CHAPTER - 12 THERMODYNAMICS

Similar documents
THERMODYNAMICS. Zeroth law of thermodynamics. Isotherm

THERMODYNAMICS b) If the temperatures of two bodies are equal then they are said to be in thermal equilibrium.

Answer: Volume of water heated = 3.0 litre per minute Mass of water heated, m = 3000 g per minute Increase in temperature,

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

Thermodynamic system is classified into the following three systems. (ii) Closed System It exchanges only energy (not matter) with surroundings.

Reversibility, Irreversibility and Carnot cycle. Irreversible Processes. Reversible Processes. Carnot Cycle

Classification following properties of the system in Intensive and Extensive

Handout 12: Thermodynamics. Zeroth law of thermodynamics

Handout 12: Thermodynamics. Zeroth law of thermodynamics

Chapter 12. The Laws of Thermodynamics

Downloaded from

THERMODYNAMICS. Chapter Twelve MCQ I


Physics 202 Homework 5

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

Chapter 12. The Laws of Thermodynamics. First Law of Thermodynamics

Engineering Thermodynamics. Chapter 5. The Second Law of Thermodynamics

Chapter 1: FUNDAMENTAL CONCEPTS OF THERMODYNAMICS AND VARIOUS THERMODYMIC PROCESSES

1. INTRODUCTION TO REFRIGERATION AND AIR CONDITION

MAHALAKSHMI ENGINEERING COLLEGE

18.13 Review & Summary

Spring_#7. Thermodynamics. Youngsuk Nam.

THERMODYNAMICS CONCEPTUAL PROBLEMS

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

Chapter 16 Thermodynamics

1. Second Law of Thermodynamics

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

Entropy and the second law of thermodynamics

Module - 1: Thermodynamics

The laws of Thermodynamics. Work in thermodynamic processes

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

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

PY2005: Thermodynamics

Distinguish between an isothermal process and an adiabatic process as applied to an ideal gas (2)

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

Free expansion (Joule); Constant U Forced expansion (Joule-Kelvin); Constant H. Joule-Kelvin coefficient - heating or cooling on JK expansion?

1. Second Law of Thermodynamics

Laws of Thermodynamics

Chapter 19. Heat Engines

Reversibility. Processes in nature are always irreversible: far from equilibrium

Chapter 1: FUNDAMENTAL CONCEPTS OF THERMODYNAMICS AND VARIOUS THERMODYMIC PROCESSES

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

Content 10 Thermodynamics of gases Objectives Objectives 10.1 Heat capacity

THERMODYNAMICS Lecture 5: Second Law of Thermodynamics

THERMODYNAMICS MODULE - 3 OBJECTIVES. Notes

Heat Machines (Chapters 18.6, 19)

T s change via collisions at boundary (not mechanical interaction)

Chapter 19. First Law of Thermodynamics. Dr. Armen Kocharian, 04/04/05

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

Lecture 7, 8 and 9 : Thermodynamic process by: Asst. lect. Karrar Al-Mansoori CONTENTS. 7) Thermodynamic process, path and cycle 2

Entropy & the Second Law of Thermodynamics

12 The Laws of Thermodynamics

CHAPTER 6 THE SECOND LAW OF THERMODYNAMICS

10. Heat devices: heat engines and refrigerators (Hiroshi Matsuoka)

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

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

Niraj Sir THERMODYNAMICS

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

The First Law of Thermodynamics

Thermodynamics. 1.1 Introduction. Thermodynamics is a phenomenological description of properties of macroscopic systems in thermal equilibrium.

UNIT I Basic concepts and Work & Heat Transfer

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

Physics 5D PRACTICE FINAL EXAM Fall 2013

October 18, 2011 Carnot cycle - 1

CH 15. Zeroth and First Law of Thermodynamics

Chapter 5. The Second Law of Thermodynamics (continued)

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

Lecture 2 Entropy and Second Law

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

CARNOT CYCLE = T = S ( U,V )

Kinetic Theory continued

Chapter 19. Heat Engines

Lecture Outline Chapter 18. Physics, 4 th Edition James S. Walker. Copyright 2010 Pearson Education, Inc.

