A Practical Approach to the Carnot Efficiency

Size: px
Start display at page:

Download "A Practical Approach to the Carnot Efficiency"

Transcription

1 Paper ID #9198 A Practical Approach to the Carnot Efficiency Dr. David C Zietlow, Bradley University Professor of Mechanical Engineering c American Society for Engineering Education, 2014 Page

2 Background Practical Approach to the Carnot Efficiency The Carnot cycle is a valuable tool to help students and practitioners understand the theoretical limits of heat engines, refrigeration cycles and heat pumps. Presented here is a practical approach to developing the Carnot efficiency for a heat engine and coefficient of performance for refrigeration and heat pump systems. This practical approach helps students connect actual hardware with the ideal cycle. The material presented here is designed for first semester thermodynamic students before they take a course in heat transfer. Although the course is open to all engineers the vast majority of the students are mechanical engineers. The prerequisite knowledge of the students is algebra and an introduction to conduction and convection heat transfer along with the corresponding constitutive equations. Providing students with an application is a significant aid to their understanding of theory. In one study the authors discovered 68 percent of second-year students tend to agree that having fun activities, interesting assignments, and applying the material to the real world make a course engaging. (1) Another study found that student participation in laboratory or demonstration exercises in conjunction with a lecture produces a more positive learning outcome. (2) Application and demonstration are two key tools of an educator and will be explained further in this paper so students will be able to comprehend the abstract ideas of irreversibility and Carnot efficiency. This paper ties the theoretical Carnot efficiency to the applications to which it is related. One of the more challenging concepts for students is the irreversibility of heat transfer through a finite temperature difference. It is easier to understand the irreversibility of other processes such as friction. To lead into the concept of irreversible heat transfer, a multi-sensory and multimedia demonstration is conducted. Easily understood irreversible processes in the production of tea are used; from the harvesting of the tea plant to the making of a hot cup of tea. This natural progression helps with the more abstract concept of what is necessary to restore the hot tea to its original condition once it cools. It is noted that as the temperature difference between the tea and the room increases it becomes more challenging (greater irreversibility) to restore the temperature of the tea to its original condition. Assuming the students have been exposed to the three basic modes of heat transfer, and the associated constitutive equations, it is possible to make the connection with the conductance form of the heat exchanger equation. At this point in their education, they may be able to understand a qualitative explanation of the conductance form (UA) of the heat exchanger equation. Qualitatively, the conductance represents the combination of Newton s Law of Cooling for the convective heat transfer through the boundary layers of the fluids and Fourier s Law for the conduction through the material used in the heat transfer surface. With the conductance form, the students are equipped to relate the size of the heat exchanger to the temperature difference between the two fluids. Since the Carnot Cycle is ideal, the irreversibility is zero. No irreversibility means the temperature difference driving the heat transfer is zero. For a finite rate of heat transfer, no temperature difference can only happen when the heat transfer surface area is infinite. Therefore, maximizing the efficiency (i.e. Carnot efficiency) of a thermal system is not a realistic objective function. This paper will take you through the process of how Page

3 to present this approach to students. It will also show you how much of this information students retain into the next semester. Irreversible Heat Transfer In thermodynamics, it is critical students understand the abstract terms, heat and irreversibility. The learning process is facilitated when concrete concepts are connected with more abstract concepts. It is useful to begin the discussion of irreversibility with concrete examples that most students comprehend. Therefore, it is recommended to lead students through the tea making process. Begin with cutting the green tea plant from its roots. Next, ask the students to consider the irreversible nature of this process. The plant cannot be reattached at this point; it has died. To make this a multi-sensory and multi-media presentation it is helpful to grow your own tea plants. Spearmint or peppermint is most effective because of the strong aroma produced when a leaf is rubbed between the fingers. The next irreversible step is to dry the plant. Here the moisture has left the leaves and cannot be returned to the plant cells. The color has changed from green to brown and cannot be restored. Dry some of the tea plants by hanging them in a dry place for a few weeks. The results will be an effective visual aid. After drying, comes separation of the leaves from the stems. (The use of a document camera will immensely aid the presentation of this process.) The leaves cannot be reattached without significant input from outside the system (e.g. a human with superglue). Even then, the dried leaves are not restored to their original condition. After the separation from the stems, the leaves are crushed into small pieces. Illustrate this under a document camera to amplify the futility of restoring the leaves to their original condition. Next, a tea bag emerges from the pocket of the instructor and is dropped into a clear glass mug where the diffusion process is easily observed. Note the color and flavor of the tea has left the tea leaves irreversibly. For the motivated teacher who would like to expand the multi-sensory experience to the students senses of smell and taste, a thermos of hot tea and disposable cups are a pleasant way to drive the point home. The irreversibility of absorbing the tea into the human body can be discussed as well. Now with the presentation of several concrete examples of irreversible processes, the more abstract concept of heat can be addressed as shown in Figure 1. T H T L Time (t) Figure 1. Cooling a Cup of Tea Page

4 The cup of tea begins with a highh initial temperature (T H ) and cools towards the ambient temperature (T L ) as the heat flows from the high temperature to the low temperature. The students are asked how this cup of tea can be restored to its original condition. Whether the answer is a microwave, electric heating element, or a flame, the students need to consider how the surroundings are affected. For the microwave and electric heating element the students need to understand the abstract concept of the heat engine (power plant) that is required to supply electrical power to the outlet to which the appliance is connected. T H Q H W net Boiler Pump Turbine Condenser T L Q L Figure 2. Schematic of a Heat Engine The heat engine, like a flame, requires the consumption of a fuel (e.g. gas, oil, coal or wood) which is highly irreversible. To restore the gas, oil or coal to its original state requires biomass and several months at high temperatures and pressures. Restoring the wood requires a seed, sun, soil (fertilized by the ashes) and decades of time. Taking students through these processes, Page

5 clearly and concretely, demonstrates the irreversibility of the heat transfer process. It should also be emphasized that the greater the temperature difference, the greater the irreversibility. Heat Exchangers Unfortunately, heat exchangers are not adequately addressed in most courses of thermodynamics. In most problems, heat transfer is either a given input or is a dependent variable where the conservation of energy is used to solve for this elusive quantity. In this section, a basic understanding of heat exchangers (see Figure 3) is presented. A triangle is used to represent one-side of a heat exchanger. The hypotenuse of the triangle represents the heat transfer surface area while the sides allow for the entering and exiting of the heat transfer fluid. T L Q T H Figure 3. Schematic of a Heat Exchanger Assuming the students have already been exposed to the three modes of heat transfer and their corresponding constitutive equations, the conductance form of the heat exchanger equation (Equation 1) is not difficult for them to grasp in a qualitative sense. For the ambitious instructor, an optional lecture on the development of this equation using Ohm s analogy and a mathematical relationship will give them a firmer understanding of the conductance equation. ( ) Q = UA T T H L (1) The rate of heat transfer,, equals the product of the conductance of the heat exchanger, UA, and the driving potential or the temperature difference between the high-tempera T, ) ature fluid ( ) and the low-temperature fluid ( T L. Qualitatively, the conductance represents a combination of convective heat transfer of the two fluids and conduction through the wall of the heat transfer H Page

