Chapter 20: Exercises: 3, 7, 11, 22, 28, 34 EOC: 40, 43, 46, 58

Similar documents
THE FIRST LAW OF THERMODYNAMICS

HEAT, WORK, AND THE FIRST LAW OF THERMODYNAMICS

Physics 2A (Fall 2012) Chapters 11:Using Energy and 12: Thermal Properties of Matter

Handout 12: Thermodynamics. Zeroth law of thermodynamics

Lecture 13 Heat Engines

PHYS1001 PHYSICS 1 REGULAR Module 2 Thermal Physics Chapter 17 First Law of Thermodynamics

Example problems. Chapter 3: The Kinetic Theory of Gases. Homework: 13, 18, 20, 23, 25, 27 (p )

Phys 22: Homework 10 Solutions W A = 5W B Q IN QIN B QOUT A = 2Q OUT 2 QOUT B QIN B A = 3Q IN = QIN B QOUT. e A = W A e B W B A Q IN.

Lecture 13. Heat Engines. Thermodynamic processes and entropy Thermodynamic cycles Extracting work from heat

Handout 12: Thermodynamics. Zeroth law of thermodynamics

02. Equilibrium Thermodynamics II: Engines

Entropy in Macroscopic Systems

Version 001 HW 15 Thermodynamics C&J sizemore (21301jtsizemore) 1

Chapter 20 The Second Law of Thermodynamics

Chemistry 420/523 Chemical Thermodynamics (Spring ) Examination 1

The Second Law of Thermodynamics. (Second Law of Thermodynamics)

Irreversible Processes

I affirm that I have never given nor received aid on this examination. I understand that cheating in the exam will result in a grade F for the class.

AP PHYSICS 2 WHS-CH-15 Thermodynamics Show all your work, equations used, and box in your answers!

Irreversible Processes

Speed Distribution at CONSTANT Temperature is given by the Maxwell Boltzmann Speed Distribution

Heat Engines and the Second Law of Thermodynamics

Phase transition. Asaf Pe er Background

Sec# Wave Motion - Superposition and Interference of Waves Grade# 50

Phase Changes and Latent Heat

Entropy & the Second Law of Thermodynamics

Chapter 9 Practical cycles

Chapter 1 Fundamentals

I have not proofread these notes; so please watch out for typos, anything misleading or just plain wrong.

S = S(f) S(i) dq rev /T. ds = dq rev /T

δq T = nr ln(v B/V A )

5. We use the following relation derived in Sample Problem Entropy change of two blocks coming to equilibrium:

Chemistry 531 Spring 2009 Problem Set 6 Solutions

Aljalal-Phys March 2004-Ch21-page 1. Chapter 21. Entropy and the Second Law of Thermodynamics

T ice T water T water = T ice =0 0 C. e =1

A) 2.0 atm B) 2.2 atm C) 2.4 atm D) 2.9 atm E) 3.3 atm

Chapter 20. Heat Engines, Entropy and the Second Law of Thermodynamics. Dr. Armen Kocharian

For the refrigerator of this problem, T H = 96 F = 309 K and T L = 70 F = 294 K, so K = (294 K)/(309 K 294 K) = 19.6.

PHYS102 Previous Exam Problems. Temperature, Heat & The First Law of Thermodynamics

ln. 1 We substitute V 2 = 2.00V 1 to obtain

dn i where we have used the Gibbs equation for the Gibbs energy and the definition of chemical potential

CHAPTER 19: Heat and the First Law of Thermodynamics


EF 152 Exam 3 - Fall, 2016 Page 1 Copy 223

Physics 202 Homework 5

Temperature Thermal Expansion Ideal Gas Law Kinetic Theory Heat Heat Transfer Phase Changes Specific Heat Calorimetry Heat Engines

Lecture Thermodynamics 9. Entropy form of the 1 st law. Let us start with the differential form of the 1 st law: du = d Q + d W

The laws of Thermodynamics. Work in thermodynamic processes

(Heat capacity c is also called specific heat) this means that the heat capacity number c for water is 1 calorie/gram-k.

