a After heating to 320 K at constant pressure, the system is still gaseous.. b Isothermal compression at 320 K to 100 atm pressure brings the sample into the supercritical region.. c Aft
Trang 1pure substances
Solutions to exercises
Discussion questions
E6.1(b) Refer to Fig 6.8 The white lines represent the regions of superheating and supercooling The chemical
potentials along these lines are higher than the chemical potentials of the stable phases represented by the colored lines Though thermodynamically unstable, these so-called metastable phases may persist for a long time if the system remains undisturbed, but will eventually transform into the thermo-dynamically stable phase having the lower chemical potential Transformation to the condensed phases usually requires nucleation centers In the absence of such centers, the metastable regions are said to be kinetically stable
E6.2(b) At 298 K and 1.0 atm, the sample of carbon dioxide is a gas (a) After heating to 320 K at constant
pressure, the system is still gaseous (b) Isothermal compression at 320 K to 100 atm pressure brings the sample into the supercritical region The sample is now not much different in appearance from ordinary carbon dioxide, but some of its properties are (see Box 6.1) (c) After cooling the sample to
210 K at constant pressure, the carbon dioxide sample solidifies (d) Upon reducing the pressure to 1.0 atm at 210 K, the sample vapourizes (sublimes); and finally (e) upon heating to 298 K at 1.0 atm, the system has resumed its initial conditions in the gaseous state Note the lack of a sharp gas to liquid transition in steps (b) and (c) This process illustrates the continuity of the gaseous and liquid states
E6.3(b) First-order phase transitions show discontinuities in the first derivative of the Gibbs energy with
respect to temperature They are recognized by finite discontinuities in plots ofH , U, S, and V
against temperature and by an infinite discontinuity in C p Second-order phase transitions show discontinuities in the second derivatives of the Gibbs energy with respect to temperature, but the first derivatives are continuous The second-order transitions are recognized by kinks in plots ofH, U, S,
andV against temperature, but most easily by a finite discontinuity in a plot of C pagainst temperature
Aλ-transition shows characteristics of both first and second-order transitions and, hence, is difficult
to classify by the Ehrenfest scheme It resembles a first-order transition in a plot ofC pagainstT , but
appears to be a higher-order transition with respect to other properties See the book by H E Stanley listed under Further reading for more details
Numerical exercises
E6.4(b) Assume vapour is a perfect gas and vapH is independent of temperature
lnp∗
p = +
vapH R
1
T −
1
T∗
1
T =
1
T∗ + R
vapH ln
p∗ p
293.2 K+
8.314 J K−1mol−1
32.7 × 103J mol−1 × ln
58.0
66.0
= 3.378 × 10−3K−1
3.378 × 10−3K−1 = 296 K = 23◦C
Trang 2E6.5(b) dp
dT =
Sm
Vm
fusS = Vm
dp
dT
≈ Vm p T
assuming fusS and Vm independent of temperature
fusS = (152.6 cm3mol−1− 142.0 cm3mol−1) × (1.2 × 106Pa) − (1.01 × 105Pa)
429.26 K − 427.15 K
= (10.6 cm3mol−1) ×
1 m3
106cm3
× (5.21 × 105Pa K−1)
= 5.52 Pa m3K−1mol−1= 5.5 J K−1mol−1
fusH = Tf S = (427.15 K) × (5.52 J K−1mol−1)
= 2.4 kJ mol−1
E6.6(b) Use
d lnp = vapH
RT2 dT
lnp = constant − vapH
RT
Terms with 1
T dependence must be equal, so
−3036.8 K
T /K = −
vapH RT vapH = (3036.8 K)R = (8.314 J K−1mol−1) × (3036.8 K)
= 25.25 kJ mol−1
E6.7(b) (a) logp = constant − vapH
RT (2.303)
Thus
