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388 parameters with one constraint) are said to possess two 388 parameters with one constraint) are said to possess two
389 /degrees of freedom/; for the range of possible equilibrium states is defined 389 /degrees of freedom/; for the range of possible equilibrium states is defined
390 by specifying any two of the variables arbitrarily, whereupon the 390 by specifying any two of the variables arbitrarily, whereupon the
391 third, and all others we may introduce, are determined. 391 third, and all others we may introduce, are determined.
392 Mathematically, this is expressed by the existence of a functional 392 Mathematically, this is expressed by the existence of a functional
393 relationship of the form[fn:: The set of solutions to an equation 393 relationship of the form[fn:: Edit: The set of solutions to an equation
394 like /f(X,x,t)=/ const. is called a /level set/. Here, Jaynes is 394 like /f(X,x,t)=/ const. is called a /level set/. Here, Jaynes is
395 saying that the quantities /X/, /x/, and /t/ follow a \ldquo{}functional 395 saying that the quantities /X/, /x/, and /t/ follow a \ldquo{}functional
396 rule\rdquo{}, so the set of physically allowed combinations of /X/, 396 rule\rdquo{}, so the set of physically allowed combinations of /X/,
397 /x/, and /t/ in equilibrium states can be 397 /x/, and /t/ in equilibrium states can be
398 expressed as the level set of a function. 398 expressed as the level set of a function.
631 thermal interaction, which can be carried out as soon as a primitive 631 thermal interaction, which can be carried out as soon as a primitive
632 thermometer is at hand. In fact these experiments, which we summarize 632 thermometer is at hand. In fact these experiments, which we summarize
633 so quickly, required a very long time for their first performance, and 633 so quickly, required a very long time for their first performance, and
634 the essential conclusions of this Section were first arrived at only 634 the essential conclusions of this Section were first arrived at only
635 about 1760---more than 160 years after Galileo's invention of the 635 about 1760---more than 160 years after Galileo's invention of the
636 thermometer---by Joseph Black, who was Professor of Chemistry at 636 thermometer---[[http://web.lemoyne.edu/~giunta/blackheat.html][by Joseph Black]], who was Professor of Chemistry at
637 Glasgow University. Black's analysis of calorimetric experiments 637 Glasgow University. Black's analysis of calorimetric experiments
638 initiated by G. D. Fahrenheit before 1736 led to the first recognition 638 initiated by G. D. Fahrenheit before 1736 led to the first recognition
639 of the distinction between temperature and heat, and prepared the way 639 of the distinction between temperature and heat, and prepared the way
640 for the work of his better-known pupil, James Watt. 640 for the work of his better-known pupil, James Watt.
641 641
1029 in the same units. 1029 in the same units.
1030 1030
1031 Secondly, we have already stressed that the theory being 1031 Secondly, we have already stressed that the theory being
1032 developed must, strictly speaking, be a theory only of 1032 developed must, strictly speaking, be a theory only of
1033 equilibrium states, since otherwise we have no operational definition 1033 equilibrium states, since otherwise we have no operational definition
1034 of temperature . When we integrate over any \ldquo{}path\rdquo{} in the $(V-t)$ 1034 of temperature When we integrate over any \ldquo{}path\rdquo{} in the $(V-t)$
1035 plane, therefore, it must be understood that the path of 1035 plane, therefore, it must be understood that the path of
1036 integration is, strictly speaking, just a /locus of equilibrium 1036 integration is, strictly speaking, just a /locus of equilibrium
1037 states/; nonequilibrium states cannot be represented by points 1037 states/; nonequilibrium states cannot be represented by points
1038 in the $(V-t)$ plane. 1038 in the $(V-t)$ plane.
1039 1039
1065 arbitrarily slowly is /reversible/; if a system is arbitrarily 1065 arbitrarily slowly is /reversible/; if a system is arbitrarily
1066 close to equilibrium, then an arbitrarily small change in its 1066 close to equilibrium, then an arbitrarily small change in its
1067 environment can reverse the direction of the process. 1067 environment can reverse the direction of the process.
1068 Recognizing this, we can then say that the paths of integra 1068 Recognizing this, we can then say that the paths of integra
1069 tion in our equations are to be interpreted physically as 1069 tion in our equations are to be interpreted physically as
1070 /reversible paths/ . In practice, some systems (such as gases) 1070 /reversible paths/ In practice, some systems (such as gases)
1071 come to equilibrium so rapidly that rather fast changes of 1071 come to equilibrium so rapidly that rather fast changes of
1072 state (on the time scale of our own perceptions) may be quite 1072 state (on the time scale of our own perceptions) may be quite
1073 good approximations to reversible changes; thus the change of 1073 good approximations to reversible changes; thus the change of
1074 state of water vapor in a steam engine may be considered 1074 state of water vapor in a steam engine may be considered
1075 reversible to a useful engineering approximation. 1075 reversible to a useful engineering approximation.
1098 freedom, in part an anthropomorphic one, because it may depend 1098 freedom, in part an anthropomorphic one, because it may depend
1099 on the particular kind of subdivision we choose to imagine. For 1099 on the particular kind of subdivision we choose to imagine. For
1100 example, a volume of air may be imagined to consist of a number 1100 example, a volume of air may be imagined to consist of a number
1101 of smaller contiguous volume elements. With this subdivision, 1101 of smaller contiguous volume elements. With this subdivision,
1102 the pressure is the same in all subsystems, and is therefore in 1102 the pressure is the same in all subsystems, and is therefore in
1103 tensive; while the volume is additive and therefore extensive . 1103 tensive; while the volume is additive and therefore extensive
1104 But we may equally well regard the volume of air as composed of 1104 But we may equally well regard the volume of air as composed of
1105 its constituent nitrogen and oxygen subsystems (or we could re 1105 its constituent nitrogen and oxygen subsystems (or we could re
1106 gard pure hydrogen as composed of two subsystems, in which the 1106 gard pure hydrogen as composed of two subsystems, in which the
1107 molecules have odd and even rotational quantum numbers 1107 molecules have odd and even rotational quantum numbers
1108 respectively, etc.) . With this kind of subdivision the volume is the 1108 respectively, etc.) With this kind of subdivision the volume is the
1109 same in all subsystems, while the pressure is the sum of the 1109 same in all subsystems, while the pressure is the sum of the
1110 partial pressures of its constituents; and it appears that the 1110 partial pressures of its constituents; and it appears that the
1111 roles of \ldquo{}intensive\rdquo{} and \ldquo{}extensive\rdquo{} 1111 roles of \ldquo{}intensive\rdquo{} and \ldquo{}extensive\rdquo{}
1112 have been interchanged. Note that this ambiguity cannot be removed by requiring 1112 have been interchanged. Note that this ambiguity cannot be removed by requiring
1113 that we consider only spatial subdivisions, such that each sub 1113 that we consider only spatial subdivisions, such that each sub
1114 system has the same local composi tion . For, consider a s tressed 1114 system has the same local composi tion For, consider a s tressed
1115 elastic solid, such as a stretched rubber band. If we imagine 1115 elastic solid, such as a stretched rubber band. If we imagine
1116 the rubber band as divided, conceptually, into small subsystems 1116 the rubber band as divided, conceptually, into small subsystems
1117 by passing planes through it normal to its axis, then the tension 1117 by passing planes through it normal to its axis, then the tension
1118 is the same in all subsystems, while the elongation is additive. 1118 is the same in all subsystems, while the elongation is additive.