I.D The Second Law Q C

Chapter 11 Heat Engines and The Second Law of Thermodynamics

Kinetic Theory continued

Part III Second Law of Thermodynamics

Boundary. Surroundings

Irreversible Processes

Process Nature of Process

Entropy and the Second and Third Laws of Thermodynamics

Physics 207 Lecture 27. Lecture 26. Chapters 18, entropy and second law of thermodynamics Chapter 19, heat engines and refrigerators

Lecture 2.7 Entropy and the Second law of Thermodynamics During last several lectures we have been talking about different thermodynamic processes.

Reversible Processes. Furthermore, there must be no friction (i.e. mechanical energy loss) or turbulence i.e. it must be infinitely slow.

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

Heat Engines and the Second Law of Thermodynamics

Heat What is heat? Work = 2. PdV 1

Irreversible Processes

Basic thermodynamics. heat to the high temperature reservoir.

BME-A PREVIOUS YEAR QUESTIONS

Lecture 10: Heat Engines and Reversible Processes

A thermodynamic system is taken from an initial state X along the path XYZX as shown in the PV-diagram.

VEER SURENDRA SAI UNIVERSITY OF TECHNOLOGY BURLA, ODISHA DEPARTMENT OF MECHANICAL ENGINEERING ENGINEERING THERMODYNAMICS.

Lecture 44: Review Thermodynamics I

T H E R M O D Y N A M I C S M E

Lecture Notes Set 4c: Heat engines and the Carnot cycle

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

S6. (a) State what is meant by an ideal gas...

Classes at: - Topic: Thermodynamics. = E v. = G f T 1

CHAPTER 8 ENTROPY. Blank

Transcription:

CHAPER - HERMODYNAMICS ONE MARK QUESIONS. What is hermodynamics?. Mention the Macroscopic variables to specify the thermodynamics. 3. How does thermodynamics differ from Mechanics? 4. What is thermodynamic equilibrium? 5. Give the meaning of the term adiabatic wall. 6. Give the meaning of diathermic wall. 7. Name the scientist who formulated. Zeroth law of thermodynamics. 8. Write the significance of Zero th law of thermodynamics? 9. Mention the factor on which internal energy depends on. 0. Mention the modes of changing internal energy.. What are thermodynamic state variables?. Mention the modes of energy transfer to a system. 3. Define Internal energy. 4. Mention the principle of first law of thermodynamics 5. Define specific heat capacity of water. 6. Write the value of specific heat capacity of water. 7. Define one calorie. 8. What is equation of state? 9. Give the equation of state of ideal gas. 0. What is isothermal curve?. Mention the kinds of thermodynamic state variables.. Give an example of extensive state variable. 3. Give an example of intensive state variable. 4. What is quasi-static process? 5. What is isothermal process? 6. What is isobaric process? 7. What is isochoric process?

8. What is adiabatic process? 9. When does gas absorb heat and does work during isothermal process? 30. When does gas release heat and work is done by the surrounding? 3. Mention the condition for work done by the gas in an adiabatic process. 3. Mention the condition for work done on the gas in an adiabatic process. 33. What is the work done in isochoric process? 34. Mention the expression for work done in isobaric process. 35. What is the work done in cyclic process? 36. What is heat engine? 37. Define the efficiency of a heat engine. 38. Mention the expression for coefficient of performance of refrigerator 39. Mention the expression for amount of heat released to the heat reservoir. 40. What is Heat pump? 4. Mention the thermodynamic process in which highest efficiency is possible. 4. Mention the thermodynamic process in which lowest efficiency is possible. 43. What is Carnot engine? 44. Who designed the Carnot engine? 45. What is Carnot cycle? 46. Name the working substance used in Carnot cycle. WO MARK QUESIONS :. State and explain Zero th law of thermodynamics.. Justify the statement A gas in a given state has a certain amount of work. 3. Justify the statement A gas in a given state has a certain amount of heat 4. State and explain First law of thermodynamics. 5. Explain isothermal process by applying first law of thermodynamics. 6. Explain isobaric process by applying first law of thermodynamics. 7. Write the equation of state for ideal gas. Explain the terms. 8. Show that molar specific heat of solids, C 3R. 9. Mention the two ways of Mechanism of conversion of heat into work. 0. State both forms of second law of thermodynamics.