1985B4. A kilogram sample of a material is initially a solid at a temperature of 20 C. Heat is added to the sample at a constant rate of 100

The first law of thermodynamics. U = internal energy. Q = amount of heat energy transfer

C e. Negative. In a clockwise cycle, the work done on the gas is negative. Or for the cycle Qnet = +600 J and U = 0 so W = Q = 600 J

CHEM 305 Solutions for assignment #4

MULTIPLE CHOICE. Choose the one alternative that best completes the statement or answers the question.

Kinetic Theory continued

The extreme case of the anisothermal calorimeter when there is no heat exchange is the adiabatic calorimeter.

Heat What is heat? Work = 2. PdV 1

Kinetic Theory continued

First Law of Thermodynamics

Q(J) Wen = 0 &UCD = QCD - WCD ~ QCD = -60 L atm. .<.-^-l- M -«K

A short note on Reitlinger thermodynamic cycles

Chapter 20 Entropy and the 2nd Law of Thermodynamics

Efficiencies. Damian Vogt Course MJ2429. Nomenclature. Symbol Denotation Unit c Flow speed m/s c p. pressure c v. Specific heat at constant J/kgK

Theory of turbomachinery. Chapter 1

Physics 101: Lecture 28 Thermodynamics II

Module - 1: Thermodynamics

PV/T = k or PV = kt Describe the difference between an ideal gas and a real gas.

COMPENDIUM OF EQUATIONS Unified Engineering Thermodynamics

Example problems. Chapter 2: Temperature, heat, and the 1 st law of Thermodynamic. Homework: 2, 3, 4, 5, 6, 10, 15, 19, 21 (pages )

A) 120 degrees B) 90 degrees C) 60 degrees D) 45 degrees E) 30 degrees

The First Law of Thermodynamics

6. (6) Show all the steps of how to convert 50.0 F into its equivalent on the Kelvin scale.

11/15/2017. F GonP. F PonG THERMAL ENERGY OF IDEAL GAS HIGH PRESSURE GAS IN A CYLINDER REMEMBER HIGH PRESSURE GAS IN A CYLINDER

FINITE TIME THERMODYNAMIC MODELING AND ANALYSIS FOR AN IRREVERSIBLE ATKINSON CYCLE. By Yanlin GE, Lingen CHEN, and Fengrui SUN

Chapter 12 Solutions. Q Reason: We ll use Equation Q = McΔT and solve for M. We are given. In each case we want to solve for.

THERMODYNAMICS. Zeroth law of thermodynamics. Isotherm

Chapter 20. and the corresponding change in entropy is 1 absorbed (see Eq. 20-2). S T dq Q T, where Q is the heat

HEAT, WORK, AND THE FIRST LAW OF THERMODYNAMICS

Chapters 17 &19 Temperature, Thermal Expansion and The Ideal Gas Law

Non-Equilibrium Thermodynamics for Engineers

Phys102 First Major-182 Zero Version Coordinator: A A Naqvi Thursday, February 14, 2019 Page: 1

Actual exergy intake to perform the same task

Class 22 - Second Law of Thermodynamics and Entropy

First major ( 043 ) a) 180 degrees b) 90 degrees c) 135 degrees d) 45 degrees e) 270 degrees

How to please the rulers of NPL-213 the geese

Speed Distribution at CONSTANT Temperature is given by the Maxwell Boltzmann Speed Distribution

S15--AP Phys Q4--Heat-Thermo Ch13_14_15 PRACTICE

Quiz C&J page 365 (top), Check Your Understanding #12: Consider an ob. A) a,b,c,d B) b,c,a,d C) a,c,b,d D) c,b,d,a E) b,a,c,d

Physics 5D PRACTICE FINAL EXAM Fall 2013

PHYsics 1150 Homework, Chapter 14, Thermodynamics Ch 14: 1, 17, 26, 27, 37, 44, 46, 52, 58

University of Washington Department of Chemistry Chemistry 452/456 Summer Quarter 2011

Physics 115. Specific heats revisited Entropy. General Physics II. Session 13

UNIVERSITY COLLEGE LONDON. University of London EXAMINATION FOR INTERNAL STUDENTS. For The Following Qualifications:-

FUGACITY. It is simply a measure of molar Gibbs energy of a real gas.