1119 But if the dividing planes are parallel to the axis, the elonga 1119 But if the dividing planes are parallel to the axis, the elonga
1149 in an infinitesimal reversible change of state can be separated 1149 in an infinitesimal reversible change of state can be separated
1150 into a product $dW = PdV$ of an intensive and an extensive quantity. 1150 into a product $dW = PdV$ of an intensive and an extensive quantity.
1151 Furthermore, we know that the pressure $P$ is not only the 1151 Furthermore, we know that the pressure $P$ is not only the
1152 intensive factor of the work; it is also the \ldquo{}potential\rdquo{} 1152 intensive factor of the work; it is also the \ldquo{}potential\rdquo{}
1153 which governs mechanical equilibrium (in this case, equilibrium with respect 1153 which governs mechanical equilibrium (in this case, equilibrium with respect
1154 to exchange of volume) between two systems; i .e., if they are 1154 to exchange of volume) between two systems; ie., if they are
1155 separated by a flexible but impermeable membrane, the two systems 1155 separated by a flexible but impermeable membrane, the two systems
1156 will exchange volume $dV_1 = -dV_2$ in a direction determined by the 1156 will exchange volume $dV_1 = -dV_2$ in a direction determined by the
1157 pressure difference, until the pressures are equalized. The 1157 pressure difference, until the pressures are equalized. The
1158 energy exchanged in this way between the systems is a product 1158 energy exchanged in this way between the systems is a product
1159 of the form 1159 of the form
1173 in the same way that pressure does for volume exchange. 1173 in the same way that pressure does for volume exchange.
1174 1174
1175 1175
1176 But we already know that the /temperature/ is the quantity 1176 But we already know that the /temperature/ is the quantity
1177 that governs the heat flow (i.e., heat flows from the hotter to 1177 that governs the heat flow (i.e., heat flows from the hotter to
1178 the cooler body until the temperatures are equalized) . So the 1178 the cooler body until the temperatures are equalized) So the
1179 intensive factor in $dQ$ must be essentially the temperature. But 1179 intensive factor in $dQ$ must be essentially the temperature. But
1180 our temperature scale is at present still arbitrary, and we can 1180 our temperature scale is at present still arbitrary, and we can
1181 hardly expect that such a factorization will be possible for all 1181 hardly expect that such a factorization will be possible for all
1182 calibrations of our thermometers. 1182 calibrations of our thermometers.
1183 1183
1216 (nor does the \ldquo{}amount of work\rdquo{} $W$; 1216 (nor does the \ldquo{}amount of work\rdquo{} $W$;
1217 only the total energy is a well-defined quantity). 1217 only the total energy is a well-defined quantity).
1218 But we want the entropy $S(U,V)$ to be a definite quantity, 1218 But we want the entropy $S(U,V)$ to be a definite quantity,
1219 like the energy or volume, and so $dS$ must be an exact differential. 1219 like the energy or volume, and so $dS$ must be an exact differential.
1220 On an infinitesimal reversible change from one equilibrium state 1220 On an infinitesimal reversible change from one equilibrium state
1221 to another, the first law requires that it satisfy[fn:: The first 1221 to another, the first law requires that it satisfy[fn:: Edit: The first
1222 equality comes from our requirement that $dQ = T\,dS$. The second 1222 equality comes from our requirement that $dQ = T\,dS$. The second
1223 equality comes from the fact that $dU = dQ - dW$ (the first law) and 1223 equality comes from the fact that $dU = dQ - dW$ (the first law) and
1224 that $dW = PdV$ in the case where the state has two degrees of 1224 that $dW = PdV$ in the case where the state has two degrees of
1225 freedom, pressure and volume.] 1225 freedom, pressure and volume.]
1226 1226
1227 \begin{equation} 1227 \begin{equation}
1228 dS(U,V) = \frac{dQ}{T} = \frac{dU}{T} + \frac{P}{T}dV 1228 dS(U,V) = \frac{dQ}{T} = \frac{dU}{T} + \frac{P}{T}dV
1229 \end{equation} 1229 \end{equation}
1230 1230
1231 Thus $(1/T)$ must be an /integrating factor/ which converts $dQ$ into 1231 Thus $(1/T)$ must be an /integrating factor/ which converts $dQ$ into
1232 an exact differential [[fn::A differential $M(x,y)dx + 1232 an exact differential [[fn::Edit: A differential $M(x,y)dx +
1233 N(x,y)dy$ is called /exact/ if there is a scalar function 1233 N(x,y)dy$ is called /exact/ if there is a scalar function
1234 $\Phi(x,y)$ such that $M = \frac{\partial \Phi}{\partial x}$ and 1234 $\Phi(x,y)$ such that $M = \frac{\partial \Phi}{\partial x}$ and
1235 $N=\frac{\partial \Phi}{\partial y}$. If there is, \Phi is called the 1235 $N=\frac{\partial \Phi}{\partial y}$. If there is, \Phi is called the
1236 /potential function/ of the differential, Conceptually, this means 1236 /potential function/ of the differential, Conceptually, this means
1237 that M(x,y)dx + N(x,y) dy is the derivative of a scalar potential and 1237 that M(x,y)dx + N(x,y) dy is the derivative of a scalar potential and
1312 each adiabat is still completely undetermined. 1312 each adiabat is still completely undetermined.
1313 1313
1314 In order to fix the relative values of $S$ on different 1314 In order to fix the relative values of $S$ on different
1315 adiabats we need to add the condition, not yet put into the equations, 1315 adiabats we need to add the condition, not yet put into the equations,
1316 that the integrating factor $w(U,V) = T^{-1}$ is to define a new 1316 that the integrating factor $w(U,V) = T^{-1}$ is to define a new
1317 temperature scale . In other words, we now ask: out of the 1317 temperature scale In other words, we now ask: out of the
1318 infinite number of different integrating factors allowed by 1318 infinite number of different integrating factors allowed by
1319 the differential equation (1-23), is it possible to find one 1319 the differential equation (1-23), is it possible to find one
1320 which is a function only of the empirical temperature $t$? If 1320 which is a function only of the empirical temperature $t$? If
1321 $w=w(t)$, we can write 1321 $w=w(t)$, we can write
1322 1322
1495 \begin{equation}PV = n \cdot f(t)\end{equation} 1495 \begin{equation}PV = n \cdot f(t)\end{equation}
1496 1496
1497 where f(t) is a function that depends on the particular empirical 1497 where f(t) is a function that depends on the particular empirical
1498 temperature scale used. But from (1-33) we must then have 1498 temperature scale used. But from (1-33) we must then have
1499 $f(t) = RT$, where $R$ is a constant, the universal gas constant whose 1499 $f(t) = RT$, where $R$ is a constant, the universal gas constant whose
1500 numerical value (1.986 calories per mole per degree K) , depends 1500 numerical value (1.986 calories per mole per degree K), depends
1501 on the size of the units in which we choose to measure the Kelvin 1501 on the size of the units in which we choose to measure the Kelvin
1502 temperature $T$. In terms of the Kelvin temperature, the ideal gas 1502 temperature $T$. In terms of the Kelvin temperature, the ideal gas
1503 equation of state is therefore simply 1503 equation of state is therefore simply
1504 1504
1505 \begin{equation} 1505 \begin{equation}
1552 definition of a physical unit, its numerical value is of course chosen 1552 definition of a physical unit, its numerical value is of course chosen
1553 so as to be well inside the limits of error with which the old 1553 so as to be well inside the limits of error with which the old
1554 unit could be defined. Thus the old Centigrade and new Celsius 1554 unit could be defined. Thus the old Centigrade and new Celsius
1555 scales are the same, within the accuracy with which the 1555 scales are the same, within the accuracy with which the
1556 Centigrade scale could be realized; so the same notation, ^\circ C, is used 1556 Centigrade scale could be realized; so the same notation, ^\circ C, is used
1557 for both . Only in this way can old measurements retain their 1557 for both Only in this way can old measurements retain their
1558 value and accuracy, without need of corrections every time a 1558 value and accuracy, without need of corrections every time a
1559 unit is redefined. 1559 unit is redefined.