. According to II law of thermodynamic, what are the limitations of efficiency and co-efficient of performance.. What is reversible process? Give an example. 3. What is irreversible process? Give an example. 4. Mention the causes of irreversibility. QUESIONS CARRIES 4 OR 5 MARKS.. Using first law of thermodynamics, arrive at the relation, C p -C v R.. What is isothermal process? Obtain the equation of isothermal process OR What is isothermal process? Obtain the expression for work done by isothermal process. 3. What is adiabatic process? Obtain the expression for work done in adiabatic process. 4. Explain the features of a heat engine with schematic diagram. 5. Distinguish between isothermal and adiabatic process. 6. Describe the Carnot cycle of operation using P diagram. 7. Discuss the Carnot cycle of operation and deduce the expression for efficiency. 8. What is refrigirator? Explaine the working of refrigerator with schematic diagram. PROBLEMS :. A cylinder with a movable piston contains 3 moles of hydrogen at constant temperature and pressure. he walls of a cylinder are made up of a heat insulator, and the piston is insulated by having a pile of sand on it. By what factor does the pressure of a gas increases if the gas is compressed to half its original volume?. In changing the state of a gas adiabatically from an equilibrium state A to another equilibrium state B, an amount of work equal to.3 J is done on the system. If the gs is taken from state A to B via a process in which the net heat absorbed by the system is 9.35 cal., how much is the network done by the system in the later case? (ake cal 4.9J) 3

3. An electric heater supplies heat to a system at the rate of 0W. If the system performs work at a rate of 75 joules per second. At what rate is the internal energy increasing? 4. A steam engine delivers 5.4 x 0 8 J of work per minute and services 3.6 x 0 9 J of heat per minute from the boiler. What is the efficiency of the engine? How much heat is wasted per minute? 5. A perfect Carnot engine utilizes an ideal gas. he source temperature is 500 K and sink temperature is 375K. If the engine takes 600K cal per cycle from the source, compute: (a) the efficiency of the engine. (b) Work done per cycle. (c) Heat rejected to the sink per cycle. 6. A refrigerator has to transfer an average of 63 J of heat per second from temperature - 0 0 C to 5 0 C. Calculate the average power consumed assuming ideal reversible cycle and no other losses. 7. What is the coefficient of performance ( β ) or a Carnot refrigerator working between 30 0 C and 0 0 C? 8. A certain volume of dry air at NP is allowed to expand 4 times of its original volume under (a) isothermal conditions (b) adiabatic conditions. Calculate the final pressure and temperature in each case.4. 9. In a refrigerator, heat from inside at 77 K is transferred to a room at 300K. How many joules of heat will be delivered to the room for each joule of electric energy consumed ideally? 4

ANSWER O ONE MARK QUESIONS. he branch of physics that deals with the concept of heat and temperature and inter-conversion of heat and other forms of energy.. Pressure, olume, emperature, mass and composition. 3. Mechanics deals with motion of particles under the action of forces, while hermodynamics concerned with internal Microscopic state of the body. 4. he system is said to be in the hermodynamic equilibrium when the macroscopic variables do not change with time. 5. It is an insulating wall (can be movable) that does not allow flow of energy (heat) from one system to another. 6. It is a conducting wall that allows energy flow (heat) from one system to another. 7. R.H. Fowler in 93. 8. It signifies the concept of temperature. 9. It depends on state of system 0. Heat and work.. ariables like Pressure, emperature, internal Energy which determines the hermodynamic state are called hermodynamics state variables.. Heat and work. 3. Internal energy is the sum of molecular kinetic and potential energies in the frame of reference relative to which the centre of mass of the system is at rest. 4. Law of conservation of energy. 5. Specific heat capacity of water is equal to the amount of heat required to raise the temperature of kg of water by K. 6. 486Jkg - K - 7. One calorie is defined to be the amount of heat required to raise the temperature of g of water from 4.5 0 C to 5.5 0 C. 8. he relation connecting between state variables is called equation of state. 5

