Physics 53. Thermal Physics 1. Statistics are like a bikini. What they reveal is suggestive; what they conceal is vital.

Similar documents
18.13 Review & Summary

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

Chapter 19 The First Law of Thermodynamics

Honors Physics. Notes Nov 16, 20 Heat. Persans 1

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

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

Introduction to thermodynamics

CHAPTER 17 WORK, HEAT, & FIRST LAW OF THERMODYNAMICS

Chapter 18 Heat and the First Law of Thermodynamics

The First Law of Thermodynamics

ADIABATIC PROCESS Q = 0

Lesson 12. Luis Anchordoqui. Physics 168. Tuesday, November 28, 17

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

NOTE: Only CHANGE in internal energy matters

Lecture 7: Kinetic Theory of Gases, Part 2. ! = mn v x

More Thermodynamics. Specific Specific Heats of a Gas Equipartition of Energy Reversible and Irreversible Processes

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

Phase Changes and Latent Heat

Monday, October 21, 13. Copyright 2009 Pearson Education, Inc.

17-1 Ideal Gases. Gases are the easiest state of matter to describe - All ideal gases exhibit similar behavior.

Thermodynamics. Thermodynamics is the study of the collective properties of a system containing many bodies (typically of order 10 23!

Physics 123 Thermodynamics Review

Chapter 15 Thermal Properties of Matter

Physics 2: Fluid Mechanics and Thermodynamics

Internal Energy (example)

Chapter 18 Temperature, Heat, and the First Law of Thermodynamics. Thermodynamics and Statistical Physics

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

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

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

Heat. Heat is energy transferred between a system and its surroundings because of a temperature difference between them.

MME 2010 METALLURGICAL THERMODYNAMICS II. Fundamentals of Thermodynamics for Systems of Constant Composition

First Law of Thermodynamics

First Law of Thermodynamics Basic Concepts

PHYSICS 715 COURSE NOTES WEEK 1

Kinetic Theory continued

Temperature and Heat. Ken Intriligator s week 4 lectures, Oct 21, 2013

THERMODYNAMICS. Zeroth law of thermodynamics. Isotherm

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

Hence. The second law describes the direction of energy transfer in spontaneous processes

, is placed in thermal contact with object B, with mass m, specific heat c B. and initially at temperature T B

The first law of thermodynamics continued

Kinetic Theory continued

Ch. 19: The Kinetic Theory of Gases

Enthalpy and Adiabatic Changes

3. First Law of Thermodynamics and Energy Equation

Physics 2: Fluid Mechanics and Thermodynamics

Lecture 4: The First Law of Thermodynamics

16-1. Sections Covered in the Text: Chapter 17. Example Problem 16-1 Estimating the Thermal Energy of a gas. Energy Revisited

Chapter 10 Temperature and Heat

Chapter 17. Temperature. Dr. Armen Kocharian

Chapter 14 Temperature and Heat

Physics 121, April 24. Heat and the First Law of Thermodynamics. Department of Physics and Astronomy, University of Rochester

Physics 121, April 24. Heat and the First Law of Thermodynamics. Physics 121. April 24, Physics 121. April 24, Course Information

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

First Law of Thermodynamics

CHAPTER 3 TEST REVIEW

19-9 Adiabatic Expansion of an Ideal Gas

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

- Apply closed system energy balances, observe sign convention for work and heat transfer.

Temperature, Energy and the First Law of Thermodynamics. 8.01t Nov 29, 2004

Concepts of Thermodynamics

Chapter 10. Thermal Physics. Thermodynamic Quantities: Volume V and Mass Density ρ Pressure P Temperature T: Zeroth Law of Thermodynamics

Specific Heat of Diatomic Gases and. The Adiabatic Process

Thermodynamics 1 Lecture Note 2

Chapter 12. Temperature and Heat. continued

Chapter 6: The States of Matter

SKMM 2413 Thermodynamics

Topic 3 &10 Review Thermodynamics

First Law of Thermodynamics Second Law of Thermodynamics Mechanical Equivalent of Heat Zeroth Law of Thermodynamics Thermal Expansion of Solids

Chapter 19 Entropy Pearson Education, Inc. Slide 20-1

Chapter 9. Preview. Objectives Defining Temperature. Thermal Equilibrium. Thermal Expansion Measuring Temperature. Section 1 Temperature and

Lecture 2: Zero law of thermodynamics

Chapter 2 Carnot Principle

X α = E x α = E. Ω Y (E,x)

Chapter 6 The States of Matter. Examples of Physical Properties of Three States of Matter

Chapter 17. Work, Heat, and the First Law of Thermodynamics Topics: Chapter Goal: Conservation of Energy Work in Ideal-Gas Processes

Physics Fall Mechanics, Thermodynamics, Waves, Fluids. Lecture 32: Heat and Work II. Slide 32-1

Chapter 14. The Ideal Gas Law and Kinetic Theory

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

Physics 111. Lecture 39 (Walker: 17.6, 18.2) Latent Heat Internal Energy First Law of Thermodynamics May 8, Latent Heats

CHAPTER - 12 THERMODYNAMICS

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

Lecture 5. PHYC 161 Fall 2016

Lecture 24. Ideal Gas Law and Kinetic Theory

Temperature and Its Measurement

MP203 Statistical and Thermal Physics. Jon-Ivar Skullerud and James Smith

Thermodynamic System. A thermodynamic system is a volume in space containing a quantity of matter that is being studied for thermodynamic analysis.

