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TRC2200: Thermo Fluids & Power Systems
LECTURE 10
Introduc)on & Basic Concepts of Thermodynamics
Lecturer: Alpha Agape Gopalai
• Basic concepts to form a sound foundation for the development of the principles of thermodynamics.
• Explain the basic concepts of thermodynamics such as system,
state, state postulate, equilibrium, process, and cycle.
• Review concepts of temperature, temperature scales, pressure,
and absolute and gage pressure.
• Energy • Introduce an intuitive systematic problem-solving technique.
Lecture Outline
• Many form of Energy
Energy
• In thermodynamic analysis, total energy of a system can be classified into two groups:
• Macroscopic forms of energy • Microscopic forms of energy
Energy
Energy: Macroscopic Macroscopic energy: Forms of energy that are possessed by a system with respect to an outside reference frame.
Kine)c Energy (KE)
Poten)al Energy (KE)
𝐾𝐸= 1/2 𝑚𝑉2 where : m = mass of a body (kg)
V = velocity of the body (m/s)
𝑃𝐸=𝑚𝑔𝑧 where : m = mass of a body (kg)
g = gravita)onal accelera)on (m/s2) z = eleva)on (m)
Energy: Microscopic • Microscopic energy: Forms of energy that are related to the molecular structure of a system and the degree of molecular ac)vity. They are independent of outside reference frames.
Sensible energy: Kine)c energy of the molecules.
Transla)onal energy Rota)onal kine)c energy
Vibra)onal kine)c energy
Spin energy
Sum of all microscopic forms of energy is referred as the internal energy of a system (U)
Energy: Microscopic • Latent energy: Internal energy associated with the phase of a system.
• Chemical energy: Internal energy associated with the atomic bonds in a molecule.
• Nuclear energy: Internal energy associated with the strong bonds within the nucleus of the atom.
Solid Liquid Gas
• We define the total energy in a system as:
• We can also represent total energy as specific energy (per unit mass)
Total Energy of a System
E =U +KE +PE =U +mV 2
2+mgz
E =me =m u+ ke+ pe( )
E =m(u+V2
2+ gz)
Where e = total energy of a system per unit mass (kJ/kg) ke = Kine)c energy per unit mass (kJ/kg)
pe = Poten)al energy per unit mass (kJ/kg) u = internal energy per unit mass (kJ/kg)
Total Energy of a System
Closed system Most closed systems remains sta)onary during a process à No change in their kine)c and poten)al energies
E =me =m u+ ke+ pe( )
• Open system Open system involves fluid flow for long periods of )me. It is commonly expressed in term of energy flow rate (𝐸 ) à incorpora)ng mass flow rate ( 𝑚 )
m = ρV = ρAcVavg
ρ = fluid density V = volume flow rate
Ac = Cross-‐sec1onal area of flow Vavg = the average flow velocity normal to Ac
• Energy can be contained or transferred
• In a closed system Energy can be transferred by • Heat • Work
• In a control volume Energy can be transferred by • Heat • Work • Mass
Total Energy of a System
Mechanical Energy Mechanical energy systems are designed to transport fluid from one loca)on to another at a specified flow rate, velocity and eleva)on difference.
Such systems may generate mechanical work in a turbine or it may consume mechanical work in a pump/ fan during this process.
We can analyze these systems by considering the mechanical forms of energy only and the fric)onal effect that cause the mechanical energy to be lost.
Mechanical Energy Mechanical energy: The form of energy that can be converted to mechanical work completely and directly by an ideal mechanical device such as an ideal turbine. Kinetic and potential energies: The familiar forms of mechanical energy.
• A pump transfers mechanical energy to a fluid by raising its pressure • A turbine extracts mechanical energy from a fluid by dropping its pressure
• Therefore, the pressure of a flowing fluid is also associated with mechanical energy
• Pressure on its own is not a form of energy
• Pressure ac)ng on a fluid through a distance produces work • Flow work , which can be calculated as
• Therefore
Mechanical Energy
Mechanical energy of a flowing fluid per unit mass
Mechanical Energy
Rate of mechanical energy of a flowing fluid
For a system with fluids flowing, we know that
Therefore,
Mechanical Energy
Mechanical Energy
• 16
Mechanical energy change of a fluid during incompressible flow per unit mass
Rate of mechanical energy change of a fluid during incompressible flow
Example
17
AssumpIon: Let’s assume wind flows steadily – at a constant speed of 8.5 m/s
Understanding: A site with a specified wind speed is considered. Wind energy per unit mass, for a specified mass, and for a given mass flow rate of air is to be determined.
