Modern Engineering Thermodynamics

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Problems 725 the officer asks Paul for the value of his experimental LTN, promising to release him if his answer is correct. Paul replies, “0.29, sir.” The officer then consults the state patrolman’s guide to locomotion transport numbers for the correct value. Does Paul get arrested? 47.* Tom is a 75.0 kg bicyclist who recently averaged 42.0 km/h during a 240. km race with an 8.40 kg racing bike. If he consumes 4100. L of oxygen and has a muscle energy conversion efficiency of 25.0%, determine a. His rate of conversion of oxygen in L/min. b. His locomotion transport number. 48. Sharla, weighing 140. lbf, absorbs 0.500 hp in her muscles while pedaling a 7.00 lbf bicycle at 25.0 mph into a 5.00 mph head wind in air at 70.0°F. Her frontal cross-section is 4.00 ft by 2.00 ft, and her drag coefficient is 0.500. a. Compute her locomotion transport number. b. Determine her most efficient velocity on the bicycle. 49.* Jim has a frontal cross-section of 2.00 m high by 0.500 m wide and can run at 4.00 m/s and swim at 1.00 m/s. His drag coefficients in air and water are 1.30 and 1.10, respectively. What speeds should Jim run and swim at to be most efficient? Assume Jim’s BMR is 0.300 MJ/h. 50.* Determine which of the following expends the most energy over a 20.0 mi course: a. A 126 kg pedal-powered aircraft flying at a speed of 15.0 mph with a locomotion transport number of 0.134. b. A fast walking 75.0 kg person walking at a speed of 2.50 mph, c. Determine the energy expenditure rates of the person powering the aircraft and the person walking and comment on the feasibility of maintaining these rates over the 20.0 mi course. 51. If King Kong was ten times bigger than a normal human being, a. Find his locomotion transport number while riding a bicycle (assume his bicycle locomotion transport number is 25.0% of the minimum value shown on Figure 17.12). b. What was his most efficient walking velocity (assume the same drag coefficient as for a human). 52. Convert the k d /α information associated with Eq. (17.33) from metric units into <strong>Engineering</strong> English units. 53.* If a cold-blooded animal has an activation entropy of death of 3088 kJ/(kgmole · K) at 25.0°C, what is the change in k d /α for the animal if it moves to an environment at 20.0°C? 54.* If the specific molar activation enthalpy of death is 800. MJ/ kgmole, the compensation temperature is 330. K, and the constant β = −276 kJ/ðkgmole.KÞ, determine the specific molar activation entropy of death. Design Problems The following are open-ended design problems. The objective is to carryoutapreliminarydesignasindicated. A detailed design with working drawings is not required unless otherwise specified by your instructor. These problems have no specific answers, so each student’s design is unique. 55. Design an inexpensive apparatus that measures the energy conversion efficiency of an in vivo human arm or leg muscle. Measure the oxygen consumption rate of the test subject to determine the energy input rate. Include proper transducer instrumentation for the necessary input data, and specify adequate output electronics. Provide assembly and detailed drawings sufficient to allow a technician to fabricate, assemble, and test your design. 56. One of the problems with the commercially available bomb calorimeters is that they can test only small samples on the order of a few grams. Design a bomb calorimeter large enough to burn a sample as large as 1 pound. Pay special attention to safety considerations in your design. Do not attempt to construct or test your design. 57. Design a system that measures the rate of metabolic heat production of a small warm-blooded animal. You may use either a direct or an indirect calorimetry technique. Provide engineering drawings and instrumentation specifications. 58. Design a whole body calorimeter that measures the instantaneous metabolic heat loss rate from an entire human body. Your system must be large enough or else sufficiently mobile that measurements can be made while the test subject is doing physical labor without restraint from your system. 59. Design a variable resistance rowing exercise machine that has a direct digital readout of the instantaneous energy expenditure rate of the user. This means you have to specify or design transducers that measure the instantaneous work rate (i.e., power) done on the machine. This power can be absorbed by the machine either electrically or mechanically. Provide assembly and detail drawings of your design plus specify all the electronics necessary to process the transducer signals and provide the proper digital output. 60. Design an apparatus that measures the metabolic heat loss rate and surface temperature of a yeast culture or a small insect at various environmental temperatures. Construct and calibrate this apparatus if possible, and make enough measurements to plot _Q /T b for some living system vs. time at various environmental temperatures. Does _Q /T b increase or decrease as the environmental temperature decreases? Computer Problems The following open-ended computer problems are designed to be done on a personal computer using a spreadsheet, equation solver, or programming language. 61. Develop an interactive computer program that returns the user’s basal metabolic rate, oxygen uptake rate, carbon dioxide production rate, pulse rate, and breathing rate when the user inputs his or her mass or weight. 62. Develop an interactive computer program that outputs the energy conversion efficiency of a person or an animal. The user must be prompted for input data regarding work performed, energy output resulting in increases in potential or kinetic energies, and changes in body total internal energy. You may assume that the specific internal energy of the body is constant for activities that occur over short time periods. 63. Develop an interactive computer program that provides the user with the metabolizable energy content of foods chosen from a menu. Allow the user to specify the desired energy units (Calories, Btu, MJ) of the output.