1560 1560
1561 #capitalize Joules? 1561 #capitalize Joules?
1562 Exactly the same thing has happened in the definition of 1562 Exactly the same thing has happened in the definition of
1563 the calorie; for a century, beginning with the work of Joule, 1563 the calorie; for a century, beginning with the work of Joule,
1564 more and more precise experiments were performed to determine 1564 more and more precise experiments were performed to determine
1565 the mechanical equivalent of heat more and more accurately . But 1565 the mechanical equivalent of heat more and more accurately But
1566 eventually mechanical and electrical measurements of energy be 1566 eventually mechanical and electrical measurements of energy be
1567 came far more reproducible than calorimetric measurements; so 1567 came far more reproducible than calorimetric measurements; so
1568 recently the calorie was redefined to be 4.1840 Joules, this 1568 recently the calorie was redefined to be 4.1840 Joules, this
1569 number now being exact by definition. Further details are given 1569 number now being exact by definition. Further details are given
1570 in the aforementioned Bureau of Standards Bulletin. 1570 in the aforementioned Bureau of Standards Bulletin.
1598 appeal to the second law. From the standpoint of logic, there 1598 appeal to the second law. From the standpoint of logic, there
1599 fore, the second law serves /only/ to establish that the Kelvin 1599 fore, the second law serves /only/ to establish that the Kelvin
1600 temperature scale is the same for all substances. 1600 temperature scale is the same for all substances.
1601 1601
1602 1602
1603 ** COMMENT Entropy of an Ideal Boltzmann Gas 1603 ** Entropy of an Ideal Boltzmann Gas
1604 1604
1605 At the present stage we are far from understanding the physical 1605 At the present stage we are far from understanding the physical
1606 meaning of the function $S$ defined by (1-19); but we can investigate its mathematical 1606 meaning of the function $S$ defined by (1-19); but we can investigate
1607 form and numerical values. Let us do this for a system con 1607 its mathematical form and numerical values. Let us do this for a
1608 sisting cf n moles of a substance which obeys the ideal gas 1608 system
1609 consisting of $n$ moles of a substance which obeys the ideal gas
1609 equation of state 1610 equation of state
1610 and for which the heat capacity at constant volume CV is a 1611
1611 constant. The difference in entropy between any two states (1) 1612 \begin{equation}PV = nRT\end{equation}
1613
1614 and for which the heat capacity at constant volume
1615 $C_V$ is a constant. The difference in entropy between any two states (1)
1612 and (2) is from (1-19), 1616 and (2) is from (1-19),
1613 1617
1618 \begin{equation}
1619 S_2 - S_1 = \int_1^2 \frac{dQ}{T} = \int_1^2
1620 \left[\left(\frac{\partial S}{\partial V}\right)+\left(\frac{\partial S}{\partial T}\right)_V dT\right]
1621 \end{equation}
1614 1622
1615 where we integrate over any reversible path connecting the two 1623 where we integrate over any reversible path connecting the two
1616 states. From the manner in which S was defined, this integral 1624 states. From the manner in which $S$ was defined, this integral
1617 must be the same whatever path we choose. Consider, then, a 1625 must be the same whatever path we choose. Consider, then, a
1618 path consisting of a reversible expansion at constant tempera 1626 path consisting of a reversible expansion at constant
1619 ture to a state 3 which has the initial temperature T, and the 1627 temperature to a state 3 which has the initial temperature $T_1$, and the
1620 .L ' "'1 final volume V2; followed by heating at constant volume to the final temperature T2. Then (1-47) becomes 1628 the final volume $V_2$; followed by heating at constant volume to the
1621 3 2 I If r85 - on - db — = d — -4 S2 51 J V [aT]v M (1 8) 1629 final temperature $T_2$.
1622 1 3 1630 Then (1-47) becomes
1623 To evaluate the integral over (1 +3) , note that since 1631
1624 dU = T :15 — P dV, the Helmholtz free energy function F E U — TS 1632 \begin{equation}
1625 has the property dF = --S - P 61V; and of course is an exact 1633 S_2 - S_1 = \int_1^3 \left(\frac{\partial S}{\partial V}\right)_T dV +
1626 differential since F is a definite state function. The condition 1634 \int_3^2 \left(\frac{\partial S}{\partial T}\right)_V dT
1627 that dF be exact is, analogous to (1-22), 1635 \end{equation}
1636
1637 To evaluate the integral over $(1\rightarrow 3)$, note that since $dU
1638 = TdS - PdV$, the Helmholtz free energy function $F \equiv U -TS$ has
1639 the property $dF = -SdT - PdV$; and of course $dF$ is an exact
1640 differential since $F$ is a definite state function. The condition
1641 that $dF$ be exact is, analogous to (1-22),
1642
1643 \begin{equation}
1644 \left(\frac{\partial S}{\partial V}\right)_T = \left(\frac{\partial
1645 P}{\partial T}\right)_V
1646 \end{equation}
1647
1628 which is one of the Maxwell relations, discussed further in 1648 which is one of the Maxwell relations, discussed further in
1629 where CV is the molar heat capacity at constant volume. Collec 1649 Chapter 2. But [the value of this expression] is determined by the equation of state
1630 ting these results, we have 1650 (1-46):
1631 3 1651
1632 l 3 1652 \begin{equation}
1633 1 nR log(V2/V1) + nCV log(T2/Tl) (1-52) 1653 \left(\frac{\partial S}{\partial V}\right)_T = \frac{nR}{V}
1634 since CV was assumed independent of T. Thus the entropy function 1654 \end{equation}
1655
1656 Likewise, along the path $(3\rightarrow 2)$, we have
1657
1658 \begin{equation}
1659 \left(\frac{\partial S}{\partial T}\right)_V = \frac{n C_V}{T}
1660 \end{equation}
1661
1662 where $C_V$ is the molar heat capacity at constant volume.
