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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

    2

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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

    3

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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)

    5

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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

    6

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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.

    7

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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

    8

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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

    9

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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.

    10

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    Questions?

    [email protected] 410

    x5041

    11

    mailto:[email protected]:[email protected]
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    Items Highlightedin Light Blue

    ThroughoutAre a Must-Know

    12

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    13

    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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    14

    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.

    15

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    JUST A FEW PIECES OF DATA ON

    ENERGY, FOR NOW

    16

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    Global Energy Consumption

    17

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    18

    http://nuclearfissionary.com/2010/04/02/comparing-energy-costs-of-nuclear-coal-gas-wind-and-solar/

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    19

    Energy Consumption vs GDP

    GJ/capit

    a-yr

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    20

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    What is Energy?

    What definitions would you

    give? Think about the varioussystems shown on Slide 15

    21

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    22

    COW CATCHER: An invention of the Stevens

    family

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    WHEN DID THERMODYNAMICS

    START?

    23

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    The Newcomen Engine 1712

    24

    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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    25

    A much improved Steam Engine of the type one would have

    found around 1800+

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    26

    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

    27

    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.

    28

    Based on : J. Tester and M. Modell, Thermodynamics and its Applications 3d

    edition, Prentice Hall, p.13

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    Types of Boundaries

    29

    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)

    30

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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

    31

    Defining the System

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    32

    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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    33

    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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    34

    Control Volume: Examples

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    35

    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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    36

    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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    37

    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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    38

    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

    42

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    43

    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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    46

    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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    56

    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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    61

    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

    62

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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.


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