Grain elevator. You need to convince your boss that this is a very inefficient system.

Questions and Problems

Physics 231. Topic 14: Laws of Thermodynamics. Alex Brown Dec MSU Physics 231 Fall

What is thermodynamics? and what can it do for us?

EF 152 Exam 3 - Fall, 2018 Page 1 Version: A Copy 50

Thermal Conductivity, k

Transcription:

Chater 0: Exercises:, 7,,, 8, 4 EOC: 40, 4, 46, 8 E: A gasoline engine takes in.80 0 4 and delivers 800 of work er cycle. The heat is obtained by burning gasoline with a heat of combustion of 4.60 0 4. What is the thermal efficiency? Part B ow much heat is discarded in each cycle? Part C What mass of fuel is burned in each cycle? Part D If the engine goes through 0.0 cycles er second, what is its ower outut in kilowatts? Part E If the engine goes through 0.0 cycles er second, what is its ower outut in horseower?

E7: What comression ratio must an Otto cycle have to achieve an ideal efficiency of 66. if.4? E: A window air-conditioner unit absorbs 9.80 0 4 same time eriod deosits.0 0 What is the ower consumtion of the unit? of heat er minute from the room being cooled and in the of heat into the outside air. Part B What is the energy efficiency rating of the unit? E: Descrition: A Carnot heat engine uses a hot reservoir consisting of a large amount of boiling water and a cold reservoir consisting of a large tub of ice and water. In five minutes of oeration of the engine, the heat rejected by the engine melts 0.0400 kg of... A Carnot heat engine uses a hot reservoir consisting of a large amount of boiling water and a cold reservoir consisting of a large tub of ice and water. In five minutes of oeration of the engine, the heat rejected by the engine melts 0.0400 of ice. During this time, how much work is erformed by the engine?

E8: Descrition: You make tea with 0.0 kg of T water and let it cool to room temerature (0.0 degree(s) C) before drinking it. (a) Calculate the entroy change of the water while it cools. (b) The cooling rocess is essentially isothermal for the air in your... You make tea with 0.0 of 86.0 water and let it cool to room temerature (0.0 ) before drinking it. Calculate the entroy change of the water while it cools. Part B The cooling rocess is essentially isothermal for the air in your kitchen. Calculate the change in entroy of the air while the tea cools, assuming that all the heat lost by the water goes into the air. Part C What is the total entroy change of the system tea + air? Exress your answer using two significant figures.

E4: Descrition: A box is searated by a artition into two arts of equal volume. The left side of the box contains 00 molecules of nitrogen gas; the right side contains 00 molecules of oxygen gas. The two gases are at the same temerature. The artition is... A box is searated by a artition into two arts of equal volume. The left side of the box contains 00 molecules of nitrogen gas; the right side contains 00 molecules of oxygen gas. The two gases are at the same temerature. The artition is unctured, and equilibrium is eventually attained. Assume that the volume of the box is large enough for each gas to undergo a free exansion and not change temerature. On average, how many molecules of oxygen will there be in either half of the box? Exress your answer using two significant figures. molecules Part B On average, how many molecules of nitrogen will there be in either half of the box? Exress your answer using two significant figures. molecules Part C What is the change in entroy of the system when the artition is unctured? Part D What is the robability that the molecules will be found in the same distribution as they were before the artition was unctured, that is, 00 nitrogen molecules in the left half and 00 oxygen molecules in the right half? Give the order of magnitude. Exress your answer as the order of magnitude. If your answer is, so you would enter -7, then the order of magnitude is