1663 Collecting these results, we have
1664
1665 \begin{equation}
1666 S_2 - S_1 = \int_1^3 \frac{nR}{V} dV + \int_2^3 \frac{n C_V}{T} dT =
1667 nR\log{(V_2/V_1)} + nC_V \log{(T_2/T_1)}
1668 \end{equation}
1669
1670 since $C_V$ was assumed independent of $T$. Thus the entropy function
1635 must have the form 1671 must have the form
1636 S(n,V,T) = nR log V + n CV log T + (const.) (l~53) 1672
1637 1673 \begin{equation}
1674 S(n,V,T) = nR \log{V} + n C_V \log{T} + (\text{const.})
1675 \end{equation}
1638 1676
1639 From the derivation, the additive constant must be independent 1677 From the derivation, the additive constant must be independent
1640 of V and T; but it can still depend on n. We indicate this by 1678 of V and T; but it can still depend on n. We indicate this by
1641 writing 1679 writing
1642 where f (n) is a function not determined by the definition (1-47). 1680
1643 The form of f (n) is , however, restricted by the condition that 1681 \begin{equation}
1644 the entropy be an extensive quantity; i .e . , two identical systems 1682 S(n,V,T) = n\left[R \log{V} + C_V \log{T}\right] + f(n)
1645 placed together should have twice the entropy of a single system; 1683 \end{equation}
1646 Substituting (l—-54) into (1-55), we find that f(n) must satisfy 1684
1647 To solve this, one can differentiate with respect to q and set 1685 where $f(n)$ is a function not determined by the definition (1-47).
1648 q = 1; we then obtain the differential equation 1686 The form of $f(n)$ is, however, restricted by the condition that
1649 n f ' (n) — f (n) + Rn = 0 (1-57) 1687 the entropy be an extensive quantity; i.e., two identical systems
1650 which is readily solved; alternatively, just set n = 1 in (1-56) 1688 placed together should have twice the entropy of a single system; or
1651 and replace q by n . By either procedure we find 1689 more generally,
1652 f (n) = n f (1) — Rn log n . (1-58) 1690
1653 As a check, it is easily verified that this is the solution of 1691 \begin{equation}
1654 where A E f (l) is still an arbitrary constant, not determined 1692 S(qn, qV, T) = q\cdot S(n,v,T),\qquad 0<q<\infty
1655 by the definition (l—l9) , or by the condition (l-55) that S be 1693 \end{equation}
1656 extensive. However, A is not without physical meaning; we will 1694
1657 see in the next Section that the vapor pressure of this sub 1695 Substituting (1-54) into (1-55), we find that $f(n)$ must satisfy
1658 stance (and more generally, its chemical potential) depends on 1696 the functional equation
1659 A. Later, it will appear that the numerical value of A involves 1697
1698 \begin{equation}
1699 f(q\cdot n) = q\cdot f(n) - R\cdot n\cdot q\log{q}\end{equation}
1700
1701
1702 To solve this, one can differentiate with respect to $q$ and set
1703 $q = 1$; we then obtain the differential equation
1704
1705 \begin{equation}
1706 n\cdot f^\prime(n) - f(n) + R\cdot n = 0
1707 \end{equation}
1708 # xy' - y + rx = 0
1709 which is readily solved; alternatively, just set $n = 1$ in (1-56)
1710 and replace $q$ by $n$ By either procedure we find
1711
1712 \begin{equation}
1713 f(n) = n\cdot f(1) - R\cdot n \log{n} (1-58)
1714 \end{equation}
1715
1716 As a check, it is easily verified that this is the solution of (1-56)
1717 and (1-57). We then have finally,
1718
1719 \begin{equation}
1720 S(n,V,t) = n\left[C_v\cdot\log{t} + R\cdot \log{\left(\frac{V}{n}\right)} +
1721 A\right]
1722 \end{equation}
1723
1724 where $A\equiv f(1)$ is still an arbitrary constant, not determined
1725 by the definition (1-19), or by the condition (1-55) that $S$ be
1726 extensive. However, $A$ is not without physical meaning; we will
1727 see in the next Section that the vapor pressure of this
1728 substance (and more generally, its chemical potential) depends on
1729 $A$. Later, it will appear that the numerical value of $A$ involves
1660 Planck's constant, and its theoretical determination therefore 1730 Planck's constant, and its theoretical determination therefore
1661 requires quantum statistics . 1731 requires quantum statistics.
1662 We conclude from this that, in any region where experi 1732
1663 mentally CV const. , and the ideal gas equation of state is 1733 #edit: "is constant"
1664 1734 We conclude from this that, in any region where experimentally
1665 1735 $C_V$ is constant, and the ideal gas equation of state is
1666 obeyed, the entropy must have the form (1-59) . The fact that 1736 obeyed, the entropy must have the form (1-59) The fact that
1667 classical statistical mechanics does not lead to this result, 1737 classical statistical mechanics does not lead to this result,
1668 the term nR log (l/n) being missing (Gibbs paradox) , was his 1738 the term $n\cdot R \cdot \log{(1/n)}$ being missing (Gibbs paradox),
1669 torically one of the earliest clues indicating the need for the 1739 was historically one of the earliest clues indicating the need for the
1670 quantum theory. 1740 quantum theory.
1671 In the case of a liquid, the volume does not change appre 1741
1672 ciably on heating, and so d5 = n CV dT/T, and if CV is indepen 1742 In the case of a liquid, the volume does not change
1673 dent of temperature, we would have in place of (1-59) , 1743 appreciably on heating, and so $dS = n\cdot C_V\cdot dT/T$, and if
1674 where Ag is an integration constant, which also has physical 1744 $C_V$ is independent of temperature, we would have in place of (1-59),
1745
1746 \begin{equation}
1747 S = n\left[C_V\ln{T}+A_\ell\right]
1748 \end{equation}
1749
1750 where $A_\ell$ is an integration constant, which also has physical
1675 meaning in connection with conditions of equilibrium between 1751 meaning in connection with conditions of equilibrium between
1676 two different phases. 1752 two different phases.
1677 1.1.0 The Second Law: Definition. Probably no proposition in 1753
1678 physics has been the subject of more deep and sus tained confusion 1754 ** The Second Law: Definition
1679 than the second law of thermodynamics . It is not in the province 1755
1756 Probably no proposition in physics has been the subject of more deep
1757 and sustained confusion
1758 than the second law of thermodynamics It is not in the province
1680 of macroscopic thermodynamics to explain the underlying reason 1759 of macroscopic thermodynamics to explain the underlying reason
1681 for the second law; but at this stage we should at least be able 1760 for the second law; but at this stage we should at least be able
1682 to state this law in clear and experimentally meaningful terms. 1761 to /state/ this law in clear and experimentally meaningful terms.
1683 However, examination of some current textbooks reveals that, 1762 However, examination of some current textbooks reveals that,
1684 after more than a century, different authors still disagree as 1763 after more than a century, different authors still disagree as
1685 to the proper statement of the second law, its physical meaning, 1764 to the proper statement of the second law, its physical meaning,
1686 and its exact range of validity. 1765 and its exact range of validity.
1766
1687 Later on in this book it will be one of our major objectives 1767 Later on in this book it will be one of our major objectives
1688 to show, from several different viewpoints , how much clearer and 1768 to show, from several different viewpoints, how much clearer and
1689 simpler these problems now appear in the light of recent develop 1769 simpler these problems now appear in the light of recent develop
1690 ments in statistical mechanics . For the present, however, our 1770 ments in statistical mechanics For the present, however, our
1691 aim is only to prepare the way for this by pointing out exactly 1771 aim is only to prepare the way for this by pointing out exactly
1692 what it is that is to be proved later. As a start on this at 1772 what it is that is to be proved later. As a start on this at
1693 tempt, we note that the second law conveys a certain piece of 1773 tempt, we note that the second law conveys a certain piece of
1694 informations about the direction in which processes take place. 1774 informations about the /direction/ in which processes take place.
1695 In application it enables us to predict such things as the final 1775 In application it enables us to predict such things as the final
1696 equilibrium state of a system, in situations where the first law 1776 equilibrium state of a system, in situations where the first law
1697 alone is insufficient to do this. 1777 alone is insufficient to do this.
