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Sample Problem Setting Pa � Pd and solving for T4 yield Letting Ld � 2.0La and kd � 5.0ka, and inserting the known temperatures, we find � �8.0°C. (Answer) T4 � ka(2.0La) (5.0ka)La (25�C � 20�C) � (�10�C) T4 � kaLd kdLa (T1 � T2) � T5. Thermal conduction through a layered wall Figure 18-22 shows the cross section of a wall made of white pine of thickness La and brick of thickness Ld (� 2.0La), sandwiching two layers of unknown material with identical thicknesses and thermal conductivities. The thermal conductivity of the pine is ka and that of the brick is kd (� 5.0ka). The face area A of the wall is unknown. Thermal conduction through the wall has reached the steady state; the only known interface temperatures are T1 � 25°C, T2 � 20°C, and T5 � �10°C. What is interface temperature T4? (1) Temperature T4 helps determine the rate Pd at which en- ergy is conducted through the brick, as given by Eq. 18-32. However, we lack enough data to solve Eq. 18-32 for T4. (2) Because the conduction is steady, the conduction rate Pd through the brick must equal the conduction rate Pa through the pine.That gets us going. Calculations: From Eq. 18-32 and Fig. 18-22, we can write Pa � kaA T1 � T2 La and Pd � kdA T4 � T5 Ld . Fig. 18-22 Steady-state heat transfer through a wall. Indoors Outdoors (a) (b) (d)(c) La Lb Lc Ld ka kb kc kd T1 T2 T3 T4 T5 The energy transfer per second is the same in each layer. KEY I DEAS Additional examples, video, and practice available at WileyPLUS 497R EVI EW & S U M MARY PART 2 HALLIDAY REVISED Thermal radiation is involved in the numerous medical cases of a dead rat- tlesnake striking a hand reaching toward it. Pits between each eye and nostril of a rattlesnake (Fig. 18-21) serve as sensors of thermal radiation. When, say, a mouse moves close to a rattlesnake’s head, the thermal radiation from the mouse trig- gers these sensors, causing a reflex action in which the snake strikes the mouse with its fangs and injects its venom. The thermal radiation from a reaching hand can cause the same reflex action even if the snake has been dead for as long as 30 min because the snake’s nervous system continues to function. As one snake ex- pert advised, if you must remove a recently killed rattlesnake, use a long stick rather than your hand. Temperature; Thermometers Temperature is an SI base quantity related to our sense of hot and cold. It is measured with a thermometer, which contains a working substance with a measur- able property, such as length or pressure, that changes in a regular way as the substance becomes hotter or colder. Zeroth Law of Thermodynamics When a thermometer and some other object are placed in contact with each other, they even- tually reach thermal equilibrium. The reading of the thermometer is then taken to be the temperature of the other object.The process provides consistent and useful temperature measurements because of the zeroth law of thermodynamics: If bodies A and B are each in thermal equilibrium with a third body C (the thermome- ter), then A and B are in thermal equilibrium with each other. The Kelvin Temperature Scale In the SI system, tempera- ture is measured on the Kelvin scale, which is based on the triple point of water (273.16 K). Other temperatures are then defined by halliday_c18_476-506v2.qxd 22-10-2009 12:03 Page 497 498 CHAPTE R 18 TE M PE RATU R E, H EAT, AN D TH E F I RST LAW OF TH E R MODYNAM ICS HALLIDAY REVISED of work W done by a gas as it expands or contracts from an initial volume Vi to a final volume Vf is given by (18-25) The integration is necessary because the pressure p may vary dur- ing the volume change. First Law of Thermodynamics The principle of conser- vation of energy for a thermodynamic process is expressed in the first law of thermodynamics, which may assume either of the forms �Eint � Eint, f � Eint,i � Q � W (first law) (18-26) or dEint � dQ � dW (first law). (18-27) Eint represents the internal energy of the material, which depends only on the material’s state (temperature, pressure, and volume). Q represents the energy exchanged as heat between the system and its surroundings; Q is positive if the system absorbs heat and negative if the system loses heat. W is the work done by the sys- tem; W is positive if the