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    ChemicalEngineeringThermodynamics

    CCB 2024Dr. Lukman Ismail (Block 05-03-35) & Dr. Lau Kok Keong

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    Nama Mata Pelajaran /

    Subject Name

    Termodinamik Kejuruteraan Kimia / Chemical Engineering

    Thermodynamics

    Kod / Code CCB 2024

    Status Mata Pelajaran /

    Subject Status

    Teras / Core

    Peringkat / Level Sarjana Muda / Bachelor

    Nilai Kredit / Credit Value 4

    Prasyarat (jika ada) /

    Prerequisite (if any)

    Physical Chemistry

    Penilaian / AssessmentQuiz / Test / Assignment 40%

    Final Exam 60%

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    Outcome-Based Education (OBE)

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    1. Apply knowledge of mathematics, science and engineering fundamentals and an engineering

    specialisation to the solution of complex chemical engineering problems.

    2. Identify, formulate, research literature and analyse complex chemical engineering problems

    reaching substantiated conclusions using principles of mathematics, natural sciences and

    engineering sciences3. Design solutions for complex chemical engineering problems and design systems, components or

    processes that meet specified needs with appropriate consideration for public health and safety,

    cultural, societal, and environmental considerations.

    4. Investigate complex chemical engineering problems using research based knowledge and

    research methods including design of experiments, analysis and interpretation of data and

    synthesis of information to provide valid conclusions.

    5. Use modern engineering and IT tools to evaluate complex chemical engineering activities.

    6. Apply reasoning informed by contextual knowledge to assess societal, health, safety, legal and

    cultural issues and the consequent responsibilities relevant to professional engineering practice.

    7. Understand the impact of professional engineering solutions in societal and environmental

    contexts and demonstrate knowledge of and need for sustainable development.

    8. Apply ethical principles and commit to professional ethics and responsibilities and norms of

    chemical engineering practice

    9. Communicate effectively on complex chemical engineering activities with the engineering

    community and society.10. Function effectively as an individual, and as a member or leader in diverse teams and in multi-

    disciplinary settings.

    11. Recognise the need for, and have the preparation and ability to engage in independent and life-

    long learning in the broadest context of technological change.

    12. Demonstrate knowledge and understanding of engineering and management principles and apply

    these to ones own work, as a member and leader in a team, to manage projects and in

    multidisciplinary environments.

    Chemical Engineering Programme Outcomes (PO)

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    At the end of this course, students should be able to:

    1. explain and apply the fundamental principles and laws

    of thermodynamics.

    2. apply the laws of thermodynamics to solve chemical

    engineering problems such as fluid properties, phaseequilibria, chemical reaction equilibria and power

    cycle.

    3. perform different methods of solution to solve ideal/real

    gas/liquid in pure component/mixtures.

    4. relate the chemical thermodynamics principles with the

    application in separation and reaction processes.

    Course Learning Outcomes

    The above course learn ing outcomes are mapped to the three highl ighted

    programme outcomes i.e., PO1& 2

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    References:Text book for the 1st part

    Thermodynamics: An Engineering Approach(7 th edition)

    Yunus A. Cengel & Michael A. Boles

    Supplements:

    1) Fundamentals of Engineering Thermodynamics

    by Moran & Shapiro

    2) Fundamentals of Thermodynamics

    by Sonntag, Borgnakke & Van Wylen3) Engineering Thermodynamics

    by J.B. Jones

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    Coursework

    Total = 40 %

    20% - Dr. Lukman

    20% - Dr. Lau

    20% - Test 10%

    - Quiz 2%

    - Video assignment 8%

    Final exam (60%): Must obtain 20% minimum

    marks, otherwise fail for the course

    Attendance : Must exceed 90%, below which the students canbe barred from the final exam.

    Attendance of all international students will be recorded and

    submitted to the Ministry of Education and will be forwarded to the

    Ministry of Home Affairs.

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    Course Outlines:

    Chapter 1: Basics Concepts of Thermodynamics

    Chapter 2: Properties of Pure SubstancesChapter 3: Energy Transfer by Heat, Work and

    Mass

    Chapter 4: The First Law of ThermodynamicsChapter 5: The Second Law of Thermodynamicsand Entropy

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    CHAPTER 1

    BASIC

    CONCEPTS OF

    THERMODYNAMICS

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    What is Thermodynamics?

    Early description: Convert heat into power

    Current Definition:

    The study of energy and energy transformations, includingpower generation, refrigeration and relationship among theproperties of matter.

    Greek Words

    Therme

    (Heat)

    Dynamis

    (Power)

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    1.1 What is Energy?