Chapter 10. Thermal Physics

Chapter 18. Temperature, Heat, and the First Law of Thermodynamics Temperature

Energy: 1. Energy is an abstract physical quantity 2. It can be measured only by means of its effect Vikasana - Bridge Course

The Second Law of Thermodynamics (Chapter 4)

Revision Guide for Chapter 13

Physics 123 Unit #2 Review

Work and heat. Expansion Work. Heat Transactions. Chapter 2 of Atkins: The First Law: Concepts. Sections of Atkins

Chemistry. Lecture 10 Maxwell Relations. NC State University

Thermodynamics 2013/2014, lecturer: Martin Zápotocký

Thermal Physics. Temperature (Definition #1): a measure of the average random kinetic energy of all the particles of a system Units: o C, K

Lecture Outline Chapter 17. Physics, 4 th Edition James S. Walker. Copyright 2010 Pearson Education, Inc.

Thermodynamics (Lecture Notes) Heat and Thermodynamics (7 th Edition) by Mark W. Zemansky & Richard H. Dittman

Chapter 19 Entropy Pearson Education, Inc. Slide 20-1

Transcription:

Physics 53 Thermal Physics 1 Statistics are like a bikini. What they reveal is suggestive; what they conceal is vital. Arthur Koestler Overview In the following sections we will treat macroscopic systems that are in thermal equilibrium. Most of our discussion will center on the behavior of gases. We will use appropriate macroscopic variables, some of which are already familiar, such as density, volume and pressure. We will usually assume the CM of the system is at rest, and that molecular velocities are randomly distributed as to direction, so there is no bulk flow or velocity field to consider. There may be energy (kinetic or potential or both) internal to the molecules themselves, if they are not monatomic. The total kinetic energy of the random molecular motion, plus any energy the molecules may have internal to themselves, constitutes the internal energy of the system. This is one of the new macroscopic variables we will use in our description. Thermal equilibrium, temperature and the Zeroth Law Macroscopic variables used to describe the state of a system in thermal equilibrium are called state variables. Density, volume and pressure are state variables, as is internal energy. We will introduce two more as we go along: temperature and entropy. What is meant by thermal equilibrium is this: If the system is in thermal equilibrium, state variables all have definite values. Since the state variables all represent averages of some kind, what it means to have a definite value is that the fluctuations which might make the average uncertain are small enough to be ignored. In a statistical situation, such fluctuations are generally inversely proportional to the number of particles. In systems of macroscopic size that number (roughly Avogadro s number) is extremely large, so the fluctuations are tiny. Most of the possible situations a system may be in are not states of thermal equilibrium. Nevertheless, it is an experimental fact that a system left to itself evolves toward thermal equilibrium. (How that happens is still not fully understood in detail.) The PHY 53 1 Thermal Physics 1

time it takes for a non-equilibrium state to evolve to equilibrium is called the relaxation time. It varies from case to case, but is often quite short by human standards. Two macroscopic systems can exchange energy with each other. This exchange can be accomplished by collisions among particles at a common interface, or by other methods such as emission and absorption of electromagnetic radiation. If energy exchanges can take place, we say the systems are in thermal contact. Such exchanges generally disrupt, at least temporarily, the states of equilibrium of the two systems. It may happen, however, that two systems brought into thermal contact undergo no disruption of equilibrium in either system. Then we say the systems are in equilibrium with each other. The properties of this mutual thermal equilibrium constitute a fundamental law: Zeroth Law of thermodynamics If systems A and B are both in thermal equilibrium with system C, then they are also in equilibrium with each other. This principle is the basis for the state variable called temperature. Two systems in equilibrium with each other are said to have the same temperature. If two systems with different temperatures are brought into thermal contact, there is exchange of energy until they come to mutual equilibrium at the same (new) temperature. Temperature is a scalar quantity. It is defined operationally by its measurement, using a device called a thermometer. When this (small) device is placed in thermal contact with the (large) system in question, some energy is exchanged between the two. (Because the thermometer is small, this energy exchange does not change appreciably the state of the large system.) Some physical aspect of the thermometer (for example, the length of a column of liquid) changes in an observable way on account of the energy exchange; when this aspect stops changing we know the system and the thermometer are in equilibrium. By calibrating the changes in the thermometer one makes a scale of temperatures. The first thermometer and scale was made by Fahrenheit around 1700. How is temperature related to average behavior of the microscopic states? We will find that temperature is one measure of the average energy of (random) motion of the molecules in the system. The ideal gas law For a gas the most commonly used state variables are pressure (P), volume (V) and temperature (T). For reasons to be made clear later, the temperature of a gas is usually specified using a scale with the lowest possible temperature chosen as zero. The most popular of these scales is that due to Lord Kelvin (William Thomson), which has 100 PHY 53 2 Thermal Physics 1