6 surface area. For a given application, the key benefit of this equation is it establishes a relationship between the size of the heat exchanger (A) and the temperature difference between the two fluids. The higher the temperature difference the greater the irreversibility. The greater the irreversibility the lower the efficiency and the higher the operating costs for a cycle in a given application. Heat Engines The state points from the heat engine shown in Figure 2 are plotted in Figure 4 on pressure versus specific enthalpy coordinates. The first state point is the inlet to the pump. Each subsequent state-point is numbered sequentially at the inlet to the next component of the heat engine as you follow the working fluid through the cycle. For this particular application, the heat engine cycle is receiving heat from a high temperature thermal reservoir at 370 C and is rejecting heat to a low temperature thermal reservoir at 15 C. The condenser is sized to allow a condensing temperature of 35 C while the boiler is sized to allow a saturation temperature of 320 C Water T H = 370 C T sat,b =320 [C] P [kpa] T sat,c =35 [C] 10 0 T L = 15 C ,000 1,500 2,000 2,500 3,000 3,500 h [kj/kg] Figure 4: Property Plot for the Heat Engine Cycle Next, the definition of efficiency is applied to the heat engine cycle. This produces Equation 2. (2) Page

7 Here the desired result is the net power output from the turbine. The required input is the rate of heat transfer received by the boiler from the high temperature thermal reservoir. Since reversible heat transfer can be calculated with the conductance form of the heat transfer equation it would be useful to replace the net work output with equivalent heat transfer rates. To determine the equivalent rates apply the conservation of energy to the entire heat engine cycle. At steady-state conditions, the rate of change of energy stored within the heat engine cycle is zero, so the rate of energy in equals the rate of energy out. This is shown in Equation 3. (3) Solving for net power output and substituting into Equation 2 yields Equation 4. (4) This expression of efficiency works for all heat engine cycles, real and ideal. If the flow rate of one of the heat transfer fluids for each heat exchanger and the corresponding state-points at both the inlet and outlet of the heat exchanger were known for both the condenser and boiler then the actual efficiency could be determined. Next, the conductance equation will be applied to the two heat exchangers. For the boiler, focusing on the phase change region of the heat exchange and an high mass flow rate of combustion air, the conductance equation can be used to calculate the heat transfer rate as seen in Equation 5., (5) For a given application and set of components, the heat transfer rate is constant and known, along with the flow rates, as well as the heat exchanger material, which fixes U. The flame temperature will fix the temperature of the high temperature thermal reservoir (T H ). As the heat transfer surface area increases the saturation temperature of the water (T sat,b ) in the boiler approaches the temperature of the high temperature thermal reservoir. This decreases the irreversibility of the heat transfer to zero when the area reaches infinity. For the condenser, the conductance equation can be used to determine the heat transfer in the condensing regions of the heat exchanger, when the cooling water flow rate is high. Equation 6 is the result., (6) The same arguments that were used for the boiler can be used for the condenser to fix the heat transfer rate and U. Since the location of the heat engine is fixed for a given application, the temperature of the low temperature thermal reservoir (T L ) is fixed by temperature of the water in the lake, river or cooling tower. As the heat transfer surface area increases, the saturation temperature of the water in the condenser (T sat,c ) approaches the temperature of the low Page

8 temperature thermal reservoir. Similar to the boiler, this decreases the irreversibility of the heat transfer to zero when the area reaches infinity. For the ideal case, an argument is made using mathematical reasoning that the ratio of heat transfer rates is only a function of the ratio of the thermal reservoirs. This reasoning is currently presented in most traditional thermodynamic textbooks. Technically you would need to divide both the numerator and denominator of Equation 4 by the rate of heat transferred from the high temperature thermal reservoir to obtain a ratio of the heat transfer rates. This ratio can then be replaced by the ratio of temperatures for the thermal reservoirs. Practically though, for the Carnot Cycle, where the heat transfer surfaces are infinite, and the irreversibility of the cycle is zero the heat transfer rates can be replaced by the temperature of the corresponding thermal reservoir. This yields Equation 7. TH T ηi = T H L (7) Refrigeration Cycles The basic refrigeration cycle is composed of four primary components as shown in Figure 5. The compressor, condenser, expansion device and evaporator are the primary components. Since the evaporator transfers more heat than the work required to operate the compressor, a new term is necessary to replace the efficiency of this cycle. Therefore, instead of Carnot efficiency the term Carnot coefficient of performance is used to assess the performance of refrigeration and heat pump cycles. Q H Condenser W Q L Compressor Evaporator Figure 5. Schematic of the Refrigeration Cycle The state-points are plotted in Figure 6 on pressure versus specific enthalpy (P-h) coordinates. For this particular application, the refrigeration cycle is cooling a building wheree the indoor environment is being maintained at T L =20 C in a climate where the outdoor temperature T H is 40 C. The condenser is sized to allow a condensing saturation temperature (T sat t,c) of 45 C while the evaporator is sized to allow an evaporating saturation temperature (T sat t,e) of 12.5 C. Page

9 2 x 10 3 R134a Τc Isentropic s=.9 Isotherms 3 T sat,c =45 C 2s P [kpa] 10 3 T L =20 C T H =40 C 4 T sat,e =12.5 C 1 Τe 2 x Figure 6. Property plot of a refrigeration cycle h [kj/kg] Next the definition of Coefficient of Performance is applied to the refrigeration cycle. This produces Equation 8. (8) Here the desired result is the rate of heat transfer removed from the low temperature reservoir. The required input is the power into the compressor. Since reversible heat transfer can be determined with the conductance form of the heat transfer equation, it would be useful to replace the compressor work with equivalent heat transfer rates. Applying the conservation of energy to the refrigeration cycle will accomplish this relationship. At steady-state conditions the rate of change of energy stored within the refrigeration cycle is zero so the rate of energy in equals the rate of energy out. This is shown in Equation 9. (9) Solving for compressor power and substituting into Equation 8 yields Equation 10. Page

10 (10) Next, the conductance equation will be applied to the two heat exchangers. For the evaporator, the conductance equation yields Equation 11. The conductance equation assumes no superheat of the refrigerant at the outlet, and an high mass flow rate of air., (11) For a given application, the heat transfer rate is specified and constant. The flow rates are known and fixed as well as the heat exchanger material which fixes U. The thermostat setting will fix the temperature of the low temperature thermal reservoir. As the heat transfer surface area increases, the saturation temperature of the refrigerant in the evaporator approaches the temperature of the low temperature thermal reservoir. This decreases the irreversibility of the heat transfer to zero as the area approaches infinity. For the condenser, the conductance equation is used to determine the heat transfer in the condensing region alone. This assumes the refrigerant is a saturated vapor at the inlet and a saturated liquid at the outlet and the air flow rate is high. These assumptions are valid if the condenser is divided into three separate heat exchangers, one for de-superheating, one for condensing and one for sub-cooling the refrigerant. Equation 12 is the result of applying the conductance equation to the condensing region., (12) The same arguments can be used to fix the heat transfer rate and U. Since the location is fixed for a given application, the temperature of the high temperature thermal reservoir is fixed by the climate. As the heat transfer surface area increases, the saturation temperature of the refrigerant in the condenser approaches the temperature of the high temperature thermal reservoir. This decreases the irreversibility of the heat transfer to zero as the area approaches infinity. Replacing the heat transfer rates, with the temperature of the corresponding thermal reservoir, yields Equation 13. (13) Heat Pumps Heat pumps use the same cycle as the refrigeration system. The main difference is the desired result of the system is the heat rejected by the condenser rather than the heat removed by the evaporator. This affects the numerator of the COP as given in Equation 14. (14) Page