9. P R for moles of ideal gas. 0. he pressure- volume curve for fixed temperature is called isothermal curve.. Extensive variables and intensive variable.. olume, Mass, Internal Energy etc. 3. Pressure, emperature, Density etc. 4. he process in the system the variables (P) changes vary slowly so that the system remain in thermal and mechanical equilibrium with its surrounding throughout is called quasi-static process. 5. A process in which the temperature of the system is kept constant throughout is called isothermal process. (i.e. 0) 6. A process in which the pressure is kept constant is called isobaric process. (i.e. P0) 7. A process in which the volume is kept fixed is called isochoric process (i.e. 0) 8. A process in which no heat flows between system and its surrounding is called adiabatic process. (i.e. Q 0) 9. during isothermal expansion. 30. during isothermal compression. 3. during adiabatic expansion. 3. during adiabatic compression. 33. Zero Joule (because heat absorbed by the gas is entirely utilized to change its internal energy only). 34. W P( - ) 35. otal work done is equal to total heat absorbed. 36. Heat engine is a device by which a system is made to undergo a cyclic process that results in conversion of heat into work. 37. It is defined as the ratio of useful work done (W) to the heat input (Q ) 6

38. α Q W 39. Q W + Q 40. A device used to increase the temperature of a system is known as heat pump. 4. Reversible process. 4. Irreversible process. 43. A reversible heat engine operating between two temperatures is called a Carnot engine. 44. N.L. Sodi Carnot - a French Engineer. 45. he sequence of steps constituting one cycle of operation of Carnot Engine is called Carnot cycle. 46. Ideal Gas. WO MARK QUESIONS :. Statement: two systems in thermal equilibrium with a third system separately are in thermal equilibrium with each other. Explanation : If A and B are two systems are equilibrium with system C then A C and B C. his implies that A B i.e. the system A and B are also in thermal equilibrium. hus we arrived the concept of temperature formally via the Zero th Law.. No, A gas in a given state has a certain amount of internal energy is a meaningful statement. 3. No, A certain amount of heat is supplied to the system or a certain amount of work was done by the system is a meaningful statement. 4. When an amount of heat energy is supplied to the system, part of it increases internal energy of the system and remaining is utilized by the system to do work. Explanation: If Q is heat supplied to the system by the surrounding, u is change in internal energy of the system and w is work done by the system on the surrounding. hen according to first law of thermodynamics Q u + w 7

* It is the principle of the conservation of energy. 5. For isothermal process temperature remains constant i.e. u 0. herefore according to first law of thermodynamics Q w Heat supplied to the system is used up entirely by the system in doing work on environment. 6. For isobaric process pressure remains constant. W P i.e. work done by the system. hen we write first law of thermodynamics as Q u + P. 7. For an ideal gas, the equation of state is P µ R., where P is pressure, is volume, R is universal gas constant and is absolute temperature and µ is number of moles. 8. Consider a solid of N atoms, each vibrating about its mean position. An oscillator in one dimension has average energy of x ½ k B k B. For a mole of a solid. he total energy, U 3k B x N A 3 R At constant pressure, Q u + P U Since for a solid is negligible. herefore, molar specific heat. Q U C 3R C 3R 9. *he system is heated by an external furnace as in steam engine. *he system is heated internally by an exothermic chemical reaction as in internal combustion engine. 0. Kelvin-Planck statement: No process is possible whose sole result is the absorption of heat from a reservoir and the complete conversion of the heat into work Clausius statement: No process is possible whose sole result is the transfer of heat from a colder object to a hotter object. * It can be proved that the two statements above are completely equivalent.. According the II Law, *efficiency never be unity or never exceed unity. *Coefficient of performance never be infinite.. A process is reversible only if it is quasi-static and non dissipative. Eg. A quasi-static isothermal expansion of an ideal gas in a cylinder fitted with a frictionless movable piston is reversible process. 8

3. A process which takes the system to the non equilibrium state is called irreversible process. *It can t be retraced in the reverse direction. Eg. he Free expansion of gas. he combustion reaction of mixture of petrol and air, ignited by a spark. 4. Friction, viscosity and other dissipative effect. QUESIONS CARRIES 4 OR 5 MARKS.. According to st law of thermodynamics Q u + P, consider one mole of ideal gas, if Q is the amount of heat absorbed at constant volume then 0. and molar specific heat of gas at constant volume becomes Q U U Cv --------------- Where the subscript v is dropped in the last step, since U of an ideal gas depends only on temperature. If Q is the amount of heat absorbed at constant pressure then C p Q p U p + P p or Q U C p + P --------------- Since U of an ideal gas depend only on. For one mole of ideal gas P R which gives P R --------------- 3 p substituting equations and 3 in equation, we get C p C v + R > C p - C v R [his relation is called Mayer s relation. Where R is universal gas constant and C p and C v are molar specific heat capacities of an ideal gas at constant pressure and constant volume respectively.]. A thermodynamic process which takes place at a constant temperature is called an isothermal process. 9