units ( Kelvins, denoted by K) between the ice point and the steam point of water. In this scale the absolute zero of temperature is approximately 273 K below the ice point. Pressure, volume and temperature are not all independent of each other. An equation relating them is called an equation of state. It is generally written in the form T = f ( P,V ). Much research has been done to find the function f (P,V) appropriate to particular gases. In the late 17th century it was found that for a wide variety of gases, at conditions of pressure and temperature easily obtainable in the technology of that time, there is a simple and universal function that describes them all. It is f (P,V) = (const) PV. This formula is called the ideal gas law. In SI units, it is usually written in either of two equivalent forms: Ideal gas law PV = NkT PV = nrt In the first form N is the number of molecules in the gas and k is a universal constant, called Boltzmann's constant, which in SI units is k = 1.38 10 23. The second form specifies the quantity of gas in terms of the number of moles n, and R is the universal gas constant. R = 8.31 in SI units. The two forms are related through Avagadro s number N A, the number of molecules per mole. We have N = nn A and so R = N A k. Experimentally N A 6.02 10 23. The ideal gas law is an approximation that gives good results for gases that are not very dense, at temperatures and pressures near those in which we live. Internal energy The internal energy of a system, denoted by E int, consists of the total energy of random motion of the particles, plus any energy associated with internal structure of the particles, such as rotation and vibration about their individual CM. The notation given here for internal energy is not standard; more commonly it is denoted by U. We use a notation that avoids confusion with potential energy, since internal energy also includes the kinetic energy of random motion of the molecules of the system. In terms of the average energy E av of the particles, E int = NE av, where N is the total number of particles. Since E av generally depends on the temperature, E int depends on T. For an ideal gas it depends only on T. PHY 53 3 Thermal Physics 1

In general, both of these energies increase with increasing T. The internal energy of a system can be changed by transfers of energy in or out of the system, which can be accomplished by a variety of methods. Two are of special importance: The system can be put into thermal contact with another system at a different temperature. Energy will be transferred from the system whose particles have higher average energy (higher T) to the one with lower average energy (lower T). The energy transferred this way is called heat, denoted by Q, and the process is called heat flow. We will discuss later some of the details of this kind of process. Energy can be transferred through work done by external forces. If external forces do positive work on the system, then (assuming no other energy transfers are occurring) the internal energy increases. If the system does positive work on something external to it then the internal energy decreases. An example of work done is the motion of a piston in a cylinder filled with gas. If an external force pushes the piston inward to reduce the volume, the internal energy of the gas increases. If the gas expands, pushing the piston outward against the external force, the internal energy of the gas decreases. The First Law of thermodynamics The energy balance in this situation is described by an important law: First Law of thermodynamics If heat dq is taken into a system, while the system does work dw, then the internal energy of the system changes by the amount de int = dq dw. Although all the quantities in this law have the dimensions of energy, they have quite different meanings: Heat and work are energy in transit, not energy a system possesses. They are not state variables. The amount of heat flow or work done in changing the state of the system depends not only on the initial and final states of the system, but on what process was used to make the change. Internal energy, on the other hand, is a state variable. The change of internal energy depends only on the initial and final states of the system, not at all on the process. The logical content of the 1st law is often described as the assertion that internal energy exists and is a state variable. PHY 53 4 Thermal Physics 1

Thermal processes A given change in internal energy can result from many different combinations of heat flow and work done. Each such combination is a different thermal process. There are a few simple processes of importance in our analysis: Constant volume For a gas, this usually means dw = 0. Constant pressure If the volume changes by dv, then the work done by the system is dw = PdV. Constant temperature. If E int depends only Isothermal on T, then de int = 0 and dq = dw. This is the case for an ideal gas. Adiabatic No heat flow: dq = 0. Specific heats If heat flows into a system its temperature increases unless the system loses as much energy through work done as the heat flow brings in, or unless a change of phase (discussed below) is taking place. The amount of heat necessary to raise the temperature by one unit (in SI units, 1 K) is called the heat capacity of the system, denoted by C. Clearly this depends on how large the system is (how many particles it contains) as well as what kind of substance is involved. To eliminate the dependence on quantity it is common to define the heat capacity for a unit quantity of matter. This is called the specific heat of the substance, denoted by c. Heat capacity and specific heat both depend on the process by which the heat is taken in. One often attaches subscripts to the symbols to denote the process used. For example, if the volume is kept constant, the specific heat is denoted by c V. If the pressure is kept constant we have c P. The general definition of specific heat is 1 dq Specific heat c (process) = (quantity) dt (process) PHY 53 5 Thermal Physics 1