726 CHAPTER 17: <strong>Thermodynamics</strong> of Biological Systems 64. Develop an interactive computer program that returns the user’s daily caloric food intake needs when the user selects his or her activities from a screen menu and inputs the time devoted to each activity. 65. Combine the programs of Problems 63 and 64 to produce an interactive computer program that returns a series of three possible exercise programs to achieve a weight-loss goal input by the user. The user must also input his or her current caloric consumption and physical activities. (Note: This is a computer exercise only. You are not qualified to give medical advice to anyone regarding eating or exercise habits, so do not allow anyone, including yourself, to use your program to develop an actual weight-loss schedule. Anyone seeking this advice must consult a qualified physician.)
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Modern Engineering Thermodynamics
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Modern Engineering Thermodynamics R
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Dedication WHAT IS AN ENGINEER AND
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Contents PREFACE . . . . . . . . .
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Contents ix 7.6 Heat Engines Runnin
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Contents xi 14.13 Air Standard Gas
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Preface TEXT OBJECTIVES This textbo
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Preface xv Step 5. Write down the b
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Acknowledgments I wish to acknowled
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Resources That Accompany This Book
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List of Symbols A a B COP CR c c p
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Prologue PARIS FRANCE, 10:35 AM, AU
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CHAPTER 1 The Beginning CONTENTS 1.
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1.2 Why Is Thermodynamics Important
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1.3 Getting Answers: A Basic Proble
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1.5 How Do We Measure Things? 7 bei
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1.6 Temperature Units 9 THE DEVELOP
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1.7 Classical Mechanical and Electr
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1.7 Classical Mechanical and Electr
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1.9 Modern Units Systems 15 where M
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1.10 Significant Figures 17 CRITICA
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1.10 Significant Figures 19 WHAT AB
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1.11 Potential and Kinetic Energies
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1.11 Potential and Kinetic Energies
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Summary 25 FIGURE 1.19 Case study 1
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Problems 27 Problems (* indicates p
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Problems 29 14. Determine the mass
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Problems 31 49. Using the CGS units
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CHAPTER 2 Thermodynamic Concepts CO
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2.3 Phases of Matter 35 System boun
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2.4 System States and Thermodynamic
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2.6 Thermodynamic Processes 39 WHAT
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2.7 Pressure and Temperature Scales
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2.9 The Continuum Hypothesis 43 Sur
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2.10 The Balance Concept 45 Solutio
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2.11 The Conservation Concept 47 or
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2.11 The Conservation Concept 49 Th
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Summary 51 change in the mass of X
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Problems 53 Problems (* indicates p
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Problems 55 and Death rate = α 2 +
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CHAPTER 3 Thermodynamic Properties
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3.3 Fun with Mathematics 59 CRITICA
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3.4 Some Exciting New Thermodynamic
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3.6 Enthalpy 63 WHO WAS AMALIE EMMY
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3.7 Phase Diagrams 65 WHO WAS EMMY
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Pressure Vapor 3.7 Phase Diagrams 6
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3.7 Phase Diagrams 69 WHAT IS A “
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3.7 Phase Diagrams 71 considerable
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3.8 Quality 73 10 5 300 C Critical
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3.8 Quality 75 Although Eq. (3.26)
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3.9 Thermodynamic Equations of Stat
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3.10 Thermodynamic Tables 85 Critic
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3.12 Thermodynamic Charts 87 vð100
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3.13 Thermodynamic Property Softwar
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Summary 91 and e = E/m = u + V2 2g
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Problems 93 c. For a saturated mixt
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Problems 95 specific enthalpy of sa
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Problems 97 Table 3.23 Problem 65 M
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CHAPTER 4 The First Law of Thermody
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4.3 The First Law of Thermodynamics
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4.3 The First Law of Thermodynamics
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4.4 Energy Transport Mechanisms 105
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4.5 Point and Path Functions 107 4.