For an ideal gas in isothermal process, the equation of state for mole of gas is P constant > P µ R he gas under goes isothermal expansion from (P ) to (P ), at any intermediate stage with pressure P, and volume changes from to + hen work done W P. aking ( 0) and summing the quantity W over the entire process. W W Pd d µr µrln µrln his is the expression for work done during isothermal expansion. 3. A thermodynamic process during which no heat enters or leaves the system is known as an adiabatic process. Consider µ moles of ideal gas undergoing a adiabatic expansion from to. For adiabatic process P constant, where is the ratio of specific heats at C p constant pressure and at constant volume. i.e. C If gas under goes change in its state adiabatically from (P, ) to (P, ) hen P P he work done in adiabatic change of an ideal gas from the sate (P,, ) to the state (P,, ) is v W Pd constant x + d cons tan t x 0

cons tan t x ( ) From equation () the constant is P or P then W W cons tan t x ( ) P P x ( ) or W ( P P ) ( ) µ R( ) µ R( ) W is the expression for work done by the gas in adiabatic process. 4. Heat engine is a device by which a system is made to undergo a cyclic process that results in conversion of heat to work. * It consists of a working substance-the system. Eg. a mixture of fuel vapour and air in a gasoline. * he working substance goes through a cycle consisting of several processes. In some of these processes, it absorbs a total amount of heat Q from an external reservoir at some high temperature. * In some other processes of the cycle, the working substance releases a total amount of heat Q to an external reservoir at some lower temperature. * he work done (W) by the system in a cycle is transferred to the environment via some arrangement like cylinder with piston system and is as shown in fig. W Hot Reservior Q Q Cold Reservior he cycle is repeated again and again to get useful work for some purpose.

5.. emperature remains constant. Heat energy exchange is 0.. It is a slow process. It is sudden process. 3. It is represented by 3. It is represented by equation P Const. equation P constant. 4. Slope of P graph is 4. Slope of P graph is comparatively small. comparatively large( time) 5. Work done W µ Rln 5. W µ R ( ) 6. Carnot cycle consists of two adiabatic and two isothermal processes, all are reversible. o describe the carnot cycle, assume the working substance or ideal gas contained in a cylinder fitted with a movable piston. * he cylinder walls and piston are non-conducting. Step : Isothermal expansion of the gas taking its state from (P,, ) to (P,, ). hus the work done ( w ) by the gas on the environment is w Q ln R µ --------- () Step 3 : Adaibatic expansion of the gas from (P,, ) to (P 3, 3, ). hus the work done ( w 3 ) by the gas is µ R( ) w 3 --------- () Step 3 4 : Isothermal compression of the gas taking its state from (P 3, 3, ) to (P 4, 4, ). Heat released (Q ) by the gas to the reservior at temperature. hus the work done ( w 3 4 ) on the gas by the environment is 3 w 3 4 Q µ R ln --------- (3) 4

Step 4 : Adaibatic compression of the gas from (P 4, 4, ) to (P,, ). hus the work done ( w 4 ) on the gas is µ R( ) w 4 --------- (4) From equation () to (4) total work done by the gas in one complete cycle W w + w 3 - w3 4 - w 4 W µ R ln - µ R ln he efficiency of the carnot engine is η W Q Q Q 3 4 η 3 ln 4 ln ------------(5) Step 3 : is an adiabatic process hen 3 i.e. 3 /( ) ------------(6) Similarly in Step 4 is an adiabatic process hen 4 i.e. 4 /( ) ------------(7) From equations (6) and (7) we get 3 ------------(8) 4 3