1778
1779
1698 A concrete example will be helpful. We have a vessel 1780 A concrete example will be helpful. We have a vessel
1699 equipped with a piston, containing N moles of carbon dioxide. 1781 equipped with a piston, containing $N$ moles of carbon dioxide.
1700 1782
1701 1783 #changed V_f to V_1
1702 The system is initially at thermal equilibrium at temperature To, volume V0 and pressure PO; and under these conditions it contains 1784 The system is initially at thermal equilibrium at temperature $T_0$,
1703 n moles of CO2 in the vapor phase and moles in the liquid 1785 volume $V_0$ and pressure $P_O$; and under these conditions it contains
1704 phase . The system is now thermally insulated from its surround 1786 $n$ moles of CO_2 in the vapor phase and $N-n$ moles in the liquid
1705 ings, and the piston is moved rapidly (i.e. , so that n does not 1787 phase The system is now thermally insulated from its
1788 surroundings, and the piston is moved rapidly (i.e., so that $n$ does not
1706 change appreciably during the motion) so that the system has a 1789 change appreciably during the motion) so that the system has a
1707 new volume Vf; and immediately after the motion, a new pressure 1790 new volume $V_1$; and immediately after the motion, a new pressure
1708 PI . The piston is now held fixed in its new position , and the 1791 $P_1$ The piston is now held fixed in its new position, and the
1709 system allowed to come once more to equilibrium. During this 1792 system allowed to come once more to equilibrium. During this
1710 process, will the CO2 tend to evaporate further, or condense further? What will be the final equilibrium temperature Teq, the final pressure PeCE , and final value of n eq? 1793 process, will the CO_2 tend to evaporate further, or condense further?
1711 It is clear that the firs t law alone is incapable of answering 1794 What will be the final equilibrium temperature $T_{eq}$,
1795 the final pressure $P_eq$, and final value of $n_{eq}$?
1796
1797 It is clear that the first law alone is incapable of answering
1712 these questions; for if the only requirement is conservation of 1798 these questions; for if the only requirement is conservation of
1713 energy, then the CO2 might condense , giving up i ts heat of vapor 1799 energy, then the CO_2 might condense, giving up its heat of
1714 ization and raising the temperature of the system; or it might 1800 vaporization and raising the temperature of the system; or it might
1715 evaporate further, lowering the temperature. Indeed, all values 1801 evaporate further, lowering the temperature. Indeed, all values
1716 of neq in O i neq i N would be possible without any violation of the first law. In practice, however, this process will be found 1802 of $n_{eq}$ in $O \leq n_{eq} \leq N$ would be possible without any
1717 to go in only one direction and the sys term will reach a definite 1803 violation of the first law. In practice, however, this process will be found
1804 to go in only one direction and the system will reach a definite
1718 final equilibrium state with a temperature, pressure, and vapor 1805 final equilibrium state with a temperature, pressure, and vapor
1719 density predictable from the second law. 1806 density predictable from the second law.
1807
1808
1720 Now there are dozens of possible verbal statements of the 1809 Now there are dozens of possible verbal statements of the
1721 second law; and from one standpoint, any statement which conveys 1810 second law; and from one standpoint, any statement which conveys
1722 the same information has equal right to be called "the second 1811 the same information has equal right to be called \ldquo{}the second
1723 law." However, not all of them are equally direct statements of 1812 law.\rdquo{} However, not all of them are equally direct statements of
1724 experimental fact, or equally convenient for applications, or 1813 experimental fact, or equally convenient for applications, or
1725 equally general; and it is on these grounds that we ought to 1814 equally general; and it is on these grounds that we ought to
1726 choose among them . 1815 choose among them.
1727 Some of the mos t popular statements of the s econd law be 1816
1728 long to the class of the well-—known "impossibility" assertions ; 1817 Some of the mos t popular statements of the second law
1729 i.e. , it is impossible to transfer heat from a lower to a higher 1818 belong to the class of the well-known \ldquo{}impossibility\rdquo{}
1819 assertions; i.e., it is impossible to transfer heat from a lower to a higher
1730 temperature without leaving compensating changes in the rest of 1820 temperature without leaving compensating changes in the rest of
1731 the universe , it is imposs ible to convert heat into useful work 1821 the universe, it is impossible to convert heat into useful work
1732 without leaving compensating changes, it is impossible to make 1822 without leaving compensating changes, it is impossible to make
1733 a perpetual motion machine of the second kind, etc. 1823 a perpetual motion machine of the second kind, etc.
1734
1735 1824
1736 Suoh formulations have one clear logical merit; they are 1825 Suoh formulations have one clear logical merit; they are
1737 stated in such a way that, if the assertion should be false, a 1826 stated in such a way that, if the assertion should be false, a
1738 single experiment would suffice to demonstrate that fact conclu 1827 single experiment would suffice to demonstrate that fact
1739 sively. It is good to have our principles stated in such a 1828 conclusively. It is good to have our principles stated in such a
1740 clear, unequivocal way. 1829 clear, unequivocal way.
1741 However, impossibility statements also have some disadvan 1830
1742 tages . In the first place, their_ are not, and their very 1831 However, impossibility statements also have some
1743 nature cannot be, statements of eiperimental fact. Indeed, we 1832 disadvantages In the first place, /they are not, and by their very
1833 nature cannot be, statements of eiperimental fact/. Indeed, we
1744 can put it more strongly; we have no record of anyone having 1834 can put it more strongly; we have no record of anyone having
1745 seriously tried to do any of the various things which have been 1835 seriously tried to do any of the various things which have been
1746 asserted to be impossible, except for one case which actually 1836 asserted to be impossible, except for one case which actually
1747 succeeded‘. In the experimental realization of negative spin 1837 succeeded. In the experimental realization of negative spin
1748 temperatures , one can transfer heat from a lower to a higher 1838 temperatures, one can transfer heat from a lower to a higher
1749 temperature without external changes; and so one of the common 1839 temperature without external changes; and so one of the common
1750 impossibility statements is now known to be false [for a clear 1840 impossibility statements is now known to be false [for a clear
1751 discussion of this, see the article of N. F . Ramsey (1956) ; 1841 discussion of this, see the [[../sources/Ramsey.pdf][article of N. F. Ramsey (1956)]];
1752 experimental details of calorimetry with negative temperature 1842 experimental details of calorimetry with negative temperature
1753 spin systems are given by Abragam and Proctor (1958) ] . 1843 spin systems are given by Abragam and Proctor (1958)]
1844
1845
1754 Finally, impossibility statements are of very little use in 1846 Finally, impossibility statements are of very little use in
1755 applications of thermodynamics; the assertion that a certain kind 1847 /applications/ of thermodynamics; the assertion that a certain kind
1756 of machine cannot be built, or that a -certain laboratory feat 1848 of machine cannot be built, or that a certain laboratory feat
1757 cannot be performed, does not tell me very directly whether my 1849 cannot be performed, does not tell me very directly whether my
1758 carbon dioxide will condense or evaporate. For applications, 1850 carbon dioxide will condense or evaporate. For applications,
1759 such assertions must first be converted into a more explicit 1851 such assertions must first be converted into a more explicit
1760 mathematical form. 1852 mathematical form.