For a gas it is common to use the number of moles to measure the quantity, and the specific heat is then the heat capacity per mole (often called the molar heat capacity). For solids or liquids it is more common to use the mass as the measure of quantity. In practice, one often rewrites the definition of c in the following manner: (dq) (process) = (quantity) c (process) dt This allows for easy use in conjunction with the 1 st law. Changes of phase When a substance melts, changing from solid to liquid, we say its phase has changed. The strong bonds of a solid have been converted into the weaker interactions of nearest neighbors in a liquid. This requires input of energy. Similarly, when a liquid boils or evaporates, becoming a gas, the interactions between particles have been almost completely eliminated, so input of energy is again required. The input energy needed to make these phase changes, without changing the temperature, is called the latent heat. It is denoted by L f for the case of melting ( fusion ) and L v for the case of vaporization. It is generally specified per unit mass of the material, so the amount of heat necessary to make the phase change takes the form Q = ml, where m is the mass of the substance in question. Specific heats of an ideal gas We have mentioned the specific heats of a gas for the cases of constant pressure and constant volume. In the ideal gas approximation, there is a simple relation between these quantities. From the 1st law it follows that if the volume is kept constant (no work is done) then dq V = de int. Since from the definition of c V we have dq V = nc V dt, we find a very useful relation for ideal gases: de int = nc V dt. Since both of the variables in this equation are state variables, this is a general relation, independent of the process. It allows us to write a very useful form of the 1st law that applies to ideal gases: PHY 53 6 Thermal Physics 1

First Law for ideal gas dq = nc VdT + dw Despite the appearance of c V in this relation, it holds for any process, not just one at constant volume. Now consider input of heat dq at constant pressure. This is related to c P by dq = nc P dt. But if the pressure is constant, then we have from the ideal gas law that nrdt = d(pv) = PdV = dw. The 1st law then gives dq P = de int + dw, or nc P dt = nc V dt + nrdt. This reveals a simple relation between the specific heats: Specific heats of ideal gas c P = c V + R Adiabatic Processes for Ideal Gases In an adiabatic process dq = 0, so the 1st law says that de int + dw = 0. For an ideal gas, de int = nc V dt and dw = PdV. Using the ideal gas law we see that nrdt = d(pv) = PdV + VdP. Using c V = c P R and a little algebra, we have c P c V dv V + dp P = 0. Introducing the notation γ = c P /c V and integrating, we have γ lnv + ln P = const. This give the ideal gas formula for adiabatic processes: Adiabatic process for ideal gas PV γ = const., where γ = c P /c V PHY 53 7 Thermal Physics 1

P-V diagrams We have seen that for a gas only two of the variables P,V,T are independent. This means that a point on a plot of P vs. V (called a P-V diagram) corresponds to a definite value of T as well. In dealing with equilibrium states of a gas, it is thus sufficient to specify such a state by a point on a P-V diagram. If the system moves to a different equilibrium state, the point on the P-V diagram correspondingly moves. If the process by which the change was made involves only infinitesimal changes such that all the intermediate states are also equilibrium states, then we can plot the process as a continuous curve on the P-V diagram. This would actually require the process to be infinitely slow, so we are dealing with a mathematical idealization, which gives a good approximation in many cases. It is called the quasi-static approximation. If the volume of the gas changes by dv while pressure P is applied, then the work done by the gas is dw = PdV. For a finite change in volume the work is given by W(a b) = PdV. Here a and b represent equilibrium states, and thus points on the P-V diagram. The work done by the gas is the area under the curve on a P-V diagram. It is positive if the volume increases. In many applications we will be interested in repetitive processes such that the system returns to its original state. These are cyclic processes. If such a process is quasi-static, the curve representing it on the P-V diagram is a closed curve, and the total work done per cycle is the area enclosed by the curve. The special processes listed earlier are represented by curves on the P-V diagram. Constant pressure is represented by a horizontal line. Constant volume is represented by a vertical line. No work is done. Isothermal (T = constant). For an ideal gas we find P = (const.)/v. This is a hyperbola on a P-V diagram, asymptotic to the axes. Adiabatic (dq = 0). We found earlier that for this process involving an ideal gas, PV γ = const., where γ stands for the ratio c P /c V. On a P-V diagram this is similar to the isothermal curve, but it has steeper slope since γ > 1. The figure below shows these curves. b a PHY 53 8 Thermal Physics 1