0.40. IDENTIFY: Use the ideal gas law to calculate and for each state. Use the first law and secific exressions for Q, W, and U for each rocess. Use Eq.(0.4) to calculate e. Q is the net heat flow into the gas. SET UP: γ.40 C R /( γ ) 0.79 J/mol K; C C + R 9.0 J/mol K. The cycle is sketched in Figure 0.40. Figure 0.40 EXECUTE: (a) oint.00 atm.0 0 Pa (given); nrt; nrt (0.0 mol)(8.4 J/mol K)(00 K) 8.6 0 m.0 0 Pa oint rocess at constant volume so 8.6 0 m nrt and n, R, constant imlies / T / T T T ( / ) (.00 atm)(600 K/00 K).00 atm.0 0 Pa oint Consider the rocess, since it is simler than. Process is at constant ressure so nrt and n, R, constant imlies / T / T.00 atm.0 0 Pa ( T / T ) (8.6 0 m )(49 K/00 K) 4. 0 m (b) rocess constant volume ( 0) Q nc T (0.0 mol)(0.79 J/mol K)(600 K 00 K) 80 J 0 and W 0. Then U Q W 80 J rocess Adiabatic means Q 0. U nc T (any rocess), so U (0.0 mol)(0.79 J/mol K)(49 K 600 K) 780 J T 00 K T 600 K T 49 K Then U Q W gives W Q U + 780 J. (It is correct for W to be ositive since is ositive.) rocess For constant ressure W (.0 0 Pa)(8.6 0 m 4. 0 m ) 60 J or W nr T (0.0 mol)(8.4 J/mol K)(00 K 49 K) 60 J, which checks. (It is correct for W to be negative, since is negative for this rocess.) Q nc T (0.0 mol)(9.0 J/mol K)(00 K 49 K) 960 J U Q W 960 J ( 60 K) 400 J or U nc T (0.0 mol)(0.79 J/mol K)(00 K 49 K) 400 J, which checks (c) Wnet W + W + W 0 + 780 J 60 J + 0 J (d) Qnet Q + Q + Q 80 J + 0 960 J + 0 J work outut W 0 J (e) e 0.0 0.%. heat energy inut Q 80 J e(carnot) T / T 00 K/600 K 0.00. C EALUATE: For a cycle U 0, so by U Q W it must be that Qnet Wnet for a cycle. We can also check that U net 0: U net U + U + U 80 J 00 J 0 J 0 e < e(carnot), as it must.

0.4. IDENTIFY: Tb Tc and is equal to the maximum temerature. Use the ideal gas law to calculate T a. Aly the aroriate W exression to calculate Q for each rocess. e. U 0 for a comlete cycle and for an isothermal rocess of an ideal gas. Q SET UP: For helium, C R / and C R /. The maximum efficiency is for a Carnot cycle, and ecarnot TC / T. EXECUTE: (a) Qin Qab + Qbc. Qout Q ca. Tmax Tb Tc 7 C 600 K. aa bb a nrt Ta Tb (600 K) 00 K. b ( moles)(8. J/mol K)(600 K) bb nrtb b 0.0 m. T T.0 0 Pa a b b b b c c b c b (0.0 m ) 0.0997 m a. Tb Tc c Qab nc Tab ( ) c c nrtb c Qbc Wbc d d nrtb ln nrtb ln. b b bc ( mol) 8. J/mol K (400 K) 9.97 0 J ( ) Q 4 (.00 mol) 8. J/mol K (600 K)ln.0 0 J. b Q Q Q Qout Qca nc Tca ( ) b 4 in ab + bc.0 0 J. 4 (.00 mol) 8. J/mol K (400 K).66 0 J. 4 4 (b) Q U + W 0 + W W Q Q.0 0 J.66 0 J 4.4 0 J. in out 4.4 0 J e W Qin 0. %. 4.0 0 J TC (c) e 00 K max ecarnot 0.67 67% T 600 K EALUATE: The thermal efficiency of this cycle is about one-third of the efficiency of a Carnot cycle that oerates between the same two temeratures.