1853
1854
1761 For these reasons, it appears that a different kind of 1855 For these reasons, it appears that a different kind of
1762 statement of the second law will be, not necessarily more 1856 statement of the second law will be, not necessarily more
1763 "correct,” but more useful in practice. Now both Clausius (3.875) 1857 \ldquo{}correct\rdquo{}, but more useful in practice. Now both Clausius (1875)
1764 and Planck (1897) have laid great stress on their conclusion 1858 and Planck (1897) have laid great stress on their conclusion
1765 that the most general statement, and also the most immediately 1859 that the most general statement, and also the most immediately
1766 useful in applications, is simply the existence of a state 1860 useful in applications, is simply the existence of a state
1767 function, called the entropy, which tends to increase. More 1861 function, called the entropy, which tends to increase. More
1768 precisely: in an adiabatic change of state, the entropy of 1862 precisely: in an adiabatic change of state, the entropy of
1769 a system may increase or may remain constant, but does not 1863 a system may increase or may remain constant, but does not
1770 decrease. In a process involving heat flow to or from the 1864 decrease. In a process involving heat flow to or from the
1771 system, the total entropy of all bodies involved may increase 1865 system, the total entropy of all bodies involved may increase
1772
1773
1774 or may remain constant; but does not decrease; let us call this 1866 or may remain constant; but does not decrease; let us call this
1775 the “weak form" of the second law. 1867 the \ldquo{}weak form\rdquo{} of the second law.
1868
1776 The weak form of the second law is capable of answering the 1869 The weak form of the second law is capable of answering the
1777 first question posed above; thus the carbon dioxide will evapo 1870 first question posed above; thus the carbon dioxide will
1778 rate further if , and only if , this leads to an increase in the 1871 evaporate further if, and only if, this leads to an increase in the
1779 total entropy of the system . This alone , however , is not enough 1872 total entropy of the system This alone, however, is not enough
1780 to answer the second question; to predict the exact final equili 1873 to answer the second question; to predict the exact final
1781 brium state, we need one more fact. 1874 equilibrium state, we need one more fact.
1875
1782 The strong form of the second law is obtained by adding the 1876 The strong form of the second law is obtained by adding the
1783 further assertion that the entropy not only “tends" to increase; 1877 further assertion that the entropy not only \ldquo{}tends\rdquo{} to increase;
1784 in fact it will increase, to the maximum value permitted E2 the 1878 in fact it /will/ increase, /to the maximum value permitted by the
1785 constraints imposed.* In the case of the carbon dioxide, these 1879 constraints imposed[fn::Note, however, that the second law has
1786 constraints are: fixed total energy (first law) , fixed total 1880 nothing to say about how rapidly this approach to equilibrium takes place.]/. In the case of the carbon dioxide, these
1787 amount of carbon dioxide , and fixed position of the piston . The 1881 constraints are: fixed total energy (first law), fixed total
1882 amount of carbon dioxide, and fixed position of the piston. The
1788 final equilibrium state is the one which has the maximum entropy 1883 final equilibrium state is the one which has the maximum entropy
1789 compatible with these constraints , and it can be predicted quan 1884 compatible with these constraints, and it can be predicted
1790 titatively from the strong form of the second law if we know, 1885 quantitatively from the strong form of the second law if we know,
1791 from experiment or theory, the thermodynamic properties of carbon 1886 from experiment or theory, the thermodynamic properties of carbon
1792 dioxide (i .e . , heat capacity , equation of state , heat of vapor 1887 dioxide (ie, heat capacity, equation of state, heat of vapor
1793 ization) . 1888 ization)
1794 To illus trate this , we set up the problem in a crude ap 1889
1795 proximation which supposes that (l) in the range of conditions 1890 To illustrate this, we set up the problem in a crude
1796 of interest, the molar heat capacity CV of the vapor, and C2 of 1891 approximation which supposes that (l) in the range of conditions
1797 the liquid, and the molar heat of vaporization L, are all con 1892 of interest, the molar heat capacity $C_v$ of the vapor, and $C_\ell$ of
1798 stants, and the heat capacities of cylinder and piston are neg 1893 the liquid, and the molar heat of vaporization $L$, are all con
1799 ligible; (2) the liquid volume is always a small fraction of the 1894 stants, and the heat capacities of cylinder and piston are
1800 total V, so that changes in vapor volume may be neglected; (3) the 1895 negligible; (2) the liquid volume is always a small fraction of the
1801 vapor obeys the ideal gas equation of state PV = nRT. The in 1896 total $V$, so that changes in vapor volume may be neglected; (3) the
1802 ternal energy functions of liquid and vapor then have the form 1897 vapor obeys the ideal gas equation of state $PV = nRT$. The
1803 UPb = + A} (1-61) 1898 internal energy functions of liquid and vapor then have the form
1804 T T U = n‘ C '1‘ A + L] (1-62) 1899
1805 v , v 1900 \begin{equation}
1806 where A is a constant which plays no role in the problem. The 1901 U_\ell = (N-n)\left[C_\ell\cdot T + A\right]
1807 appearance of L in (1-62) recognizes that the zero from which we 1902 \end{equation}
1808 *Note , however , that the second law has nothing to say about how rapidly this approach to equilibrium takes place. 1903 \begin{equation}
1809 1904 U_v = n\left[C_v\cdot T + A + L\right]
1810 1905 \end{equation}
1906
1907 where $A$ is a constant which plays no role in the problem. The
1908 appearance of $L$ in (1-62) recognizes that the zero from which we
1811 measure energy of the vapor is higher than that of the liquid by 1909 measure energy of the vapor is higher than that of the liquid by
1812 the energy L necessary to form the vapor. On evaporation of dn 1910 the energy $L$ necessary to form the vapor. On evaporation of $dn$
1813 moles of liquid, the total energy increment is (ill = + dUV= O, 1911 moles of liquid, the total energy increment is $dU = dU_\ell + dU_v =
1814 or 1912 0$; or
1815 [n CV [(CV — CQ)T + = O (l—63) 1913
1914 \begin{equation}
1915 \left[n\cdot C_v + (N-n)C_\ell\right] dT + \left[(C_v-C_\ell)T + L\right]dn = 0
1916 \end{equation}
1917
1816 which is the constraint imposed by the first law. As we found 1918 which is the constraint imposed by the first law. As we found
1817 previously (l~59) , (1-60) the entropies of vapor and liquid are 1919 previously (1-59), (1-60) the entropies of vapor and liquid are
1818 given by 1920 given by
1819 S = n [C 1n T + R ln (V/n) + A ] (1-64) 1921
1820 v v v 1922 \begin{equation}
1821 where AV, ASL are the constants of integration discussed in the 1923 S_v = n\left[C_v\cdot\ln{T} + R\cdot \ln{\left(V/n\right)} + A_v\right]
1822 Si 1924 \end{equation}
1925 \begin{equation}
1926 S_\ell = (N-n)\left[C_\ell\cdot \ln{T}+A_\ell\right]
1927 \end{equation}
1928
1929 where $A_v$, $A_\ell$ are the constants of integration discussed in the
1823 last Section. 1930 last Section.