11 The application of the heat transfer equation to the heat exchangers is the same as the refrigeration cycle. In the ideal case, the heat transfer rates are replaced by the temperature of the corresponding thermal reservoir. (15) Conclusions The multi-media and multi-sensory demonstration of the irreversible processes in the production of tea is a excellent analogy to help students understand irreversible heat transfer. This practical approach to developing the Carnot Cycle was presented to first semester students of thermodynamics on October 22, They were tested, without advance warning, over four months later on February 25, On the test they were asked to derive the Carnot efficiency for a heat engine. Out of forty students 82% were able to apply the definition of efficiency to the cycle, and 75% successfully derived the expression for the Carnot efficiency as a function of the temperatures of the thermal reservoirs. This approach is an effective way for students to understand energy systems and determine the maximum possible performance of these systems. Instructors are encouraged to adopt this practical approach to Carnot efficiency. Expanding the coverage of heat exchangers from the one-sided presentation in traditional thermodynamics to the other side of the exchanger leads to two key concepts. First, it exposes the students to the conductance form of the heat transfer equation. Second, it allows a graphical representation of the irreversibility on the pressure-enthalpy diagram. The conductance equation not only helps students understand the development of the Carnot Cycle but also relates the tradeoffs necessary to optimize energy systems. First, they realize using the efficiency or COP as an objective function leads to unrealistic optimums as the heat exchangers grow to infinity. Second, the conductance form of the heat exchanger equation relates the variables associated with the initial (heat transfer surface area) with the operating costs which are affected by the irreversibilities in the cycle. The higher the irreversibilities the less efficient the cycle and the more energy required for a given application. References 1. Student and Faculty Perception of Engagement in Engineering. Heller, Rachelle S., Beil, Cheryl and Dam, Kim. 3, s.l. : Journal of Engineering Education, 2010, Vol. 99, pp Embedding Laboratory Experiences in Lectures. Morgan, James R., Barroso, Luciana R. and Simpson, Nancy. 4, s.l. : Advances in Engineering Education, 2009, Vol. 1, pp Page

12 Acknowledgements First, I would like to thank my wife, Dixie, Ph.D., for the added load in parenting she has taken. It has permitted me time to write. Next, I appreciate the academic freedom the chair of the Department of Mechanical Engineering, Dr. Desh Paul Mehta, has allowed me. This freedom gave me the opportunities to test these ideas in the crucible of the classroom. Last, I would like to thank my student, Jack Stein, who polished the figures for me so they were consistent in font and format. Page

Lecture 35: Vapor power systems, Rankine cycle

Lecture 35: Vapor power systems, Rankine cycle ME 00 Thermodynamics I Spring 015 Lecture 35: Vapor power systems, Rankine cycle Yong Li Shanghai Jiao Tong University Institute of Refrigeration and Cryogenics 800 Dong Chuan Road Shanghai, 0040, P. R.

More information

FINAL EXAM. ME 200 Thermodynamics I, Spring 2013 CIRCLE YOUR LECTURE BELOW:

FINAL EXAM. ME 200 Thermodynamics I, Spring 2013 CIRCLE YOUR LECTURE BELOW: ME 200 Thermodynamics I, Spring 2013 CIRCLE YOUR LECTURE BELOW: Div. 5 7:30 am Div. 2 10:30 am Div. 4 12:30 am Prof. Naik Prof. Braun Prof. Bae Div. 3 2:30 pm Div. 1 4:30 pm Div. 6 4:30 pm Prof. Chen Prof.

More information

CHAPTER 6 THE SECOND LAW OF THERMODYNAMICS

CHAPTER 6 THE SECOND LAW OF THERMODYNAMICS CHAPTER 6 THE SECOND LAW OF THERMODYNAMICS S. I. Abdel-Khalik (2014) 1 CHAPTER 6 -- The Second Law of Thermodynamics OUTCOME: Identify Valid (possible) Processes as those that satisfy both the first and

More information

ME 354 THERMODYNAMICS 2 MIDTERM EXAMINATION. Instructor: R. Culham. Name: Student ID Number: Instructions

ME 354 THERMODYNAMICS 2 MIDTERM EXAMINATION. Instructor: R. Culham. Name: Student ID Number: Instructions ME 354 THERMODYNAMICS 2 MIDTERM EXAMINATION February 14, 2011 5:30 pm - 7:30 pm Instructor: R. Culham Name: Student ID Number: Instructions 1. This is a 2 hour, closed-book examination. 2. Answer all questions

More information

Availability and Irreversibility

Availability and Irreversibility Availability and Irreversibility 1.0 Overview A critical application of thermodynamics is finding the maximum amount of work that can be extracted from a given energy resource. This calculation forms the

More information

Two mark questions and answers UNIT II SECOND LAW 1. Define Clausius statement. It is impossible for a self-acting machine working in a cyclic process, to transfer heat from a body at lower temperature

More information

7. Development of the 2nd Law

7. Development of the 2nd Law 7-1 7. Development of the 2nd Law 7.1 1st Law Limitations The 1 st Law describes energy accounting. Once we have a process (or string of processes) we can calculate the relevant energy interactions. The

More information

MAHALAKSHMI ENGINEERING COLLEGE

MAHALAKSHMI ENGINEERING COLLEGE MAHALAKSHMI ENGINEERING COLLEGE TIRUCHIRAPALLI 621 213. Department: Mechanical Subject Code: ME2202 Semester: III Subject Name: ENGG. THERMODYNAMICS UNIT-I Basic Concept and First Law 1. What do you understand

More information

Refrigeration. 05/04/2011 T.Al-Shemmeri 1

Refrigeration. 05/04/2011 T.Al-Shemmeri 1 Refrigeration is a process of controlled removal of heat from a substance to keep it at a temperature below the ambient condition, often below the freezing point of water (0 O C) 05/04/0 T.Al-Shemmeri

More information

CHAPTER 8 ENTROPY. Blank

CHAPTER 8 ENTROPY. Blank CHAPER 8 ENROPY Blank SONNAG/BORGNAKKE SUDY PROBLEM 8-8. A heat engine efficiency from the inequality of Clausius Consider an actual heat engine with efficiency of η working between reservoirs at and L.