system expands against an external force from the surroundings and negative if the system contracts be- cause of an external force. Q and W are path dependent; �Eint is path independent. Applications of the First Law The first law of thermody- namics finds application in several special cases: adiabatic processes: Q � 0, �Eint � �W constant-volume processes: W � 0, �Eint � Q cyclical processes: �Eint � 0, Q � W free expansions: Q � W � �Eint � 0 Conduction, Convection, and Radiation The rate Pcond at which energy is conducted through a slab for which one face is maintained at the higher temperature TH and the other face is maintained at the lower temperature TC is (18-32) Here each face of the slab has area A, the length of the slab (the distance between the faces) is L, and k is the thermal conductivity of the material. Convection occurs when temperature differences cause an en- ergy transfer by motion within a fluid. Radiation is an energy transfer via the emission of electromag- netic energy. The rate Prad at which an object emits energy via ther- mal radiation is Prad � s�AT 4, (18-38) where s (� 5.6704 � 10�8 W/m2 K4) is the Stefan – Boltzmann constant, � is the emissivity of the object’s surface, A is its sur- face area, and T is its surface temperature (in kelvins). The rate Pabs at which an object absorbs energy via thermal radiation from its environment, which is at the uniform temperature Tenv (in kelvins), is Pabs � s�AT4env. (18-39) Pcond � Q t � kA TH � TC L W � � dW � �Vf Vi p dV. use of a constant-volume gas thermometer, in which a sample of gas is maintained at constant volume so its pressure is proportional to its temperature. We define the temperature T as measured with a gas thermometer to be (18-6) Here T is in kelvins, and p3 and p are the pressures of the gas at 273.16 K and the measured temperature, respectively. Celsius and Fahrenheit Scales The Celsius temperature scale is defined by TC � T � 273.15°, (18-7) with T in kelvins.The Fahrenheit temperature scale is defined by (18-8) Thermal Expansion All objects change size with changes in tem- perature. For a temperature change �T, a change �L in any linear di- mension L is given by �L � La �T, (18-9) in which a is the coefficient of linear expansion. The change �V in the volume V of a solid or liquid is �V � Vb �T. (18-10) Here b � 3a is the material’s coefficient of volume expansion. Heat Heat Q is energy that is transferred between a system and its environment because of a temperature difference between them. It can be measured in joules (J), calories (cal), kilocalories (Cal or kcal), or British thermal units (Btu), with 1 cal � 3.968 � 10�3 Btu � 4.1868 J. (18-12) Heat Capacity and Specific Heat If heat Q is absorbed by an object, the object’s temperature change Tf � Ti is related to Q by Q � C(Tf � Ti), (18-13) in which C is the heat capacity of the object. If the object has mass m, then Q � cm(Tf � Ti), (18-14) where c is the specific heat of the material making up the object. The molar specific heat of a material is the heat capacity per mole, which means per 6.02 � 1023 elementary units of the material. Heat of Transformation Heat absorbed by a material may change the material’s physical state—for example, from solid to liq- uid or from liquid to gas.The amount of energy required per unit mass to change the state (but not the temperature) of a particular material is its heat of transformation L.Thus, Q � Lm. (18-16) The heat of vaporization LV is the amount of energy per unit mass that must be added to vaporize a liquid or that must be removed to condense a gas. The heat of fusion LF is the amount of energy per unit mass that mustbe added to melt a solid or that must be re- moved to freeze a liquid. Work Associated with Volume Change A gas may exchange energy with its surroundings through work. The amount TF � 9 5TC � 32�. T � (273.16 K) � limgas:0 p p3 �. halliday_c18_476-506v2.qxd 22-10-2009 12:03 Page 498 529R EVI EW & S U M MARY PART 2 HALLIDAY REVISED Kinetic Theory of Gases The kinetic theory of gases relates the macroscopic properties of gases (for example, pressure and temperature) to the microscopic properties of gas molecules (for example, speed and kinetic energy). Avogadro’s Number One mole of a substance contains NA (Avogadro’s number) elementary