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4.6 Mechanical Work Modes of Energy
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4.7 Nonmechanical Work Modes of Ene
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4.9 Work Efficiency 125 In the case
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4.12 Heat Modes of Energy Transport
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4.13 Heat Transfer Modes 129 Table
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4.14 A Thermodynamic Problem Solvin
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4.14 A Thermodynamic Problem Solvin
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4.15 How to Write a Thermodynamics
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4.15 How to Write a Thermodynamics
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Summary 139 The general open system
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Problems 141 11.* Determine the hea
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Problems 143 where K = 0.810 lbf. D
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Problems 145 Table 4.12 Problem 67
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CHAPTER 5 First Law Closed System A
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5.2 Sealed, Rigid Containers 149 In
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5.4 Power Plants 151 Step 7. Calcul
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5.5 Incompressible Liquids 153 The
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1Q 2 − 1 W 2 = mðu 2 − u 1 Þ
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5.8 Closed System Unsteady State Pr
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5.9 The Explosive Energy of Pressur
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Problems 161 Problems (* indicates
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Problems 163 31. A thermoelectric g
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Problems 165 where v, T, and r are
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CHAPTER 6 First Law Open System App
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6.2 Mass Flow Energy Transport 169
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6.3 Conservation of Energy and Cons
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6.4 Flow Stream Specific Kinetic an
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6.5 Nozzles and Diffusers 175 m (a)
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6.5 Nozzles and Diffusers 177 We ar
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6.6 Throttling Devices 179 These as
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6.6 Throttling Devices 181 For an i
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6.7 Throttling Calorimeter 183 The
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6.8 Heat Exchangers 185 Convective
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6.9 Shaft Work Machines 187 6.9 SHA
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6.9 Shaft Work Machines 189 1 Basem
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6.10 Open System Unsteady State Pro
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Problems 197 we have _m R / _m D =
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Problems 201 32.* A commercial slid
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Summary 203 59. Incompressible liqu
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CHAPTER 7 Second Law of Thermodynam
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7.3 The Second Law of Thermodynamic
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7.4 Carnot’s Heat Engine and the
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7.4 Carnot’s Heat Engine and the
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7.5 The Absolute Temperature Scale
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7.5 The Absolute Temperature Scale
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7.6 Heat Engines Running Backward 2
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7.7 Clausius’s Definition of Entr
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7.8 Numerical Values for Entropy 22
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7.10 Differential Entropy Balance 2
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7.11 Heat Transport of Entropy 229
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7.13 Entropy Production Mechanisms
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7.14 Heat Transfer Production of En
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7.15 Work Mode Production of Entrop
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7.15 Work Mode Production of Entrop
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7.16 Phase Change Entropy Productio
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Summary 241 ■ Indirect method inv
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Problems 243 amount of work W irr i
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Problems 245 a. If the heat pump is
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Problems 247 51. Develop a program
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CHAPTER 8 Second Law Closed System
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8.2 Systems Undergoing Reversible P
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8.3 Systems Undergoing Irreversible
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8.4 Diffusional Mixing 271 Exercise
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Summary 273 Note that this example
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Problems 275 15. A 20.0 ft 3 tank c
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Problems 277 46. a. Determine a for
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CHAPTER 9 Second Law Open System Ap
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9.4 Open System Entropy Balance Equ
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9.4 Open System Entropy Balance Equ
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9.5 Nozzles, Diffusers, and Throttl
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9.5 Nozzles, Diffusers, and Throttl
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9.6 Heat Exchangers 289 Exercises 1
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9.6 Heat Exchangers 291 (T H ) (T H
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9.7 Mixing 293 Now, _m air is given
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9.7 Mixing 295 Critical value of y,
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9.9 Unsteady State Processes in Ope
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Problems 309 Multiplying this equat
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Problems 311 entropy production rat
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Problems 313 heat is added to the b
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Problems 315 55.* Determine the max
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Problems 317 The cavitation process
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CHAPTER 10 Availability Analysis CO
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10.3 What Are Conservative Forces?