1931
1932
1824 We leave it as an exercise for the reader to complete the 1933 We leave it as an exercise for the reader to complete the
1825 derivation from this point , and show that the total entropy 1934 derivation from this point, and show that the total entropy
1826 S = 82 + SV is maximized subject to the constraint (1-6 3) , when 1935 $S = S_\ell + S_v$ is maximized subject to the constraint (1-63), when
1827 R 1936 the values $n_{eq}$, $T_{eq}$ are related by
1828 the values 11 , T are related by 1937
1829 eq eq 1938 \begin{equation}
1939 \frac{n_{eq}}{V}= B\cdot T_{eq}^a\cdot \exp{\left(-\frac{L}{RT_{eq}}\right)}
1940 \end{equation}
1941
1942 where $B\equiv \exp{(-1-a-\frac{A_\ell-A_v}{R})}$ and $a\equiv
1943 (C_v-C_\ell)/R$ are constants.
1944
1945
1830 Equation (1-66) is recognized as an approximate form of the Vapor 1946 Equation (1-66) is recognized as an approximate form of the Vapor
1831 pressure formula . 1947 pressure formula
1832 We note that AQ, AV, which appeared first as integration 1948 We note that AQ, AV, which appeared first as integration
1833 constants for the entropy with no parti cular physical meaning , 1949 constants for the entropy with no parti cular physical meaning,
1834 now play a role in determining the vapor pressure. 1950 now play a role in determining the vapor pressure.
1835 l.ll The Second Law: Discussion. We have emphasized the dis 1951
1836 tinction between the weak and strong forms of the second law 1952 ** The Second Law: Discussion
1837 because (with the exception of Boltzmann ' s original unsuccessful 1953
1838 argument based on the H—theorem) , most attempts to deduce the 1954 We have emphasized the distinction between the weak and strong forms
1839 second law from statis tical mechanics have considered only the 1955 of the second law
1956 because (with the exception of Boltzmann's original unsuccessful
1957 argument based on the H-theorem), most attempts to deduce the
1958 second law from statistical mechanics have considered only the
1840 weak form; whereas it is evidently the strong form that leads 1959 weak form; whereas it is evidently the strong form that leads
1841 to definite quantitative predictions, and is therefore needed 1960 to definite quantitative predictions, and is therefore needed
1842 1961 for most applications. As we will see later, a demonstration of
1962 the weak form is today almost trivial---given the Hamiltonian form
1963 of the equations of motion, the weak form is a necessary
1964 condition for any experiment to be reproducible. But demonstration
1965 of the strong form is decidedly nontrivial; and we recognize from
1966 the start that the job of statistical mechanics is not complete
1967 until that demonstration is accomplished.
1968
1969
1970 As we have noted, there are many different forms of the
1971 seoond law, that have been favored by various authors. With
1972 regard to the entropy statement of the second law, we note the
1973 following. In the first place, it is a direct statement of
1974 experimental fact, verified in many thousands of quantitative
1975 measurements, /which have actually been performed/. This is worth a
1976 great deal in an age when theoretical physics tends to draw
1977 sweeping conclusions from the assumed outcomes of
1978 \ldquo{}thought-experiments.\rdqquo{} Secondly, it has stood the test
1979 of time; it is the entropy statement which remained valid in the case
1980 of negative spin temperatures, where some others failed. Thirdly, it
1981 is very easy to apply in practice, the weak form leading
1982 immediately to useful predictions as to which processes will go and
1983 which will not; the strong form giving quantitative predictions
1984 of the equilibrium state. At the present time, therefore, we
1985 cannot understand what motivates the unceasing attempts of many
1986 textbook authors to state the second law in new and more
1987 complicated ways.
1988
1989 One of the most persistent of these attempts involves the
1990 use of [[http://en.wikipedia.org/wiki/Second_law_of_thermodynamics#Principle_of_Carath.C3.A9odory][Carath\eacute{}odory's principle]]. This states that, in the
1991 neighborhood of any thermodynamic state there are other states which
1992 cannot be reached by an adiabatic process. After some mathematical
1993 analysis
1994 [Margenau and Murphy (1943), pp. 26-31; or Wannier (1966),
1995 pp. 126-132]
1996 one infers the existence of a state function (entropy) which tends
1997 to increase; or at least, cannot decrease. From a /mathematical/
1998 standpoint there can be no objection at all to this; the analysis
1999 is quite rigorous. But from a /physical/ standpoint it is subject
2000 to the same objection that its premise is an impossibility
2001 statement, and therefore not an experimental fact.
2002 Indeed, the conclusion of Carath\eacute{}odory's
2003 argument is a far more direct statement of observed fact than its
2004 premise; and so it would seem more logical to use the argument
2005 backwards. Thus, from the experimental fact that the entropy
2006 tends to increase, we would infer that there must exist
2007 neighboring states inaccessible in an adiabatic process; but the
2008 result is then trivial. In a similar way, other impossibility
2009 statements follow trivially from the entropy statement of the
2010 second law.
2011
2012
2013 Finally, we note that all statements of the second law are
2014 subject to a very important qualification, not always sufficiently
2015 emphasized. As we stress repeatedly, conventional thermodynamics
2016 is a theory only of states of thermal equilibrium; such concepts
2017 as temperature and entropy are not even defined for others.
2018 Therefore, all the above statements of the second law must be under
2019 stood as describing only the /net result/ of processes /which begin
2020 and end in states of complete thermal equilibrium/. Classical
2021 thermodynamics has nothing to say about processes that do not
2022 meet this condition, or about intermediate states of processes
2023 that do. Again, it is nuclear magnetic resonance (NMR)
2024 experiments which provide the most striking evidence showing how
2025 essential this qualification is; the spin-echo experiment
2026 (Hahn, 1950) is, as we will see in detail later, a gross violation of
2027 any statement of the second law that fails to include it.
2028
2029
2030 This situation has some interesting consequences, in that
2031 impossibility statements may be misleading if we try to read too
2032 much into them. From classical thermodynamics alone, we cannot
2033 logically infer the impossibility of a \ldquo{}perpetual motion machine\rdquo{}
2034 of the second kind (i.e., a machine which converts heat energy
2035 into useful work without requiring any low temperature heat sink,
2036 as does the Carnot engine); we can infer only that such a machine
2037 cannot operate between equilibrium states. More specifically, if
2038 the machine operates by carrying out some cyclic process, then
2039 the states of (machine + environment) at the beginning and end
2040 of a cycle cannot be states of complete thermal equilibrium, as
2041 in the reversible Carnot engine. But no real machine operates
2042 between equilibrium states anyway. Without some further analysis
2043 involving statistical mechanics, we cannot be at all certain that
2044 a sufficiently clever inventor could not find a way to convert
2045 heat energy into useful work on a commercially profitable scale;
2046 the energy is there, and the only question is whether we could
2047 persuade it to \ldquo{}organize\rdquo{} itself enough to perform useful work
2048 against pistons, magnets, gravitational or electric fields,
2049 chemical activation energy hills, etc.
2050
2051
2052 It was Maxwell himself who first ([[../sources/Maxwell-Heat.pdf][1871]])[fn::See also, the [[http://openlibrary.org/books/OL7243600M/Theory_of_heat][Open Library
2053 page]], where you can read and download Maxwell's book in a variety of formats.] suggested such
2054 possibilities, in his invention of the \ldquo{}Maxwell Demon\rdquo{},
2055 an imaginary being (or mechanism) which can regulate valves so as to allow
2056 fast molecules to pass through a partition in one direction only,
2057 thus heating up one side at the expense of the other. We could
2058 then allow the heat to flow back from the hot side to the cold
2059 through a conventional Carnot engine, generating useful work; and
2060 the whole arrangement would constitute a perpetual motion machine
2061 of the second kind.