More information

ES 202 Fluid and Thermal Systems

ES 202 Fluid and Thermal Systems ES Fluid and Thermal Systems Lecture : Power Cycles (/4/) Power cycle Road Map of Lecture use Rankine cycle as an example the ideal Rankine cycle representation on a T-s diagram divergence of constant

More information

Chapter 7. Entropy. by Asst.Prof. Dr.Woranee Paengjuntuek and Asst. Prof. Dr.Worarattana Pattaraprakorn

Chapter 7. Entropy. by Asst.Prof. Dr.Woranee Paengjuntuek and Asst. Prof. Dr.Worarattana Pattaraprakorn Chapter 7 Entropy by Asst.Prof. Dr.Woranee Paengjuntuek and Asst. Prof. Dr.Worarattana Pattaraprakorn Reference: Cengel, Yunus A. and Michael A. Boles, Thermodynamics: An Engineering Approach, 5th ed.,

More information

R13 SET - 1 '' ''' '' ' '''' Code No RT21033

R13 SET - 1 '' ''' '' ' '''' Code No RT21033 SET - 1 II B. Tech I Semester Supplementary Examinations, June - 2015 THERMODYNAMICS (Com. to ME, AE, AME) Time: 3 hours Max. Marks: 70 Note: 1. Question Paper consists of two parts (Part-A and Part-B)

More information

Course: MECH-341 Thermodynamics II Semester: Fall 2006

Course: MECH-341 Thermodynamics II Semester: Fall 2006 FINAL EXAM Date: Thursday, December 21, 2006, 9 am 12 am Examiner: Prof. E. Timofeev Associate Examiner: Prof. D. Frost READ CAREFULLY BEFORE YOU PROCEED: Course: MECH-341 Thermodynamics II Semester: Fall

More information

R13. II B. Tech I Semester Regular Examinations, Jan THERMODYNAMICS (Com. to ME, AE, AME) PART- A

R13. II B. Tech I Semester Regular Examinations, Jan THERMODYNAMICS (Com. to ME, AE, AME) PART- A SET - 1 II B. Tech I Semester Regular Examinations, Jan - 2015 THERMODYNAMICS (Com. to ME, AE, AME) Time: 3 hours Max. Marks: 70 Note 1. Question Paper consists of two parts (Part-A and Part-B) 2. Answer

More information

Unit Workbook 2 - Level 5 ENG U64 Thermofluids 2018 UniCourse Ltd. All Rights Reserved. Sample

Unit Workbook 2 - Level 5 ENG U64 Thermofluids 2018 UniCourse Ltd. All Rights Reserved. Sample Pearson BTEC Level 5 Higher Nationals in Engineering (RQF) Unit 64: Thermofluids Unit Workbook 2 in a series of 4 for this unit Learning Outcome 2 Vapour Power Cycles Page 1 of 26 2.1 Power Cycles Unit

More information

The exergy of asystemis the maximum useful work possible during a process that brings the system into equilibrium with aheat reservoir. (4.

The exergy of asystemis the maximum useful work possible during a process that brings the system into equilibrium with aheat reservoir. (4. Energy Equation Entropy equation in Chapter 4: control mass approach The second law of thermodynamics Availability (exergy) The exergy of asystemis the maximum useful work possible during a process that

More information

Spring_#7. Thermodynamics. Youngsuk Nam.

Spring_#7. Thermodynamics. Youngsuk Nam. Spring_#7 Thermodynamics Youngsuk Nam ysnam1@khu.ac.kr You can t connect the dots looking forward; you can only connect them looking backwards. So you have to trust that the dots will somehow connect in

More information

ECE309 THERMODYNAMICS & HEAT TRANSFER MIDTERM EXAMINATION. Instructor: R. Culham. Name: Student ID Number:

ECE309 THERMODYNAMICS & HEAT TRANSFER MIDTERM EXAMINATION. Instructor: R. Culham. Name: Student ID Number: ECE309 THERMODYNAMICS & HEAT TRANSFER MIDTERM EXAMINATION June 19, 2015 2:30 pm - 4:30 pm Instructor: R. Culham Name: Student ID Number: Instructions 1. This is a 2 hour, closed-book examination. 2. Permitted

More information

SECOND ENGINEER REG. III/2 APPLIED HEAT

SECOND ENGINEER REG. III/2 APPLIED HEAT SECOND ENGINEER REG. III/2 APPLIED HEAT LIST OF TOPICS A B C D E F G H I J K Pressure, Temperature, Energy Heat Transfer Internal Energy, Thermodynamic systems. First Law of Thermodynamics Gas Laws, Displacement

More information

(Refer Slide Time: 00:00:43 min) Welcome back in the last few lectures we discussed compression refrigeration systems.

(Refer Slide Time: 00:00:43 min) Welcome back in the last few lectures we discussed compression refrigeration systems. Refrigeration and Air Conditioning Prof. M. Ramgopal Department of Mechanical Engineering Indian Institute of Technology, Kharagpur Lecture No. # 14 Vapour Absorption Refrigeration Systems (Refer Slide

More information

Lecture 44: Review Thermodynamics I

Lecture 44: Review Thermodynamics I ME 00 Thermodynamics I Lecture 44: Review Thermodynamics I Yong Li Shanghai Jiao Tong University Institute of Refrigeration and Cryogenics 800 Dong Chuan Road Shanghai, 0040, P. R. China Email : liyo@sjtu.edu.cn

More information

ME6301- ENGINEERING THERMODYNAMICS UNIT I BASIC CONCEPT AND FIRST LAW PART-A

ME6301- ENGINEERING THERMODYNAMICS UNIT I BASIC CONCEPT AND FIRST LAW PART-A ME6301- ENGINEERING THERMODYNAMICS UNIT I BASIC CONCEPT AND FIRST LAW PART-A 1. What is meant by thermodynamics system? (A/M 2006) Thermodynamics system is defined as any space or matter or group of matter

More information

SECOND LAW OF THERMODYNAMICS

SECOND LAW OF THERMODYNAMICS SECOND LAW OF THERMODYNAMICS 2 ND Law of Thermodynamics Puts a limitation on the conversion of some forms of energy Determines the scope of an energy conversion and if an energy conversion is possible

More information

UBMCC11 - THERMODYNAMICS. B.E (Marine Engineering) B 16 BASIC CONCEPTS AND FIRST LAW PART- A

UBMCC11 - THERMODYNAMICS. B.E (Marine Engineering) B 16 BASIC CONCEPTS AND FIRST LAW PART- A UBMCC11 - THERMODYNAMICS B.E (Marine Engineering) B 16 UNIT I BASIC CONCEPTS AND FIRST LAW PART- A 1. What do you understand by pure substance? 2. Define thermodynamic system. 3. Name the different types

More information

Engineering Thermodynamics. Chapter 5. The Second Law of Thermodynamics

Engineering Thermodynamics. Chapter 5. The Second Law of Thermodynamics 5.1 Introduction Chapter 5 The Second aw of Thermodynamics The second law of thermodynamics states that processes occur in a certain direction, not in just any direction. Physical processes in nature can

More information

Basic Thermodynamics Prof. S K Som Department of Mechanical Engineering Indian Institute of Technology, Kharagpur. Lecture - 21 Vapors Power Cycle-II

Basic Thermodynamics Prof. S K Som Department of Mechanical Engineering Indian Institute of Technology, Kharagpur. Lecture - 21 Vapors Power Cycle-II Basic Thermodynamics Prof. S K Som Department of Mechanical Engineering Indian Institute of Technology, Kharagpur Lecture - 21 Vapors Power Cycle-II Good morning to all of you. Today, we will be continuing

More information

ME 200 Final Exam December 14, :00 a.m. to 10:00 a.m.