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10.6 Availability 323 WHAT IS A SYS
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10.6 Availability 325 and the total
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10.7 Closed System Availability Bal
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10.7 Closed System Availability Bal
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10.8 Flow Availability 331 EXAMPLE
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s − s 0 = c ln T T 0 10.8 Flow Av
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10.10 Modified Availability Rate Ba
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10.10 Modified Availability Rate Ba
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10.11 Energy Efficiency Based on th
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Summary 351 In this problem, we hav
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Summary 353 7. The general open sys
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Problems 355 12.5 Btu/hr·ft ·R. I
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Problems 357 flow rate of 15.0 lbm/
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Problems 359 85. Create a specific
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CHAPTER 11 More Thermodynamic Relat
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11.2 Two New Properties: Helmholtz
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11.2 Two New Properties: Helmholtz
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11.4 Maxwell Equations 367 11.4 MAX
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11.4 Maxwell Equations 369 then,
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11.5 The Clapeyron Equation 371 and
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11.6 Determining u, h, and s from p
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11.7 Constructing Tables and Charts
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11.8 Thermodynamic Charts 381 so th
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11.9 Gas Tables 383 where p r is th
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11.10 Compressibility Factor and Ge
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11.11 Is Steam Ever an Ideal Gas? 3
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Summary 399 equation, and a series
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Problems 401 20.* Estimate h fg for
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Problems 403 Design Problems The fo
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CHAPTER 12 Mixtures of Gases and Va
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12.2 Thermodynamic Properties of Ga
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12.3 Mixtures of Ideal Gases 413 Th
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12.3 Mixtures of Ideal Gases 415 Co
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12.4 Psychrometrics 417 Finally, th
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12.4 Psychrometrics 419 EXAMPLE 12.
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12.6 The Sling Psychrometer 421 The
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12.6 The Sling Psychrometer 423 p w
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12.7 Air Conditioning 425 WHAT ENVI
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12.8 Psychrometric Enthalpies 427 E
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12.8 Psychrometric Enthalpies 429 o
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12.9 Mixtures of Real Gases 431 Whe
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12.9 Mixtures of Real Gases 433 and
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12.9 Mixtures of Real Gases 435 The
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12.9 Mixtures of Real Gases 437 Sol
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Summary 439 Last, we combine Dalton
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Problems 443 exhaust gas is an idea
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Problems 445 57.* Cooling towers ar
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CHAPTER 13 Vapor and Gas Power Cycl
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13.2 Part I. Engines and Vapor Powe
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13.4 Rankine Cycle 457 A B Reversib
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13.5 Operating Efficiencies 459 For
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13.5 Operating Efficiencies 461 13.
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13.5 Operating Efficiencies 463 b.
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13.5 Operating Efficiencies 465 Sta
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13.6 Rankine Cycle with Superheat 4
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13.7 Rankine Cycle with Regeneratio
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13.8 The Development of the Steam T
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13.9 Rankine Cycle with Reheat 477
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13.9 Rankine Cycle with Reheat 479
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13.10 Modern Steam Power Plants 481
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13.12 Air Standard Power Cycles 487
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13.13 Stirling Cycle 489 Q H 4 1 4
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13.14 Ericsson Cycle 491 Q H 4 1 3
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13.15 Lenoir Cycle 493 Exercises 28
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13.16 Brayton Cycle 495 Solution Us
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13.16 Brayton Cycle 497 Equation (7
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13.17 Aircraft Gas Turbine Engines
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13.17 Aircraft Gas Turbine Engines
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13.18 Otto Cycle 503 T Q H 1 1 1 v
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13.18 Otto Cycle 505 Exercises 40.
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13.18 Otto Cycle 507 and, since the
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13.20 Miller Cycle 509 13.19.1 Mode
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13.20 Miller Cycle 511 Then, from F
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13.21 Diesel Cycle 513 to stroll on
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13.21 Diesel Cycle 515 Solution a.