units (usually atoms or mole- cules), where NA is found experimentally to be NA � 6.02 � 1023 mol�1 (Avogadro’s number). (19-1) One molar mass M of any substance is the mass of one mole of the substance. It is related to the mass m of the individual molecules of the substance by M � mNA. (19-4) The number of moles n contained in a sample of mass Msam, con- sisting of N molecules, is given by (19-2, 19-3) Ideal Gas An ideal gas is one for which the pressure p, volume V, and temperature T are related by pV � nRT (ideal gas law). (19-5) Here n is the number of moles of the gas present and R is a constant (8.31 J/mol �K) called the gas constant. The ideal gas law can also be written as pV � NkT, (19-9) where the Boltzmann constant k is (19-7) Work in an Isothermal Volume Change The work done by an ideal gas during an isothermal (constant-temperature) change from volume Vi to volume Vf is (ideal gas, isothermal process). (19-14) Pressure, Temperature, and Molecular Speed The pres- sure exerted by n moles of an ideal gas, in terms of the speed of its molecules, is (19-21) where is the root-mean-square speed of the mole- cules of the gas.With Eq. 19-5 this gives (19-22) Temperature and Kinetic Energy The average transla- tional kinetic energy Kavg per molecule of an ideal gas is (19-24) Mean Free Path The mean free path l of a gas molecule is its average path length between collisions and is given by (19-25) where N/V is the number of molecules per unit volume and d is the molecular diameter. � � 1 12 d2 N/V , Kavg � 3 2kT. vrms � A 3RT M . vrms � √(v2)avg p � nMv2rms 3V , W � nRT ln Vf Vi k � R NA � 1.38 � 10�23 J/K. n � N NA � Msam M � Msam mNA . Maxwell Speed Distribution The Maxwell speed distri- bution P(v) is a function such that P(v) dv gives the fraction of molecules with speeds in the interval dv at speed v: (19-27) Three measures of the distribution of speeds among the molecules of a gas are (average speed), (19-31) (most probable speed), (19-35) and the rms speed defined above in Eq. 19-22. Molar Specific Heats The molar specific heat CV of a gas at constant volume is defined as (19-39, 19-41) in which Q is the energy transferred as heat to or from a sample of n moles of the gas, �T is the resulting temperature change of the gas, and �Eint is the resulting change in the internal energy of the gas. For an ideal monatomic gas, (19-43) The molar specific heat Cp of a gas at constant pressure is defined to be (19-46) in which Q, n, and �T are defined as above. Cp is also given by Cp � CV � R. (19-49) For n moles of an ideal gas, Eint � nCVT (ideal gas). (19-44) If n moles of a confined ideal gas undergo a temperature change �T due to any process, the change in the internal energy of the gas is �Eint � nCV �T (ideal gas, any process). (19-45) Degrees of Freedom and CV We find CV by using the equipartition of energy theorem, which states that every degree of freedom of a molecule (that is, every independent way it can store energy) has associated with it—on average—an energy per molecule ( per mole). If f is the number of degrees of free- dom, then Eint ( f /2)nRT and (19-51) For monatomic gases f � 3 (three translational degrees); for diatomic gases f � 5 (three translational and two rotational degrees). Adiabatic Process When an ideal gas undergoes a slow adiabatic volume change (a change for which Q � 0), pVg � a constant (adiabatic process), (19-53) in which g (� Cp/CV) is the ratio of molar specific heats for the gas. For a free expansion, however, pV � a constant. CV � � f2 �R � 4.16f J/mol�K. � � 12RT 1 2kT Cp � Q n �T , CV � 3 2R � 12.5 J/mol�K. CV � Q n �T � �Eint n �T , vP � A 2RT M vavg � A 8RT M P(v) � 4 � M2 RT � 3/2 v2 e�Mv2/2RT. halliday_c19_507-535v2.qxd 28-10-2009 15:56 Page 529 554 CHAPTE R 20 E NTROPY AN D TH E S ECON D LAW OF TH E R MODYNAM ICS One-Way Processes An irreversible process is one that can- not be reversed by means of small changes in the environment.The direction in which an irreversible process proceeds is set by the change in entropy �S of the system undergoing the process. Entropy S is a state property (or state function) of the system; that is, it depends only on the state of the system and not on the way in which the system reached that state. The entropy postulate states (in part): If an irreversible