ME 200 Final Exam December 14, :00 a.m. to 10:00 a.m. CIRCLE YOUR LECTURE BELOW: First Name Last Name 7:30 a.m. 8:30 a.m. 10:30 a.m. 11:30 a.m. Boregowda Boregowda Braun Bae 2:30 p.m. 3:30 p.m. 4:30 p.m. Meyer Naik Hess ME 200 Final Exam December 14, 2015

More information

Basic Thermodynamics Prof. S.K Som Department of Mechanical Engineering Indian Institute of Technology, Kharagpur

Basic Thermodynamics Prof. S.K Som Department of Mechanical Engineering Indian Institute of Technology, Kharagpur Basic Thermodynamics Prof. S.K Som Department of Mechanical Engineering Indian Institute of Technology, Kharagpur Lecture - 17 Properties of Pure Substances-I Good morning to all of you. We were discussing

More information

1. INTRODUCTION TO REFRIGERATION AND AIR CONDITION

1. INTRODUCTION TO REFRIGERATION AND AIR CONDITION CHAPTER ONE 1. INTRODUCTION TO REFRIGERATION AND AIR CONDITION Refrigeration may be defined as the process of reducing and maintaining a temperature of a space or material below that of the surroundings.

More information

Thermodynamics II. Week 9

Thermodynamics II. Week 9 hermodynamics II Week 9 Example Oxygen gas in a piston cylinder at 300K, 00 kpa with volume o. m 3 is compressed in a reversible adiabatic process to a final temperature of 700K. Find the final pressure

More information

Lecture 38: Vapor-compression refrigeration systems

Lecture 38: Vapor-compression refrigeration systems ME 200 Termodynamics I Lecture 38: Vapor-compression refrigeration systems Yong Li Sangai Jiao Tong University Institute of Refrigeration and Cryogenics 800 Dong Cuan Road Sangai, 200240, P. R. Cina Email

More information

Readings for this homework assignment and upcoming lectures

Readings for this homework assignment and upcoming lectures Homework #3 (group) Tuesday, February 13 by 4:00 pm 5290 exercises (individual) Thursday, February 15 by 4:00 pm extra credit (individual) Thursday, February 15 by 4:00 pm Readings for this homework assignment

More information

ME Thermodynamics I. Lecture Notes and Example Problems

ME Thermodynamics I. Lecture Notes and Example Problems ME 227.3 Thermodynamics I Lecture Notes and Example Problems James D. Bugg September 2018 Department of Mechanical Engineering Introduction Part I: Lecture Notes This part contains handout versions of

More information

CHAPTER 7 ENTROPY. Copyright Hany A. Al-Ansary and S. I. Abdel-Khalik (2014) 1

CHAPTER 7 ENTROPY. Copyright Hany A. Al-Ansary and S. I. Abdel-Khalik (2014) 1 CHAPTER 7 ENTROPY S. I. Abdel-Khalik (2014) 1 ENTROPY The Clausius Inequality The Clausius inequality states that for for all cycles, reversible or irreversible, engines or refrigerators: For internally-reversible

More information

Chapter 5. Mass and Energy Analysis of Control Volumes. by Asst. Prof. Dr.Woranee Paengjuntuek and Asst. Prof. Dr.Worarattana Pattaraprakorn

Chapter 5. Mass and Energy Analysis of Control Volumes. by Asst. Prof. Dr.Woranee Paengjuntuek and Asst. Prof. Dr.Worarattana Pattaraprakorn Chapter 5 Mass and Energy Analysis of Control Volumes by Asst. Prof. Dr.Woranee Paengjuntuek and Asst. Prof. Dr.Worarattana Pattaraprakorn Reference: Cengel, Yunus A. and Michael A. Boles, Thermodynamics:

More information

Chapter 19. Heat Engines

Chapter 19. Heat Engines Chapter 19 Heat Engines QuickCheck 19.11 The efficiency of this Carnot heat engine is A. Less than 0.5. B. 0.5. C. Between 0.5 and 1.0. D. 2.0. E. Can t say without knowing Q H. 2013 Pearson Education,

More information

w = -nrt hot ln(v 2 /V 1 ) nrt cold ln(v 1 /V 2 )[sincev/v 4 3 = V 1 /V 2 ]

w = -nrt hot ln(v 2 /V 1 ) nrt cold ln(v 1 /V 2 )[sincev/v 4 3 = V 1 /V 2 ] Chemistry 433 Lecture 9 Entropy and the Second Law NC State University Spontaneity of Chemical Reactions One might be tempted based on the results of thermochemistry to predict that all exothermic reactions

More information

Thermodynamic Analysis of the Effect of Generator Temperature on the Performance of a Single-Effect Absorption Refrigeration Cycle

Thermodynamic Analysis of the Effect of Generator Temperature on the Performance of a Single-Effect Absorption Refrigeration Cycle Thermodynamic Analysis of the Effect of Generator Temperature on the Performance of a Single-Effect Absorption Refrigeration Cycle Abstract Debendra Nath Sarkar 1, Dipankar Narayan Basu 2 1 UG 4 th Year

More information

5/6/ :41 PM. Chapter 6. Using Entropy. Dr. Mohammad Abuhaiba, PE

5/6/ :41 PM. Chapter 6. Using Entropy. Dr. Mohammad Abuhaiba, PE Chapter 6 Using Entropy 1 2 Chapter Objective Means are introduced for analyzing systems from the 2 nd law perspective as they undergo processes that are not necessarily cycles. Objective: introduce entropy

More information

ME 022: Thermodynamics

ME 022: Thermodynamics ME 022: Thermodynamics General Information: Term: 2019 Summer Session Instructor: Staff Language of Instruction: English Classroom: TBA Office Hours: TBA Class Sessions Per Week: 5 Total Weeks: 5 Total

More information

University of Engineering & Technology Lahore. (KSK Campus)

University of Engineering & Technology Lahore. (KSK Campus) Course File Session-2015 Semester: Fall 2016 MT-24: Thermodynamics for Technologists Department of Mechanical Engineering University of Engineering & Technology Lahore. (KSK Campus) Course File Contents

More information

ME 2322 Thermodynamics I PRE-LECTURE Lesson 23 Complete the items below Name:

ME 2322 Thermodynamics I PRE-LECTURE Lesson 23 Complete the items below Name: Lesson 23 1. (10 pt) Write the equation for the thermal efficiency of a Carnot heat engine below: 1 L H 2. (10 pt) Can the thermal efficiency of an actual engine ever exceed that of an equivalent Carnot

More information

THERMODYNAMICS SSC-JE STAFF SELECTION COMMISSION MECHANICAL ENGINEERING STUDY MATERIAL THERMODYNAMICS THERMODYNAMICS THERMODYNAMICS

THERMODYNAMICS SSC-JE STAFF SELECTION COMMISSION MECHANICAL ENGINEERING STUDY MATERIAL THERMODYNAMICS THERMODYNAMICS THERMODYNAMICS 1 SSC-JE STAFF SELECTION COMMISSION MECHANICAL ENGINEERING STUDY MATERIAL 2 Syllabus: Thermal Engineering (Thermodynamics) Properties of Pure Substances : p-v & P-T diagrams of pure substance like H 2

More information

Existing Resources: Supplemental/reference for students with thermodynamics background and interests:

Existing Resources: Supplemental/reference for students with thermodynamics background and interests: Existing Resources: Masters, G. (1991) Introduction to Environmental Engineering and Science (Prentice Hall: NJ), pages 15 29. [ Masters_1991_Energy.pdf] Supplemental/reference for students with thermodynamics