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13.22 Modern Prime Mover Developmen
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13.23 Second Law Analysis of Vapor
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Summary 525 Fill port 160 mm End of
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Problems 527 7. The thermal efficie
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efficiency increase if the condense
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Problems 531 horsepower hour. Assum
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Problems 533 72. Determine the valu
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CHAPTER 14 Vapor and Gas Refrigerat
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14.3 Carnot Refrigeration Cycle 537
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14.4 In the Beginning There Was Ice
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14.4 In the Beginning There Was Ice
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14.5 Vapor-Compression Refrigeratio
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14.5 Vapor-Compression Refrigeratio
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14.6 Refrigerants 547 T 3 2s 2 p 3
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14.7 Refrigerant Numbers 549 14.7 R
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14.7 Refrigerant Numbers 551 R-110
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14.8 CFCs and the Ozone Layer 553 H
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14.9 Cascade and Multistage Vapor-C
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14.10 Absorption Refrigeration 561
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14.11 Commercial and Household Refr
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14.14 Reversed Brayton Cycle Refrig
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14.14 Reversed Brayton Cycle Refrig
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14.15 Reversed Stirling Cycle Refri
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14.16 Miscellaneous Refrigeration T
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14.16 Miscellaneous Refrigeration T
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14.18 Second Law Analysis of Refrig
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14.18 Second Law Analysis of Refrig
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2. The coefficient of performance o
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Problems 585 13.* A refrigeration u
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Problems 587 Loop B Station 1B Stat
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Problems 589 under these conditions
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CHAPTER 15 Chemical Thermodynamics
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15.2 Stoichiometric Equations 593 1
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15.2 Stoichiometric Equations 595 C
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15.3 Organic Fuels 597 ANSWERS SOME
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15.4 Fuel Modeling 599 Hydrocarbon
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15.4 Fuel Modeling 601 equation, si
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15.5 Standard Reference State 603 I
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15.6 Heat of Formation 605 and H 2
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15.7 Heat of Reaction 607 EXAMPLE 1
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15.7 Heat of Reaction 609 CRITICAL
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15.7 Heat of Reaction 611 Then, h P
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15.8 Adiabatic Flame Temperature 61
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15.9 Maximum Explosion Pressure 619
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15.10 Entropy Production in Chemica
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15.10 Entropy Production in Chemica
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15.11 Entropy of Formation and Gibb
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15.12 Chemical Equilibrium and Diss
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H 2 O !ð1 − yÞH 2 O + yðv H2
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15.14 The van’t Hoff Equation 635
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15.15 Fuel Cells 637 Anode Electrol
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15.15 Fuel Cells 639 The maximum po
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15.16 Chemical Availability 641 and
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ðn i /n fuel Þðc pi Þ E system
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Problems 645 where j = 4n + m kgmol
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Problems 647 c. The percent excess
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Problems 649 77. Determine the mola
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CHAPTER 16 Compressible Fluid Flow
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16.3 Isentropic Stagnation Properti
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16.4 The Mach Number 655 Note that
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16.4 The Mach Number 657 Table 16.1
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16.4 The Mach Number 659 Since for
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16.5 Converging-Diverging Flows 661
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16.5 Converging-Diverging Flows 663
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16.6 Choked Flow 665 T a a p a = co
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16.6 Choked Flow 667 Exercises 16.
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16.7 Reynolds Transport Theorem 669
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16.7 Reynolds Transport Theorem 671
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16.8 Linear Momentum Rate Balance 6
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Page 772 and 773: 18.8 Quantum Statistical Thermodyna
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Page 776 and 777: 18.11 Monatomic Maxwell-Boltzmann G
Page 778 and 779: 18.12 Diatomic Maxwell-Boltzmann Ga
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Page 782 and 783: 18.13 Polyatomic Maxwell-Boltzmann
Page 784 and 785: Summary 759 In this chapter, we sum
Page 786 and 787: Problems 761 4. Find the temperatur
Page 788 and 789: CHAPTER 19 Introduction to Coupled
Page 790 and 791: 19.3 Linear Phenomenological Equati
Page 792 and 793: 19.4 Thermoelectric Coupling 767 Eq
Page 794 and 795: 19.4 Thermoelectric Coupling 769 Th
Page 796 and 797: 19.4 Thermoelectric Coupling 771 wh
Page 798 and 799: 19.4 Thermoelectric Coupling 773 Th
Page 800 and 801:
19.4 Thermoelectric Coupling 775 b.
Page 802 and 803:
19.5 Thermomechanical Coupling 777
Page 804 and 805:
Page 806 and 807:
Page 808 and 809:
water), it seems reasonable that li
Page 810 and 811:
Problems 785 b. For a Knudson gas,
Page 812 and 813:
Appendix A: Physical Constants and
Page 814 and 815:
Appendix B: Greek and Latin Origins
Page 816 and 817:
Appendix B 791 Table B.4 Plural End
Page 818 and 819:
Index Page numbers followed by f in
Page 820 and 821:
Index 795 E e (specific energy), 10
Page 822 and 823:
Index 797 Isobaric coefficient of v
Page 824 and 825:
Index 799 Ranque, Georges Joseph, 3
Page 826 and 827:
Index 801 William III, King of Engl
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Modern Engineering Thermodynamics

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