Analysis: Wind flow (energy) is being converted into mechanical energy. The only harvestable form of energy of atmospheric air is kine)c energy, which is captured by the wind turbine.
Wind energy per unit mass 𝑒=𝑘𝑒= 𝑉↑2 /2 = 8.5↑2 /2 =𝟑𝟔.𝟏 𝑱/𝒌𝒈
Example
18
Wind energy for an air mass of 10kg 𝑒=𝑘𝑒= 𝑉↑2 /2 = 8.5↑2 /2 =36.1 𝐽/𝑘𝑔 𝑬=𝒎𝒆=𝟑𝟔𝟏 𝑱
Wind energy for a mass flow rate of 1154 kg/s 𝑒=𝑘𝑒= 𝑉↑2 /2 = 8.5↑2 /2 =36.1 𝐽/𝑘𝑔 𝑬 = 𝒎 𝒆=𝟒𝟏.𝟕 𝒌𝑾
19
3-‐3 ENERGY TRANSFER BY HEAT Heat: The form of energy that is transferred between two systems (or a system and its surroundings) by virtue of a temperature difference.
Energy is recognized as heat transfer only as it crosses the system boundary.
During an adiabatic process, a system
exchanges no heat with its surroundings.
Heat transfer per unit mass
Amount of heat transfer when heat transfer rate changes with time
Amount of heat transfer when heat transfer rate is constant
Energy Transfer by Heat • AdiabaIc process: A process during which there is no heat transfer
• It takes place when • The system is well insulated • System and surroundings are at the same temperature, thus there is no temperature difference for heat transfer
21
Energy Transfer by Heat Heat is transferred by three mechanisms: • Conduction: The transfer of energy from
the more energetic particles of a substance to the adjacent less energetic ones as a result of interaction between particles.
• Convection: The transfer of energy between a solid surface and the adjacent fluid that is in motion, and it involves the combined effects of conduction and fluid motion.
• Radiation: The transfer of energy due to the emission of electromagnetic waves (or photons).
22
Energy Transfer
Heat and work are direc)onal quan))es. • Heat transfer to a system and work done on a system are posiIve • Heat transfer from a system and work done by a system are negaIve
23
Energy Transfer by Work • Work: The energy transfer associated with a force acIng through a distance.
• If the energy crossing the boundary of a closed system is not heat, it must be work.
• Work per unit )me is called power and is denoted 𝑊 𝑊 = 𝑑𝑊/𝑑𝑡
24
Work done per unit mass
Heat vs. Work • Both are recognized at the boundaries of a
system as they cross the boundaries. That is, both heat and work are boundary phenomena.
• Systems possess energy, but not heat or
work. • Both are associated with a process, not a
state.
• Unlike properties, heat or work has no meaning at a state.
• Both are path functions (i.e., their magnitudes depend on the path followed during a process as well as the end states).
Checkpoint
26
The interior surfaces of the oven forms the system boundary. There will definitely be a rise of temperature in the oven. -‐ That means energy is being supplied to the system What causes this energy transfer? Heat or Work? What is crossing the boundaries? Heat or Work?