More information

Chapter 19. Heat Engines

Chapter 19. Heat Engines Chapter 19 Heat Engines Thermo Processes Eint = Q+ W Adiabatic No heat exchanged Q = 0 and E int = W Isobaric Constant pressure W = P (V f V i ) and E int = Q + W Isochoric Constant Volume W = 0 and E

More information

Fundamentals of Heat Transfer (Basic Concepts)

Fundamentals of Heat Transfer (Basic Concepts) Fundamentals of Heat Transfer (Basic Concepts) 1 Topics to be covered History Thermodynamics Heat transfer Thermodynamics versus Heat Transfer Areas and Applications of Heat Transfer Heat Transfer problems

More information

Thermodynamics Lecture Series

Thermodynamics Lecture Series Thermodynamics Lecture Series Second Law uality of Energy Applied Sciences Education Research Group (ASERG) Faculty of Applied Sciences Universiti Teknologi MARA email: drjjlanita@hotmail.com http://www.uitm.edu.my/faculties/fsg/drjj.html

More information

Chapter 5. Mass and Energy Analysis of Control Volumes

Chapter 5. Mass and Energy Analysis of Control Volumes Chapter 5 Mass and Energy Analysis of Control Volumes Conservation Principles for Control volumes The conservation of mass and the conservation of energy principles for open systems (or control volumes)

More information

+ m B1 = 1. u A1. u B1. - m B1 = V A. /v A = , u B1 + V B. = 5.5 kg => = V tot. Table B.1.

+ m B1 = 1. u A1. u B1. - m B1 = V A. /v A = , u B1 + V B. = 5.5 kg => = V tot. Table B.1. 5.6 A rigid tank is divided into two rooms by a membrane, both containing water, shown in Fig. P5.6. Room A is at 200 kpa, v = 0.5 m3/kg, VA = m3, and room B contains 3.5 kg at 0.5 MPa, 400 C. The membrane

More information

BME-A PREVIOUS YEAR QUESTIONS

BME-A PREVIOUS YEAR QUESTIONS BME-A PREVIOUS YEAR QUESTIONS CREDITS CHANGE ACCHA HAI TEAM UNIT-1 Introduction: Introduction to Thermodynamics, Concepts of systems, control volume, state, properties, equilibrium, quasi-static process,

More information

International Academy Invitational Tournament Keep the Heat Test Team Name. Team Number. Predicted Water Temp C

International Academy Invitational Tournament Keep the Heat Test Team Name. Team Number. Predicted Water Temp C International Academy Invitational Tournament Keep the Heat Test 2-4-2012 Team Name Team Number Predicted Water Temp C Circle the all of the correct answer to the below questions. One or more of the answers

More information

Engineering Thermodynamics. Chapter 6. Entropy: a measure of Disorder 6.1 Introduction

Engineering Thermodynamics. Chapter 6. Entropy: a measure of Disorder 6.1 Introduction Engineering hermodynamics AAi Chapter 6 Entropy: a measure of Disorder 6. Introduction he second law of thermodynamics leads to the definition of a new property called entropy, a quantitative measure of

More information

Unit D-2: List of Subjects

Unit D-2: List of Subjects ES312 Energy Transfer Fundamentals Unit D: The Second Law of Thermodynamics ROAD MAP... D-1: From First to Second Law D-2: Second Law of Thermodynamics Unit D-2: List of Subjects Second Law of Thermodynamics

More information

MAE 320 HW 7B. 1e. For an isolated system, please circle the parameter which will change with time. (a) Total energy;

MAE 320 HW 7B. 1e. For an isolated system, please circle the parameter which will change with time. (a) Total energy; MAE 320 HW 7B his comprehensive homework is due Monday, December 5 th, 206. Each problem is worth the points indicated. Copying of the solution from another is not acceptable. Multi-choice, multi-answer

More information

first law of ThermodyNamics

first law of ThermodyNamics first law of ThermodyNamics First law of thermodynamics - Principle of conservation of energy - Energy can be neither created nor destroyed Basic statement When any closed system is taken through a cycle,

More information

SEM-2017(03HI MECHANICAL ENGINEERING. Paper II. Please read each of the following instructions carefully before attempting questions.

SEM-2017(03HI MECHANICAL ENGINEERING. Paper II. Please read each of the following instructions carefully before attempting questions. We RoU No. 700095 Candidate should write his/her Roll No. here. Total No. of Questions : 7 No. of Printed Pages : 7 SEM-2017(03HI MECHANICAL ENGINEERING Paper II Time ; 3 Hours ] [ Total Marks : 0 Instructions

More information

Chapter 1 Introduction and Basic Concepts

Chapter 1 Introduction and Basic Concepts Chapter 1 Introduction and Basic Concepts 1-1 Thermodynamics and Energy Application Areas of Thermodynamics 1-2 Importance of Dimensions and Units Some SI and English Units Dimensional Homogeneity Unity

More information

THE METHOD OF THE WORKING FLUID SELECTION FOR ORGANIC RANKINE CYCLE (ORC) SYSTEM WITH VOLUMETRIC EXPANDER. * Corresponding Author ABSTRACT

THE METHOD OF THE WORKING FLUID SELECTION FOR ORGANIC RANKINE CYCLE (ORC) SYSTEM WITH VOLUMETRIC EXPANDER. * Corresponding Author ABSTRACT Paper ID: 79, Page 1 THE METHOD OF THE WORKING FLUID SELECTION FOR ORGANIC RANKINE CYCLE (ORC) SYSTEM WITH VOLUMETRIC EXPANDER Piotr Kolasiński* 1 1 Wrocław University of Technology, Department of Thermodynamics,

More information

CHAPTER INTRODUCTION AND BASIC PRINCIPLES. (Tutorial). Determine if the following properties of the system are intensive or extensive properties: Property Intensive Extensive Volume Density Conductivity

More information

This follows from the Clausius inequality as a consequence of the second law of thermodynamics. Therefore. (for reversible process only) (22.

This follows from the Clausius inequality as a consequence of the second law of thermodynamics. Therefore. (for reversible process only) (22. Entropy Clausius inequality can be used to analyze the cyclic process in a quantitative manner. The second law became a law of wider applicability when Clausius introduced the property called entropy.