    Ability to cause changes

    Laws of Thermodynamics:

    Zeroth Law = dealing with thermal equilibrium {if two systems arein thermal equilibrium with a third system, they are also in thermalequilibrium with each other}

    First Law = deal with conservation of energy

    {during an interaction, energy can change from one form toanother but the total amount of energy remains constant. E.g. a rockfalling off a cliff & in the diet industry}

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    Second Law = energy has qualityas well as quantity,and actual processes occur in the direction of decreasingthe quality of energy.

    heatHot Cold body, spontaneous

    heatCold Hot body, requires work

    Third Law = entropy of pure crystalline substance atabsolute zero temperature is zero

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    Application Areas of Thermodynamics

    House-hold utensils appliances:Air-cond, heater, refrigerator

    humidifier, pressure cooker, water heater

    computer & TV

    Engines: Automotive, aircraft, rocket

    Plant/ Factory

    Refinery, power plants,nuclear power plant Powerplants

    The

    human

    body

    Air-condition

    ingsystems

    Airplanes

    Carradiators

    Refrigerationsystems

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    1.2 Dimensions and Units

    DimensionPrimary

    Secondary

    M - massL - length

    T - temperature

    t - time

    n - mole

    A - AmpereEg: Volume V

    velocity v

    energy E

    UnitsSI - International System- Commonly applied

    English System - also known as United States Customary

    System (USCS)

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    1.3 Closed and Open Systems

    Thermodynamic system (system) - quantity of matter or a region in

    space chosen for study.Surroundings - the mass or region outside the system

    Boundary - the real or imaginary surface that separates the system from

    its surrounding

    - is the contact surface shared by both the system & surroundings

    - has zero thickness & can either contain any mass nor occupy

    volume in space.

    - can be fixed or movable

    Boundary

    fixed

    movable

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    Types of system:

    (a) isolated - no heat/ mass transfer across boundary

    (b) closed(control mass) - only heat transferred(c) open system(control volume) - heat & mass

    transferred

    (b) (c)

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    1.4 Energy

    Forms of energy - thermal, mechanical, chemical, kinetic, potential,

    electrical, magnetic & nuclearE = total energy i.e sum of all energy in a system

    e = total energy = E (kJ/kg)

    mass m

    Forms of energy that make up the total energy of a system :

    Energy form

    macroscopic

    microscopic

    energy of a system as a wholewith respect to some outsidereference frames, e.g. KE, PE

    - related to molecular structure of asystem and the degree of molecularactivity- independent of outside referenceframes

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    Sum of all microscopic forms of energy = Internal Energy (U)

    Macroscopic forms of energy

    Therefore, E = U + KE + PE (kJ)

    Kinetic energy (KE)

    - result of motion relative to some

    reference frameKE = mv2/2 (kJ)

    where v = velocity of the system

    relative to some fixed

    reference frame (m/s)

    m = mass of an object (kg)

    Potential energy (PE)

    - due to elevation in a gravitational

    field

    PE = mgh (kJ)

    where g = gravitational acceleration,

    9.81 m/s2

    h = elevation of center of gravity of

    a system relative to somearbitrarily plane (m)

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    1.5 Internal Energy

    Internal energy - sum of all microscopic forms of energy of asystem

    related to - 1) molecular structure2) degree of molecular activity

    Latent heat - Internal energy associated to with the phase of asystem

    - phase -change process can occur without a change inthe chemical composition of a system

    I. EKE

    PE

    molecular translation

    molecular rotation

    electron translation

    molecular vibration

    electron spin

    nuclear spin

    a.k.asensible energy

    depend on thetemperature

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    1.6 Properties of a System

    Property - any characteristic of a system or any quantity thatdescribe a system

    Some familiar properties are P, T, V and m. But can be extended toinclude less familiar ones such as viscosity, thermal conductivity,thermal expansion coefficient and etc

    Density (mass per unit volume), (kg/m3) depends on T & P

    Specific gravity or relative density (ratio of the density of asubstance to the density of some standard substance at a specifiedtemperature) e.g. for water,

    Specific volume, (m3/kg)

    V

    m

    OH

    s

    2

    m

    V

    T P

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    Specific properties - extensive properties per unit mass

    E.g. specific volume (v = V/m) and specific total energy (e = E/m)

    Properties

    Intensive

    Extensive

    independent of the

    size/extent of the system

    dependent on the

    size/extent of the system

    T, P,

    age,

    colour

    m

    V

    total E

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    1.7 State & Equilibrium

    State a set of properties that describe the condition of a

    system at certain timeAt a given state, all the properties of a system have fixed values.If the value of one property changes, the state will change to adifferent one.