process occurs in a closed system, the entropy of the system always increases. Calculating Entropy Change The entropy change �S for an irreversible process that takes a system from an initial state i to a final state f is exactly equal to the entropy change �S for any reversible process that takes the system between those same two states. We can compute the latter (but not the former) with (20-1) Here Q is the energy transferred as heat to or from the system dur- ing the process, and T is the temperature of the system in kelvins during the process. For a reversible isothermal process, Eq. 20-1 reduces to (20-2) When the temperature change �T of a system is small relative to the temperature (in kelvins) before and after the process, the en- tropy change can be approximated as (20-3) where Tavg is the system’s average temperature during the process. When an ideal gas changes reversibly from an initial state with temperature Ti and volume Vi to a final state with temperature Tf and volume Vf , the change �S in the entropy of the gas is (20-4) The Second Law of Thermodynamics This law, which is an extension of the entropy postulate, states: If a process occurs in a closed system, the entropy of the system increases for irreversible processes and remains constant for reversible processes. It never de- creases. In equation form, �S � 0. (20-5) Engines An engine is a device that, operating in a cycle, extracts energy as heat |QH| from a high-temperature reservoir and does a cer- �S � Sf � Si � nR ln Vf Vi � nCV ln Tf Ti . �S � Sf � Si � Q Tavg , �S � Sf � Si � Q T . �S � Sf � Si � �f i dQ T . tain amount of work |W|.The efficiency of any engine is defined as (20-11) In an ideal engine, all processes are reversible and no wasteful energy transfers occur due to, say, friction and turbulence.A Carnot engine is an ideal engine that follows the cycle of Fig.20-9. Its efficiency is (20-12, 20-13) in which TH and TL are the temperatures of the high- and low-tem- perature reservoirs, respectively. Real engines always have an effi- ciency lower than that given by Eq. 20-13. Ideal engines that are not Carnot engines also have lower efficiencies. A perfect engine is an imaginary engine in which energy ex- tracted as heat from the high-temperature reservoir is converted completely to work. Such an engine would violate the second law of thermodynamics, which can be restated as follows: No series of processes is possible whose sole result is the absorption of energy as heat from a thermal reservoir and the complete conversion of this energy to work. Refrigerators A refrigerator is a device that, operating in a cy- cle, has work W done on it as it extracts energy |QL| as heat from a low-temperature reservoir. The coefficient of performance K of a refrigerator is defined as . (20-14) A Carnot refrigerator is a Carnot engine operating in reverse. For a Carnot refrigerator, Eq. 20-14 becomes (20-15, 20-16) A perfectrefrigerator is an imaginary refrigerator in which en- ergy extracted as heat from the low-temperature reservoir is con- verted completely to heat discharged to the high-temperature reser- voir, without any need for work. Such a refrigerator would violate the second law of thermodynamics, which can be restated as follows: No series of processes is possible whose sole result is the transfer of energy as heat from a reservoir at a given temperature to a reservoir at a higher temperature. Entropy from a Statistical View The entropy of a system can be defined in terms of the possible distributions of its molecules. For identical molecules, each possible distribution of molecules is called a microstate of the system. All equivalent mi- crostates are grouped into a configuration of the system. The num- KC � |QL| |QH| � |QL| � TL TH � TL . K � what we want what we pay for � |QL| |W| C � 1 � |QL| |QH| � 1 � TL TH , � energy we get energy we pay for � |W| |QH| . change for that process in terms of temperature and heat transfer. In this sample problem, we calculate the same in- crease in entropy with statistical mechanics using the fact that the system consists of molecules. In short, the two, very different approaches give the same answer. Additional examples, video, and practice available at WileyPLUS halliday_c20_536-560hr.qxd 4-11-2009 16:08 Page 554 555QU E