More information

2012 Thermodynamics Division C

2012 Thermodynamics Division C Team: Team Number: Team Member Names: 1. 2. Instructions: Answer all questions on the test paper. If you need more room, you may attach extra paper. The test is worth a total of 50 points. Show all work

More information

Spring_#8. Thermodynamics. Youngsuk Nam

Spring_#8. Thermodynamics. Youngsuk Nam Spring_#8 Thermodynamics Youngsuk Nam ysnam1@khu.ac.krac kr Ch.7: Entropy Apply the second law of thermodynamics to processes. Define a new property called entropy to quantify the secondlaw effects. Establish

More information

Principles of Solar Thermal Conversion

Principles of Solar Thermal Conversion Principles of Solar Thermal Conversion Conversion to Work Heat from a solar collector may be used to drive a heat engine operating in a cycle to produce work. A heat engine may be used for such applications

More information

An introduction to thermodynamics applied to Organic Rankine Cycles

An introduction to thermodynamics applied to Organic Rankine Cycles An introduction to thermodynamics applied to Organic Rankine Cycles By : Sylvain Quoilin PhD Student at the University of Liège November 2008 1 Definition of a few thermodynamic variables 1.1 Main thermodynamics

More information

Classification following properties of the system in Intensive and Extensive

Classification following properties of the system in Intensive and Extensive Unit I Classification following properties of the system in Intensive and Extensive Extensive : mass, weight, volume, potential energy, Kinetic energy, Internal energy, entropy, exergy, energy, magnetization

More information

CHAPTER 5 MASS AND ENERGY ANALYSIS OF CONTROL VOLUMES

CHAPTER 5 MASS AND ENERGY ANALYSIS OF CONTROL VOLUMES Thermodynamics: An Engineering Approach 8th Edition in SI Units Yunus A. Çengel, Michael A. Boles McGraw-Hill, 2015 CHAPTER 5 MASS AND ENERGY ANALYSIS OF CONTROL VOLUMES Lecture slides by Dr. Fawzi Elfghi

More information

THERMODYNAMICS CONCEPTUAL PROBLEMS

THERMODYNAMICS CONCEPTUAL PROBLEMS THERMODYNAMICS CONCEPTUAL PROBLEMS Q-01 Is the heat supplied to a system always equal to the increases in its internal energy? Ans Acc. to first law of thermo- dynamics If heat is supplied in such a manner

More information

(1)5. Which of the following equations is always valid for a fixed mass system undergoing an irreversible or reversible process:

(1)5. Which of the following equations is always valid for a fixed mass system undergoing an irreversible or reversible process: Last Name First Name ME 300 Engineering Thermodynamics Exam #2 Spring 2008 March 28, 2008 Form A Note : (i) (ii) (iii) (iv) Closed book, closed notes; one 8.5 x 11 sheet allowed. 60 points total; 60 minutes;

More information

ME Thermodynamics I

ME Thermodynamics I Homework - Week 01 HW-01 (25 points) Given: 5 Schematic of the solar cell/solar panel Find: 5 Identify the system and the heat/work interactions associated with it. Show the direction of the interactions.

More information

II/IV B.Tech (Regular) DEGREE EXAMINATION. (1X12 = 12 Marks) Answer ONE question from each unit.

II/IV B.Tech (Regular) DEGREE EXAMINATION. (1X12 = 12 Marks) Answer ONE question from each unit. Page 1 of 8 Hall Ticket Number: 14CH 404 II/IV B.Tech (Regular) DEGREE EXAMINATION June, 2016 Chemical Engineering Fourth Semester Engineering Thermodynamics Time: Three Hours Maximum : 60 Marks Answer

More information

MAE 11. Homework 8: Solutions 11/30/2018

MAE 11. Homework 8: Solutions 11/30/2018 MAE 11 Homework 8: Solutions 11/30/2018 MAE 11 Fall 2018 HW #8 Due: Friday, November 30 (beginning of class at 12:00p) Requirements:: Include T s diagram for all cycles. Also include p v diagrams for Ch

More information

Thermodynamics is the Science of Energy and Entropy

Thermodynamics is the Science of Energy and Entropy Definition of Thermodynamics: Thermodynamics is the Science of Energy and Entropy - Some definitions. - The zeroth law. - Properties of pure substances. - Ideal gas law. - Entropy and the second law. Some

More information

ME 200 Exam 2 October 22, :30 p.m. to 7:30 p.m.

ME 200 Exam 2 October 22, :30 p.m. to 7:30 p.m. CIRCLE YOUR LECTURE BELOW: First Name Solution Last Name 7:0 a.m. 8:0 a.m. 10:0 a.m. 11:0 a.m. Boregowda Boregowda Braun Bae :0 p.m. :0 p.m. 4:0 p.m. Meyer Naik Hess ME 00 Exam October, 015 6:0 p.m. to

More information

Equivalence of Kelvin-Planck and Clausius statements

Equivalence of Kelvin-Planck and Clausius statements Equivalence of Kelvin-Planck and Clausius statements Violation of Clausius statement Violation of Kelvin-Planck statement Violation of Kelvin-Planck statement Violation of Clausius statement Violation

More information

Chapter 7. Entropy: A Measure of Disorder

Chapter 7. Entropy: A Measure of Disorder Chapter 7 Entropy: A Measure of Disorder Entropy and the Clausius Inequality The second law of thermodynamics leads to the definition of a new property called entropy, a quantitative measure of microscopic

More information

Section A 01. (12 M) (s 2 s 3 ) = 313 s 2 = s 1, h 3 = h 4 (s 1 s 3 ) = kj/kgk. = kj/kgk. 313 (s 3 s 4f ) = ln

Section A 01. (12 M) (s 2 s 3 ) = 313 s 2 = s 1, h 3 = h 4 (s 1 s 3 ) = kj/kgk. = kj/kgk. 313 (s 3 s 4f ) = ln 0. (a) Sol: Section A A refrigerator macine uses R- as te working fluid. Te temperature of R- in te evaporator coil is 5C, and te gas leaves te compressor as dry saturated at a temperature of 40C. Te mean

More information

Physics Course Syllabus CHS Science Department

Physics Course Syllabus CHS Science Department 1 Physics Course Syllabus CHS Science Department Contact Information: Parents may contact me by phone, email or visiting the school. Teacher: Mr. Joshua Queen Email Address: joshua.queen@ccsd.us or josh.queen@students.ccsd.us

More information

ME 201 Thermodynamics

ME 201 Thermodynamics ME 0 Thermodynamics Solutions First Law Practice Problems. Consider a balloon that has been blown up inside a building and has been allowed to come to equilibrium with the inside temperature of 5 C and

More information

Jet Aircraft Propulsion Prof. Bhaskar Roy Prof. A.M. Pradeep Department of Aerospace Engineering Indian Institute of Technology, Bombay

Jet Aircraft Propulsion Prof. Bhaskar Roy Prof. A.M. Pradeep Department of Aerospace Engineering Indian Institute of Technology, Bombay Jet Aircraft Propulsion Prof. Bhaskar Roy Prof. A.M. Pradeep Department of Aerospace Engineering Indian Institute of Technology, Bombay Module No. # 01 Lecture No. # 06 Ideal and Real Brayton Cycles Hello

More information

ME 200 Thermodynamics 1 Fall 2016 Final Exam

ME 200 Thermodynamics 1 Fall 2016 Final Exam Last Name: First Name: Thermo no. ME 200 Thermodynamics 1 Fall 2016 Final Exam Circle your instructor s last name Ardekani Bae Fisher olloway Jackson Meyer Sojka INSTRUCTIONS This is a closed book and

More information

Chapter 7. Dr Ali Jawarneh. Department of Mechanical Engineering Hashemite University

Chapter 7. Dr Ali Jawarneh. Department of Mechanical Engineering Hashemite University Chapter 7 ENTROPY Dr Ali Jawarneh Department of Mechanical Engineering Hashemite University Objectives Apply the second law of thermodynamics to processes. Define a new property called entropy to quantify

More information

King Fahd University of Petroleum & Minerals

King Fahd University of Petroleum & Minerals King Fahd University of Petroleum & Minerals Mechanical Engineering Thermodynamics ME 04 BY Dr. Haitham Bahaidarah My Office Office Hours: :00 0:00 am SMW 03:00 04:00 pm UT Location: Building Room # 5.4

More information

THERMODYNAMICS (Date of document: 8 th March 2016)

THERMODYNAMICS (Date of document: 8 th March 2016) THERMODYNAMICS (Date of document: 8 th March 2016) Course Code : MEHD214 Course Status : Core Level : Diploma Semester Taught : 3 Credit : 4 Pre-requisites : None Assessments : Computerized homework 20

More information

EXAM # 1 ME 300 SP2017

EXAM # 1 ME 300 SP2017 CIRCLE YOUR LECTURE BELOW: 8:3 am :3 am 3:3 pm Prof. Lucht Prof. Chen Prof. Goldenstein EXAM # ME 3 SP7 INSTRUCTIONS. Please place all your electronics, including but not limited to cell phones, computers,

More information

Hours / 100 Marks Seat No.