    Equilibrium state steady state/ state of balance

    & no change in time

    Thermal equilibrium T is the same throughout the system

    Mechanical equilibrium P is the same throughout the system

    Phase equilibrium m of each phase unchanged

    Chemical equilibrium chemical composition unchanged

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    Thermal equilibrium

    (uniform temperature)

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    1.8 Processes & Cycle

    Process any change that a system undergoes from one

    equilibrium state to another

    Path Series of states through which a systempasses during a process

    need to specify the initial & final states of the process, as well asthe path it follows, and the interactions with the surroundings.

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    1.9 Quasi-equilibrium/ Quasi-static

    When a process proceeds in such a manner that the system remains

    infinitesimally close to equilibrium state at all times.

    Sufficiently slow process that allows the system to adjust to itself

    internally so that properties in one part of the system do not change

    any faster than those at other parts.

    Slow compression

    (quasi-equilibrium)

    very fast compression

    (non-quasi equilibrium)

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    The prefix iso- is often used to designate a process for which aparticular property remains constant.

    Isothermal Process a process when T remains constant

    Isobaric P constant

    Isochoric/ Isometric specific volume vremains constant

    A system is said to have undergone a cycle if it returns to itsinitial state at the end of the process.

    For a cycle, the initial & final states are identical

    ProcessB

    ProcessA

    1

    2P

    V

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    1.10 Pressure

    P = = Unit = N/m2 or Pa

    Gas or liquid Pressure

    Solids Stress

    Common units

    1 bar = 105 Pa

    1 atm = 101,325 Pa = 1.01325 bars

    1 kgf/ cm2 = 0.9807 bar = 0.96788 atm

    English unit Ibf/in2 or psi

    Absolute pressure Actual pressure at at given position &

    measured relative to absolute vacuumGage pressure Difference between absolute pressure & local

    atmospheric pressure

    Vacuum pressure Difference between atmospheric pressure &absolute pressure

    Area

    Force

    A

    F

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    Absolute, gage & vacuum pressures are all +ve quantities &

    related to each other by:

    Pgage = Pabs - Patm (for pressure above Patm)

    Pvac = Patm - Pabs (for pressure below Patm)

    In thermo, absolute pressure is always used unless stated.

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    Example 1-1

    A vacuum gage connected to a chamber reads 5.8 psi at a

    location where the atmospheric pressure is 14.5 psi. Determine the

    absolute pressure in the chamber.

    Using Pvac = Patm - Pabs, So, Pabs = 14.5 - 5.8 = 8.7 psi

    Manometer

    Small to moderate pressure difference are measured by a manometerand a differential fluid column of height h corresponds to a pressuredifference between the system and the surrounding of themanometer.

    P g h kPa ( )

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    Other Pressure Measurement Device

    Bourdon Tube

    Modern pressure sensors:

    1) Pressure transducers

    2) Piezoelectric material

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    Example 1-2

    A vacuum gage connected to a tank reads 30 kPa at a location

    where the atmospheric pressure is 98 kPa. What is the absolute

    pressure in the tank?Solution:

    Pabs = Patm - Pgage= 98 kPa - 30 kPa

    = 68 kPa

    Example 1-3

    A pressure gage connected to a valve stern of a truck tire reads 240kPa at a location where the atmospheric pressure is 100 kPa. What isthe absolute pressure in the tire, in kPa and in psia?

    Solution:Pabs = Patm - Pgage= 100 kPa + 240 kPa

    = 340 kPa

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    The pressure in psia is

    Pabs = 340 kPa = 49.3 psia

    What is the gage pressure of the air in the tire, in psig?Pgage = Pabs - Patm

    = 49.3 psia - 14.7 psia

    = 34.6 psig

    Example 1-4Both a gage and a manometer are attached to a gas tank to measureits pressure. If the pressure gage reads 80 kPa, determine thedistance between the two fluid levels of the manometer if the fluidsis mercury whose density is 13,600 kg/m3.

    kPa

    psia

    3.101

    7.14

    hP

    g

    hkPa

    kg

    m

    m

    s

    N mkPa

    N

    kg m s

    m

    80

    13600 9 807

    10

    1

    0 6

    3 2

    3 3

    2.

    /

    /

    .

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    Temperature Measure of hotness and coldness

    Transfer of heat from higher to lower temp. until both bodies attain

    the same temp. At that point, heat transfer stops and the two bodieshave reached thermal equilibrium

    requirement: equality of temperature

    Zeroth Law of Thermodynamics:

    Two bodies are in thermal equilibrium when they have reached thesame temperature. If two bodies are in thermal equilibrium with athird body, they are also in thermal equilibrium with each other.

    Temperature scales: Celcius (C)

    Fahrenheit (F)

    Kelvin (K)

    Rankine (R)

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    Conversion:

    T(K) = T(C) + 273.15

    T(R) = T(F) + 459.67

    T K = (T2C +273.15) - (T1C + 273.15)

    = T2C - T1C= TC

    T R = TF

    T

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    Temperature Scale Comparison