From equations (8) and (5) we get η ------------(9) is the expression for efficiency of carnot engine. Note : (i) he interesting aspect of η of Carnot engine is that it is independent of the nature of the working substance. But Carnot used an ideal gas operation which is not strictly followed by real gases or fuels. (ii) heoretically η can be 00%. (iii) he efficiency of Carnot s ideal engine depends only on the temperatures of the source and the sink. (iv) Efficiency of any reversible engine working between same two temperatures is same. 7. Discuss the Carnot cycle of operation and deduce the expression for efficiency. Carnot engine is works on the principle of Carnot cycle made up of four stages are represented as shown in (P) diagram. ) Isothermal expansion (LM): he gas is allowed to expand isothermally. During the expansion gas absorb an amount of heat Q from the source at, ()Adiabatic expansion (MN): he gas is allowed to expand adiabatically till the temperature of gas falls to, the temperature of the sink, (3) Isothermal compression (NO): he gas is compressed slowly at constant temperature. During this process a certain amount of heat Q is rejected into the sink, (4) Adiabatic compression (OL): he gas is further compressed adiabatically till it returns to its initial state L. he cycle of operations, LM, MN, NO and OL is called the Carnot cycle. It is represented by the closed loop LMNOL. P L (,P, ) O 4 4 (,P, ) M (,P, ) N 3 3 (,P, ) 4

8. A refrigerator is the reverse of a heat engine. Here the working substance extracts heat Q from the cold reservoir at temperature, some external work W is done on it and heat Q is released to the hot reservoir at temperature. W Hot Reservior Q Q Cold Reservior In a refrigerator the working substance (usually, in gaseous form) goes through the following steps: (a) Sudden expansion of the gas from high to low pressure which cools it and converts it into a vapour-liquid mixture, (b) Absorption by the cold fluid of heat from the region to be cooled converting it into vapour. (c) Heating up of the vapour due to external work done on the system, and (d) Release of heat by the vapour to the surroundings, bringing it to the initial state and completing the cycle. he coefficient of performance (a) of a refrigerator is given by Q α W SOLUIONS O HE PROBLEMS :. since the process is adiabatic P P, 7 / 5 for hydrogen Factor by which the pressure of the gas increases > P P P P > ( ) 7/ 5 5

. Since, the system is going from A to B and then back to A, it is undergoing a cyclic change. Now in cyclic change there is no change in internal energy U 0. From first law of thermodynamics Q U + W W [ Q U 0] he amount of heat absorbed by the system Q 9.35cal -.3J (9.35 x 4.9 -.3)J 6.87J he net work done by the system W 6.87J 3.Given : heat supplied per second, Q 00J Work done by the system per second W 75J Increase in internal energy per second U? From the first law of thermodynamics Q U + W U Q W U 00J 75 J U 5J per second. or U 5 W 4. Given : Q heat absorbed from the boiler per minute 3.6 x 0 9 J W work done per minute by the steam engine 5.4 x 0 8 J Q heat wasted / rejected per minute? percentage efficiency of the heat engine? W We have η% x00 Q 8 5.4x0 J 9 3.6x0 J x 00 3 0 x 00 5% Also heat absorbed Q W+Q heat wasted Q Q - W 36 x 0 8-5.4 x 0 8 30.6 x 0 8 J/min. 3.06 x 0 9 J/m 3. x 0 9 J/min. 6

5. Given : 500K 375K Q Heat absorbed per cycle 600K cal. We have η η 500-375 5 500 500 0.5 η % 0.5 x 00 5% Suppose W work done per cycle from the relation, W η we get Q W η Q 0.5 x 600 K cal. 50K cal 50 x 0 3 x 4. J 6.3 x 0 5 J. Suppose Q heat rejected to the sink. hen W Q - Q, we get Q Q -W 600-50 450 K cal. 6. 5 + 73 98 K -0 + 73 63 K Q 63 JS - We have Q Q Q 98 x Q x63 63 Q 98Js - Average power consumed Q - Q (98-63) Js - 35 W 7

7. Given : 00C 73 K 300C 73 + 30 303 K β? We have β 73 73 β 9. 303 73 30 8. Given : 4 P 76cm of Hg. P?.4 73 K? For isothermal expansion P P P P 76 9 cm of Hg. 4 As the process is isothermal, therefore the final temperature will be the same as the initial temperature. i.e. 73K For Adiabatic expansion: P P P P P 76 4.4 76 x (0.5).4 0.9 cm of Hg. 8

Also : 73 0.4 56.8 K (4) 73 4.4 9. 77K, 300 K, Q?, W J We have β 77 77 β. 04 300 77 3 Also β W Q Q We get β Q Q.04 J Now W Q - Q or Q W + Q i.e. otal heat delivered to the room, Q +.04 3.04 J * * * * * 9