Hours / 100 Marks Seat No. 17410 15116 3 Hours / 100 Seat No. Instructions (1) All Questions are Compulsory. (2) Illustrate your answers with neat sketches wherever necessary. (3) Figures to the right indicate full marks. (4) Assume

More information

Thermal Energy Final Exam Fall 2002

Thermal Energy Final Exam Fall 2002 16.050 Thermal Energy Final Exam Fall 2002 Do all eight problems. All problems count the same. 1. A system undergoes a reversible cycle while exchanging heat with three thermal reservoirs, as shown below.

More information

FUNDAMENTALS OF THERMODYNAMICS

FUNDAMENTALS OF THERMODYNAMICS FUNDAMENTALS OF THERMODYNAMICS SEVENTH EDITION CLAUS BORGNAKKE RICHARD E. SONNTAG University of Michigan John Wiley & Sons, Inc. PUBLISHER ASSOCIATE PUBLISHER ACQUISITIONS EDITOR SENIOR PRODUCTION EDITOR

More information

MATHEMATICAL MODEL OF A VAPOUR ABSORPTION REFRIGERATION UNIT

MATHEMATICAL MODEL OF A VAPOUR ABSORPTION REFRIGERATION UNIT ISSN 1726-4529 Int j simul model 9 (2010) 2, 86-97 Original scientific paper MATHEMATICAL MODEL OF A VAPOUR ABSORPTION REFRIGERATION UNIT Micallef, D. & Micallef, C. University of Malta, Department of

More information

ME 2322 Thermodynamics I PRE-LECTURE Lesson 23 Complete the items below Name:

ME 2322 Thermodynamics I PRE-LECTURE Lesson 23 Complete the items below Name: Lesson 23 1. (10 pt) Write the equation for the thermal efficiency of a Carnot heat engine below: T η = T 1 L H 2. (10 pt) Can the thermal efficiency of an actual engine ever exceed that of an equivalent

More information

wb Thermodynamics 2 Lecture 9 Energy Conversion Systems

wb Thermodynamics 2 Lecture 9 Energy Conversion Systems wb1224 - Thermodynamics 2 Lecture 9 Energy Conversion Systems Piero Colonna, Lecturer Prepared with the help of Teus van der Stelt 8-12-2010 Delft University of Technology Challenge the future Content

More information

Ttions, and its relation to states of matter. This chapter covers the

Ttions, and its relation to states of matter. This chapter covers the Related Commercial Resources CHAPTER 1 THERMODYNAMICS AND REFRIGERATION CYCLES THERMODYNAMICS... 1.1 First Law of Thermodynamics... 1.2 Second Law of Thermodynamics... 1.2 Thermodynamic Analysis of Refrigeration

More information

THE FIRST LAW APPLIED TO STEADY FLOW PROCESSES

THE FIRST LAW APPLIED TO STEADY FLOW PROCESSES Chapter 10 THE FIRST LAW APPLIED TO STEADY FLOW PROCESSES It is not the sun to overtake the moon, nor doth the night outstrip theday.theyfloateachinanorbit. The Holy Qur-ān In many engineering applications,

More information

Entropy and the Second Law of Thermodynamics

Entropy and the Second Law of Thermodynamics Entropy and the Second Law of Thermodynamics Reading Problems 7-1 7-3 7-88, 7-131, 7-135 7-6 7-10 8-24, 8-44, 8-46, 8-60, 8-73, 8-99, 8-128, 8-132, 8-1 8-10, 8-13 8-135, 8-148, 8-152, 8-166, 8-168, 8-189

More information

Assessment of Fundamental Concept in Thermodynamics

Assessment of Fundamental Concept in Thermodynamics Paper ID #10626 Assessment of Fundamental Concept in Thermodynamics Dr. Amir Karimi, University of Texas, San Antonio Amir Karimi, University of Texas, San Antonio Amir Karimi is a Professor of Mechanical

More information

ME 200 Thermodynamics I, Spring 2015, Exam 3, 8 p.m. to 9 p.m. on April 14, 2015

ME 200 Thermodynamics I, Spring 2015, Exam 3, 8 p.m. to 9 p.m. on April 14, 2015 ME 200 Thermodynamics I, Spring 2015, Exam 3, 8 p.m. to 9 p.m. on April 14, 2015 CIRCLE YOUR LECTURE BELOW: 7:30 a.m. 10:30 a.m. 12:30 p.m. 2:30 p.m. 4:30 p.m. Joglekar Chen Chen Kittel Naik INSTRUCTIONS

More information

ME 200 Exam 2 October 16, :30 p.m. to 7:30 p.m.

ME 200 Exam 2 October 16, :30 p.m. to 7:30 p.m. CIRCLE YOUR LECTURE BELOW: First Name Solution Last Name 7:30 am 8:30 am 10:30 am 11:30 am Joglekar Bae Gore Abraham 1:30 pm 3:30 pm 4:30 pm Naik Naik Cheung ME 200 Exam 2 October 16, 2013 6:30 p.m. to

More information

2.0 KEY EQUATIONS. Evaporator Net Refrigeration Effect. Compressor Work. Net Condenser Effect

2.0 KEY EQUATIONS. Evaporator Net Refrigeration Effect. Compressor Work. Net Condenser Effect 2.0 KEY EQUATIONS Evaporator Net Refrigeration Effect Q net refrigeration effect [] = (H 1 H 4 ) lb (Refrig Flow Rate) (60) min lb min hr H 1 = leaving evaporator enthalpy lb ; H 4 = entering evaporator

More information

Prediction of Evaporation Losses in Wet Cooling Towers

Prediction of Evaporation Losses in Wet Cooling Towers Heat Transfer Engineering, 27(9):86 92, 2006 Copyright C Taylor and Francis Group, LLC ISSN: 0145-7632 print / 1521-0537 online DOI: 10.1080/01457630600846372 Prediction of Evaporation Losses in Wet Cooling

More information

Lecture 29-30: Closed system entropy balance

Lecture 29-30: Closed system entropy balance ME 200 Thermodynamics I Spring 2016 Lecture 29-30: Closed system entropy balance Yong Li Shanghai Jiao Tong University Institute of Refrigeration and Cryogenics 800 Dong Chuan Road Shanghai, 200240, P.

More information