charge move
through a potential difference V, the electricalwork is We= VN
Moving Boundary Work
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Moving Boundary Work
This process is closely
approximated in real enginesprovided the piston moves atlow velocities (unlike thepistons in an automobileengine).
(Pistons in an automobile enginemove so fast the process path
cannot be specified. The workdone is determined by directmeasurements.)
The work associated with
a moving boundary is
called boundary work.
The analysis is for a quasi-static or quasi-equilibrium
process for which the work
output is a maximum.
Moving Boundary Work (cont.)
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Moving Boundary Work (cont.)
By convention, work is positivewhen the displacement is in the
same direction as the applied forceand negative when they are inopposite directions.
The differential work done is:
Expansion: dV>0, dWb< 0
Compression dV 0
The expression above is theboundary work input for theprocess.
Initial pressure: P
Total volume: V
Area of piston: A
The piston moves a
distance dsin a quasi-
equilibrium manner
2
1
t
t
PdVW
PdVPAdsFdsWd
Moving Boundary Work (cont.)
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The total boundary work doneduring the process as thepiston moves is:
The integral can only becalculated if we know the
functional relationshipbetween P and V during theprocess: P = f(V)
P = f(V) is the equation of theprocess path
The total area under theprocess path is equal, inmagnitude, to the work done inthe quasi-staticprocess
2
1
PdVWb 2
1
2
1
PdVdAAArea
This is a closed system
Moving Boundary Work (cont )
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Moving Boundary Work (cont.) The boundary work done
during a process depends on
the path followed as well asthe end states. Work is a pathfunction.
The net work during a cycle isthe difference between thework done by the system and
the work done on the system. P is the pressure at the inner
face of the piston, equal to thepressure in the gas only if theprocess is quasi-equilibrium sothat the pressure is uniform inthe cylinder at any time.
Expansion
Compression
2
1
dVPW ib
Example: Constant Volume Process
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dV = 0
dW = -PdV = 0
If the working fluid is an
ideal gas, what willhappen to the temperature
during a constant volume
process?
No work is done but:
PVt= nRT or
P/T = nR/Vt = const.
P1
/T1
= P2
/T2
In this case P1> P2Consequently T1> T2The energy of the gas
decreases
Example: constant pressure process
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For the constant pressure
process shown here, is the
boundary work positive ornegative?
It is a compression process
so the work done is negative
Will the temperature changeduring the process?
For one mole of gas
PV = RT or V/T = R/P = const.
V1/T1= V2/T2In this case V1> V2
Consequently T1> T2The energy of the gas decreases!
dW = -PdV
The integrat ion is
straighto rward sin ce P isconstant.
W = P (V1V2)
Heat Transfer
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Energy can cross theboundary of a closed system
in two distinct form: heat andwork.
Heat is the form of energythat is transferred betweentwo systems (or a system
and its surroundings) byvirtue of a temperaturedifference.We call thisprocess heat transfer.
The larger the temperaturedifference, the higher is therate of heat transfer.
Thermal energy refers to forms
of energy such a latent and
sensible energies to prevent
confusion with heat transfer
Adiabatic Process Insulation
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Adiabatic Process
During an adiabaticprocess, a system
exchanges no heatwith the surroundings.
Q = 0AdiabaticSystem
Notation and Units
Heat has the energy unit of kJ. The amount of heat transferred during a processbetween states 1 and 2 is denoted Q12 or just Q.
The heat transfer per unit mass is q = Q/m
The heat transfer per unit mass is q = Q/m The rate of heat transfer is denoted
When the rate is constant during a process:
Q = t
Q
Q
Some Important Caveats
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Heat and work are boundary phenomena.
Systems possess energy, but not heat or
work.
Both are associated with a process, not a
state.
Both are path functions: their magnitude
depends on the path followed during aprocess.
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If the energy crossing the
boundary of a closed system is
not heat, it must be work
(Heat is easy to recognize since itsdriving forceis a temperature
difference)
Problem-Solving
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Problem-solving is at the heart of the engineeringprofession. A great engineer is a great problem solver.
While problem-solving may be considered by some to bean art since different approaches may be warranteddepending on the nature of the problem at hand and thematurity of the problem solver, there is, however, a verygeneral method that is presented in this module.
As we progress in the course, specific approaches orvariations of this technique will be used.
You are more than encouraged to use thesesapproaches, which will be systematically used in thesolutions we will provide of homework, practice andexam problems.
A General Problem-Solving Technique
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1. Problem statement
2. Schematic3. Assumptions
4. Properties
5. Physical laws
6. More needed properties7. Final Equations
8. Calculations
9. Reasoning, verification and
discussion
Analysis
Synthesis
EvaluationAny engineering analysis presented to others is a form ofcommunication. Neatness, organization, completeness and visualappearance are quite important for maximum impact.
Problem-Solving TechniqueCont.
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1. Problem statement
In your own words, state the problem, the key informationgiven and the quantities to be found
2. SchematicDraw a realistic sketch of the system and list the relevantinformation on the figure, especially your choice of system orcontrol volume
3. AssumptionsState any appropriate assumptions, made to simplify theproblem. Justify these assumptions.
4. PropertiesWrite down the known properties. Identify the unknown
properties at known states necessary to solve the problem.Indicate their source
5. Physical lawsApply all the relevant basic physical laws and simplify them byusing the assumptions
Problem-Solving Technique Cont
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Problem Solving Technique Cont
6 Properties
Determine the unknown properties at known states necessaryto solve the problem. Indicate their source
6 Final Equations
Write down the final equations
7 CalculationsSubstitute the known quantities in the equations and performthe calculations to determine the unknowns. Pay attention tounits and dimensions. Keep a suitable number of significantdigits.
8 Reasoning, verification and discussionReview your work. Validity of assumptions? Do the numericalresults make sense? Repeat the calculations if a number lookstoo small or too large.