0.46. IDENTIFY: Use Eq.(0.4) to calculate e. SET UP: The cycle is sketched in Figure 0.46. C R / for an ideal gas C C + R 7 R / SET UP: rocess Figure 0.46 Calculate Q and W for each rocess. 0 imlies W 0 & 0 imlies Q nc T nc ( T T ) But nrt and constant says nrt and nrt. ( ) nr( T T ); nr T (true when is constant). Thus Q nc T nc ( / nr) ( C / R) ( C / R) ( ) ( C / R). Q > 0; heat is absorbed by the gas.) Then 0 0 0 0 0 rocess 0 so W ( ) 0( 0 0 ) 00 (W is ositive since increases.) 0 imlies Q nc ( ) T nc T T But nrt and constant says nrt and nrt. ( ) nr( T T ); nr T (true when is constant). Thus Q nc T nc ( / nr) ( C / R) ( C / R) ( ) ( C / R). ( Q > 0; heat is absorbed by the gas.) Then 0 0 0 0 0 rocess 4 0 imlies W 0 0 so Q nc T nc ( / nr) ( C / R)( )( ) ( C / R) 0 0 0 0 0 ( Q < 0 so heat is rejected by the gas.) rocess 4 0 so W ( 4 ) 0( 0 0 ) 00 (W is negative since decreases) 0 so Q nc T nc ( / nr) ( C / R) ( C / R) 0( 0 0 ) ( C / R) 00 ( Q < 0 so heat is rejected by the gas.) total work erformed by the gas during the cycle: W W + W + W + W 0 + + 0 tot 4 4 0 0 0 0 0 0 (Note that W equals the area enclosed by the cycle in the -diagram.) tot total heat absorbed by the gas during the cycle C C C + C Q Q + Q + R R R 0 0 0 0 0 0 ( Q ): eat is absorbed in rocesses and. C + ( C + R) C + R But C C + R so Q 00 00. R R total heat rejected by the gas during the cycle ( Q ): eat is rejected in rocesses 4 and 4. C C C + C Q Q + Q R R R C 4 4 0 0 0 0 0 0 C + ( C + R) C + R But C C + R so QC 00 00. R R W 00 R R efficiency e Q [C + R]/ R ( ) C + R ( R/) + R 9 ( ) 0 0 C. e 0.0 0.% C + R C + R EALUATE: As a check on the calculations note that QC + Q 00 + 00 00 W, as it should. R R

0.8. IDENTIFY and SET UP: First use the methods of Chater 7 to calculate the final temerature T of the system. EXECUTE: 0.600 kg of water (cools from 4.0 C to T) Q mc T (0.600 kg)(490 J/kg K)( T 4.0 C) (4 J/K) T. 0 J 0.000 kg of ice (warms to 0 C, melts, and water warms from 0 C to T) Q mc (0 C (.0 C)) + ml + mc ( T 0 C) ice f water Q + + 4 4 Q 7 J +.67 0 J + (09. J/K) T.88 0 J + (09. J/K) T 0.000 kg (00 J/kg K)(.0 C) 4 0 J/kg (490 J/kg K)( T 0 C) Q system 0 gives 4 (4 J/K) T. 0 J +.88 0 J + (09. J/K) T 0 4 (.74 0 J/K) T 9.48 0 J 4 T (9.48 0 J)/(.74 0 J/K) 4.8 C 08 K EALUATE: The final temerature must lie between.0 C and 4.0 C. A final temerature of 4.8 C is consistent with only liquid water being resent at equilibrium. IDENTIFY and SET UP: Now we can calculate the entroy changes. Use S Q / T for hase changes and the method of Examle 0.6 to calculate S for temerature changes. EXECUTE: ice: The rocess takes ice at C and roduces water at 4.8 C. Calculate S for a reversible rocess between these two states, in which heat is added very slowly. S is ath indeendent, so S for a reversible rocess is the same as S for the actual (irreversible) rocess as long as the initial and final states are the same. S dq / T, where T must be in kelvins For a temerature change dq mc dt so For a hase change, since it occurs at constant T, S dq / T Q / T ± ml / T. T S ( mc / T ) dt mcln( T / T ). Therefore ice ice f water T S mc ln(7 K/8 K) + ml / 7 K + mc ln(08 K/7 K) S ice (0.000 kg)[(00 J/kg K) ln(7 K/8 K) + (4 0 J/kg)/7 K + (490 J/kg K) ln(08 K/7 K)] S ice.9 J/K + 6.7 J/K +.7 J/K 9.4 J/K water: Swater mc ln( T / T ) (0.600 kg)(490 J/kg K)ln(08 K/8 K) 80. J/K For the system, S Sice + Swater 9.4 J/K 80. J/K + J/K EALUATE: Our calculation gives S > 0, as it must for an irreversible rocess of an isolated system.