STION S PART 2 ber of microstates in a configuration is the multiplicity W of the configuration. For a system of N molecules that may be distributed between the two halves of a box, the multiplicity is given by (20-20) in which n1 is the number of molecules in one half of the box and n2 is the number in the other half. A basic assumption of statistical mechanics is that all the microstates are equally probable. Thus, con- figurations with a large multiplicity occur most often.When N is very W � N! n1! n2! , large (say, N 1022 molecules or more), the molecules are nearly always in the configuration in which n1 � n2. The multiplicity W of a configuration of a system and the en- tropy S of the system in that configuration are related by Boltzmann’s entropy equation: S � k ln W, (20-21) where k � 1.38 � 10�23 J/K is the Boltzmann constant. When N is very large (the usual case), we can approximate ln N! with Stirling’s approximation: ln N! � N(ln N) � N. (20-22) � 1 Point i in Fig. 20-19 represents the initial state of an ideal gas at temperature T. Taking algebraic signs into account, rank the entropy changes that the gas undergoes as it moves, successively and reversibly, from point i to points a, b, c, and d, greatest first. 2 In four experiments, blocks A and B, starting at different initial temperatures, were brought together in an insulating box and al- lowed to reach a common final temperature. The entropy changes for the blocks in the four experiments had the following values (in joules per kelvin), but not necessarily in the order given. Determine which values for A go with which values for B. Block Values A 8 5 3 9 B �3 �8 �5 �2 3 A gas, confined to an insulated cylinder, is compressed adiabatically to half its volume. Does the entropy of the gas increase, decrease, or remain unchanged during this process? 4 An ideal monatomic gas at initial temperature T0 (in kelvins) expands from initial volume V0 to volume 2V0 by each of the five processes indicated in the T-V diagram of Fig. 20-20. In which process is the expansion (a) isothermal, (b) isobaric (constant pres- sure), and (c) adiabatic? Explain your answers. (d) In which processes does the entropy of the gas decrease? 5 In four experiments, 2.5 mol of hydrogen gas undergoes reversible isothermal expansions, starting from the same volume but at different temperatures. The corresponding p-V plots are shown in Fig. 20-21. Rank the situations according to the change in the entropy of the gas, greatest first. 6 A box contains 100 atoms in a configuration that has 50 atoms in each half of the box. Suppose that you could count the different microstates associated with this configuration at the rate of 100 bil- lion states per second, using a supercomputer. Without written cal- culation, guess how much computing time you would need: a day, a year, or much more than a year. 7 Does the entropy per cycle increase, decrease, or remain the same for (a) a Carnot engine, (b) a real engine, and (c) a perfect engine (which is, of course, impossible to build)? 8 Three Carnot engines operate between temperature limits of (a) 400 and 500 K, (b) 500 and 600 K, and (c) 400 and 600 K. Each engine extracts the same amount of energy per cycle from the high-temperature reservoir. Rank the magnitudes of the work done by the engines per cycle, greatest first. 9 An inventor claims to have invented four engines, each of which operates between constant-temperature reservoirs at 400 and 300 K. Data on each engine, per cycle of operation, are: engine A, QH � 200 J, QL � �175 J, and W � 40 J; engine B, QH � 500 J, QL � �200 J, and W � 400 J; engine C, QH � 600 J, QL � �200 J, and W � 400 J; engine D, QH � 100 J, QL � �90 J, and W � 10 J. Of the first and second laws of thermodynamics,which (if either) does each engine violate? 10 Does the entropy per cycle increase, decrease, or remain the same for (a) a Carnot refrigerator, (b) a real refrigerator, and (c) a perfect refrigerator (which is, of course, impossible to build)? Fig. 20-19 Question 1. id c b a T T + ∆T T – ∆T Volume Pr es su re a b c d p V Fig. 20-21 Question 5. Fig. 20-20 Question 4. 2V0V0 Volume T em pe ra tu re T0 A B C D E F 1.5T0 2.0T0 2.5T0 0.63T0 halliday_c20_536-560hr.qxd 4-11-2009 16:08 Page 555
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