2062
2063 #http://naca.larc.nasa.gov/search.jsp?R=19760010893&qs=Ns%3DLoaded-Date|1%26N%3D4294709597
2064
2065 Maxwell did not regard such a device as impossible in principle;
2066 only very difficult technically. Later authors ([[../sources/Szilard.pdf][Szilard, 1929]];
2067 Brillouin, 1951, 1956)
2068 have argued, on the basis of quantum
2069 theory or connections between entropy and information, that it
2070 fundamentally impossible. However, all these arguments seem
2071 to contain just enough in the way of questionable assumptions or
2072 loopholes in the logic, as to leave the critical reader not quite
2073 convinced. This is particularly so when we recall the lessons
2074 of history; clever experimenters have, over and over again, made
2075 fools of theorists who were too quick to assert that something
2076 cannot be done.
2077
2078
2079 A recent example worth recalling concerns the Overhauser
2080 effect in magnetic resonance (enhancement of the polarization
2081 of one set of spins by irradiation of another set coupled to them).
2082 When this effect was first proposed, several well-known
2083 authorities on thermodynamics and statistical mechanics ridiculed the
2084 suggestion and asserted that the effect could not possibly exist,
2085 because it violated the second law of thermodynamics. This
2086 incident is a valuable reminder of how little we really understand
2087 the second law, or how to apply it in new situations.
2088
2089 In this connection, there is a fascinating little gadget
2090 known as the Hilsch tube or Vortex tube, in which a jet of
2091 compressed air is injected into a pipe at right angles to its
2092 axis, but off center so that it sets up a rapid rotational
2093 motion of the gas. In some manner, this causes a separation of
2094 the fast and slow molecules, cold air collecting along the axis
2095 of the tube, and hot air at the walls. On one side of the jet,
2096 a diaphragm with a small hole at the center allows only the cold
2097 air to escape, the other side is left open so that the hot air
2098 can escape. The result is that when compressed air at room
2099 temperature is injected, one can obtain air from the hot side
2100 at +100^\circ F from the cold side at -70^\circ F, in sufficient quantities
2101 to be used for quick-freezing small objects, or for cooling
2102 photomultiplier tubes [for construction drawings and experi
2103 mental data, see Stong (1960); for a partial thermodynamic
2104 analysis, see Hilsch (19-47)].
2105
2106 Of course, the air could also be cooled by adiabatic expansion
2107 (i.e., by doing work against a piston); and it appears that
2108 the amount of cooling achieved in vortex tubes is comparable to,
2109 but somewhat less than, what could be obtained this way for the
2110 same pressure drop. However, the operation of the vortex tube
2111 is manifestly not simple adiabatic since no work is
2112 done; rather, part of the gas is heated up, at the cost of cooling
2113 the rest; i.e., fast and slow molecules are separated spatially.
2114 There is, apparently, no violation of the laws of thermodynamics,
2115 since work must be supplied to compress the air; nevertheless,
2116 the device resembles the Maxwell Demon so much as to make one
2117 uncomfortable.. This is so particularly because of our
2118 embarrassing inability to explain in detail (i.e., in molecular terms)
2119 how such asimple device works. If we did understand it, would
2120 we be able to see still more exciting possibilities? No one
2121 knows.
2122
2123
2124 It is interesting to note in passing that such considerations
2125 were very much in Planck's mind also; in his [[http://books.google.com/books?id=kOjy3FQqXPQC&printsec=frontcover][/Treatise on Thermodynamics/]] (Planck, 1897; 116), he begins his discussion
2126 of the second law in these words (translation of A. Ogg):
2127 #+begin_quote
2128 \ldquo{}We
2129 $\ldots$ put forward the following proposition $\ldots$ :
2130 /it is impossible to construct an engine which will work a complete cycle,
2131 and produce no effect except the raising of a weight and the cooling of a heat-reservoir./ Such an engine could be used simultaneously
2132 as a motor and a refrigerator without any waste of energy or
2133 material, and would in any case be the most profitable engine
2134 ever made. It would, it is true, not be equivalent to perpetual
2135 motion, for it does not produce work from nothing, but from the
2136 heat which it draws from the reservoir. It would not, therefore,
2137 like perpetual motion, contradict the principle of energy, but
2138 would nevertheless possess for man the essential advantage of
2139 perpetual motion, the supply of work without cost; for the in
2140 exhaustible supply of heat in the earth, in the atmosphere, and
2141 in the sea, would, like the oxygen of the atmosphere, be at
2142 everybody ‘s immediate disposal. For this reason we take the
2143 above proposition as our starting point. Since we are to deduce
2144 the second law from it, we expect, at the same time, to make a
2145 most serviceable application of any natural phenomenon which may
2146 be discovered to deviate from the second law.\rdquo{}
2147 #+end_quote
2148 The ammonia maser ([[../sources/Townes-Maser.pdf][Townes, 1954]]) is another example of an
2149 experimental device which, at first glance, violates the second
2150 law by providing \ldquo{}useful work\rdquo{} in the form of coherent microwave
2151 radiation at the expense of thermal energy. The ammonia molecule
2152 has two energy levels separated by 24.8 GHz, with a large electric
2153 dipole moment matrix element connecting them. We cannot obtain
2154 radiation from ordinary ammonia gas because the lower state
2155 populations are slightly greater than the upper, as given by
2156 the usual Boltzmann factors. However, if we release ammonia gas
2157 slowly from a tank into a vacuum so that a well-collimated jet
2158 of gas is produced, we can separate the upper state molecules
2159 from the lower. In an electric field, there is a quadratic
2160 Stark effect, the levels \ldquo{}repelling\rdquo{} each other according to
2161 the well-known rule of second-order perturbation theory. Thus,
2162 the thermally excited upper-state molecules have their energy
2163 raised further by a strong field; and vice versa for the lower
2164 state molecules. If the field is inhomogeneous, the result is
2165 that upper-state molecules experience a force drawing them into
2166 regions of weak field; and lower-state molecules are deflected
2167 toward strong field regions. The effect is so large that, in a
2168 path length of about 15 cm, one can achieve an almost complete
2169 spatial separation. The upper-state molecules then pass through
2170 a small hole into a microwave cavity, where they give up their
2171 energy in the form of coherent radiation.
2172
2173
2174 Again, we have something very similar to a Maxwell Demon;
2175 for without performing any work (since no current flows to the
2176 electrodes producing the deflecting field) we have separated
2177 the high-energy molecules from the low-energy ones, and obtained
2178 useful work from the former. This, too, was held to be
2179 impossible by some theorists before the experiment succeeded!
2180
2181 Later in this course, when we have learned how to formulate
2182 a general theory of irreversible processes, we will see that the
2183 second law can be extended to a new principle that tells us which
2184 nonequilibrium states can be reached, reproducibly, from others;
2185 and this will of course have a direct bearing on the question of
2186 perpetual motion machines of the second kind. However, the full
2187 implications of this generalized second law have not yet been
2188 worked out; our understanding has advanced just to the point
2189 where confident, dogmatic statements on either side now seem
2190 imprudent. For the present, therefore, we leave it as an open
2191 question whether such machines can or cannot be made.
1843 2192
1844 2193
1845 * COMMENT Appendix 2194 * COMMENT Appendix
1846 2195
1847 | Generalized Force | Generalized Displacement | 2196 | Generalized Force | Generalized Displacement |