Various Forms of Work
𝑊↓𝑒 =∫𝑡↓1 ↑𝑡↓2 ▒𝑉𝐼𝑑𝑡 𝑊↓𝑒 =𝑉𝐼∆𝑡 Where 𝑊 ↓𝑒 = Electrical power (W)
We = Electrical work (kJ) ∆𝑡 = t2 – t1 = )me interval (s)
Electrical Work 𝑊 ↓𝑒 =𝑉𝐼
27
Various Forms of Work ShaR Work
Force acts through a distance s, 𝑠=2𝜋𝑟𝑛 Shag work Wsh: 𝑊↓𝑠ℎ =𝐹𝑠= 𝑇/𝑟 2𝜋𝑟𝑛=2𝜋𝑛𝑇 Where n = number of revolu)on
𝑇=𝐹𝑟
Power transmihed by the shag 𝑊 ↓𝑠ℎ :
𝑊 ↓𝑠ℎ =2𝜋𝑛 𝑇
Where 𝑛 = number of revolu)on per unit )me
28
Various Forms of Work Spring Work
Rela)onship between displacement x and force F of a spring is expressed as:
F = kx
Where k = spring constant (kN/m)
Work done by the spring, Wspring
𝑊↓𝑠𝑝𝑟𝑖𝑛𝑔 = 1/2 𝑘( 𝑥2↓↑2 − 𝑥1↓↑2 ) Where x1 = ini)al displacement of the spring (m)
x2 = final displacement of the spring (m)
29
Various Forms of Work
• The work transfer needed to raise a body is equal to the change in the potenIal energy of the body
• The work transfer needed to accelerate a body is equal to the change in the kineIc energy of the body.
• It plays important roles in: (Considering the fric1on and other energy losses)
• The design of elevators • The design of automo)ve and aircrag engine • Determina)on of hydroelectric power produced by a dam
Work Done to Raise or to Accelerate a Body
30
Example 2 Consider a 1200 kg car cruising steadily at 90 km/h. Now the car starts climbing a hill that is sloped 30o from the horizontal. If the velocity of the car is to remain constant during climbing. Determine the addi)onal power that must be delivered by the engine.
Analysis: The addi)onal power required is simply the work that needs to be done per unit )me to raise the eleva)on of the car, which is equal to the change in the poten)al energy of the car per unit )me
= mg Δz/ Δt = mg Vver)cal = 1200 kg x 9.81 m/s2 x 90 km/h x sin 30o = 147 kJ/s = 147 kW
W&
31
Example 3 Determine the average power required to accelerate a 900 kg from rest to velocity of 80 km/h in 20 s on a level road.
Analysis: The work needed to accelerate a body is simply the change in the kine)c energy of the body.
22 2 22 1
1 1 80000( ) 900 02 2 3600a
mW m V V kgs
⎡ ⎤⎛ ⎞= − = × × −⎢ ⎥⎜ ⎟⎝ ⎠⎣ ⎦
=222 kJ
The average power is determined from
22220
aaW kJWt s
= =Δ
& = 11.1 kW
32
Energy Transfer
Iden)fy heat and work interac)on in the following cases
ü No heat
ü No work
ü Heat input if potato is system
ü No work
ü No heat
ü Work input (electrical)
ü No work ü Heat transfer if
element is turn on.
33
Problem Solving Technique • Step 1: Problem Statement
• Determine the interac)on between system and its surrounding. • Determine whether it is a closed system, open system or an isolated system.
InteracIon with surrounding Mass exchange
No mass exchange
Energy exchange
No energy exchange X
Open sys. (Control volume)
Closed sys. (Control mass)
Isolated system
Problem Solving Technique
• Step 2: Schema)c • Draw a schema)c diagram of the system • Define your system boundary
Q is heat supplied to/leaving the system
Problem Solving Technique
• Step 3: Assump)ons and Approxima)ons • Is it a quasista)c or non-‐quasista)c equilibrium process? • Is it a steady flow process or transient flow process? • Is there any heat loss?
Problem Solving Technique • Step 4: Physical Laws
Determine physical laws that govern the system.
∑↑▒𝑭 =𝒎𝒂
Problem Solving Technique • Step 5: Proper)es
• Determine the proper)es of the system: extensive or intensive proper)es.
• Does it involve compressed liquid or saturated liquid, saturated vapor or superheated vapor?
Problem Solving Technique • Step 6: Calcula)ons • Step 7: Reasoning, Verifica)on, and Discussion
• Are the results prac)cally viable? • What are the implica)ons of the results to the problem?
• Y. A. Cengel, J. M. Cimbala, R. H. Turner, “Fundamentals of Thermal-‐fluid Sciences”, 4th ed. Chapter 2 & Chapter 3.
Reading Material
AVendance Code
41 TRC 2200: Thermo-‐Fluids & Power Systems