vapH = (1625 K) × (8.314 J K−1mol−1) × (2.303)
= 31.11 kJ mol−1
(b) Normal boiling point corresponds top = 1.000 atm = 760 Torr
log(760) = 8.750 −1625T /K
1625
T /K = 8.750 − log(760)
8.750 − log(760) = 276.87
Tb= 276.9 K
Trang 3E6.8(b) T = fusV
fusS × p =
Tf fusV fusH × p =
Tf pM fusH ×
1
ρ
[Tf = −3.65 + 273.15 = 269.50 K]
T = (269.50 K) × (99.9 MPa)M
8.68 kJ mol−1 ×
1
0.789 g cm−3 − 1
0.801 g cm−3
= (3.1017 × 106K Pa J−1mol) × (M) × (+ 01899 cm3/g) ×
m3
106cm3
= (+ 5.889 × 10−2K Pa m3J−1g−1mol)M = (+ 5.889 × 10−2K g−1mol)M
T = (46.07 g mol−1) × (+ 5.889 × 10−2K g−1mol)
= + 2.71 K
Tf = 269.50 K + 2.71 K = 272 K
dt =
dn
dt × MH 2 O wheren = q
vapH
dn
dt =
dq/dt vapH =
(0.87 × 103W m−2) × (104m2)
44.0 × 103J mol−1
= 197.7 J s−1J−1mol
= 200 mol s−1
dm
dt = (197.7 mol s−1) × (18.02 g mol−1)
= 3.6 kg s−1
E6.10(b) The vapour pressure of ice at −5◦C is 3.9 × 10−3atm, or 3 Torr Therefore, the frost will sublime
A partial pressure of 3 Torr or more will ensure that the frost remains
E6.11(b) (a) According to Trouton’s rule (Section 4.3, eqn 4.16)
vapH = (85 J K−1mol−1) × Tb= (85 J K−1mol−1) × (342.2 K) = 29.1 kJ mol−1
Start Gas
Temperature
a d
Critical point
Figure 6.1
Trang 4(b) Use the Clausius–Clapeyron equation [Exercise 6.11(a)]
ln
p2
p1
= vapH
1
T1− 1
T2
AtT2= 342.2 K, p2= 1.000 atm; thus at 25◦C
lnp1= −
29.1 × 103J mol−1
8.314 J K−1mol−1
×
1
298.2 K−
1
342.2 K
= −1.509
p1= 0.22 atm = 168 Torr
At 60◦C,
lnp1= −
29.1 × 103J mol−1
8.314 J K−1mol−1
×
1
333.2 K−
1
342.2 K
= −0.276
p1= 0.76 atm = 576 Torr
E6.12(b) T = Tf(10 MPa) − Tf(0.1 MPa) = Tf pM
fusH
1
ρ
fusH = 6.01 kJ mol−1
T =
(273.15 K) × (9.9 × 106Pa) × (18 × 10−3kg mol−1)
6.01 × 103J mol−1
×
1
9.98 × 102kg m−3 − 1
9.15 × 102kg m−3
= −0.74 K
Tf(10 MPa) = 273.15 K − 0.74 K = 272.41 K
E6.13(b) vapH = vapU + vap(pV )
vapH = 43.5 kJ mol−1
vap(pV ) = p vapV = p(Vgas− Vliq) = pVgas= RT [per mole, perfect gas]
vap(pV ) = (8.314 J K−1mol−1) × (352 K) = 2927 J mol−1
Fraction= vap(pV )
vapH =
2.927 kJ mol−1
43.5 kJ mol−1
= 6.73 × 10−2 = 6.73 per cent
E6.14(b) Vm= M
ρ =
18.02 g mol−1
999.4 × 103g m−3 = 1.803 × 10−5m3mol−1
2γ Vm
rRT =
2(7.275 × 10−2N m−1) × (1.803 × 10−5m3mol−1) (20.0 × 10−9m) × (8.314 J K−1mol−1) × (308.2 K)
= 5.119 × 10−2
p = (5.623 kPa)e0.05119 = 5.92 kPa
Trang 5E6.15(b) γ = 1
2ρghr = 1
2(0.9956 g cm−3) × (9.807 m s−2) × (9.11 × 10−2m)
× (0.16 × 10−3m) ×
1000 kg m−3
g cm−3
= 7.12 × 10−2N m−1
E6.16(b) pin− pout =2γ
r =
2(22.39 × 10−3N m−1) (220 × 10−9m)
= 2.04 × 105N m−2= 2.04 × 105Pa
Solutions to problems
Solutions to numerical problems
dT =
vapS vapV =
vapH
Tb vapV [6.6, Clapeyron equation]
= 14.4 × 103J mol−1
(180 K) × (14.5 × 10−3− 1.15 × 10−4) m3mol−1 = + 5.56 kPa K−1
(b) dp
dT =
vapH
RT2 × p 11, with d ln p = dp
p
= (14.4 × 103J mol−1) × (1.013 × 105Pa)
(8.314 J K−1mol−1) × (180 K)2 = + 5.42 kPa K−1
The percentage error is 2.5 per cent
∂µ(l)
∂p
T −
∂µ(s)
∂p
T = Vm(l) − Vm(s)[6.13] = M
1
ρ
= (18.02 g mol−1) ×
1
1.000 g cm−3 − 1
0.917 g cm−3
= −1.63 cm3mol−1
(b)
∂µ(g)
∂p
T −
∂µ(l)
∂p
T = Vm(g) − Vm(l)
= (18.02 g mol−1) ×
1
0.598 g L−1 − 1
0.958 × 103g L−1
= + 30.1 L mol−1
At 1.0 atm and 100◦C ,µ(l) = µ(g); therefore, at 1.2 atm and 100◦Cµ(g)−µ(l) ≈ Vvap p = (as in Problem 6.4)
(30.1 × 10−3m3mol−1) × (0.2) × (1.013 × 105Pa) ≈ + 0.6 kJ mol−1
Sinceµ(g) > µ(l), the gas tends to condense into a liquid.
P6.7 The amount (moles) of water evaporated isng=pH 2 OV
RT
The heat leaving the water isq = n vapH
The temperature change of the water is T = −q
nC p,m,n = amount of liquid water
Trang 6Therefore, T = −pH2 OV vapH
RT nC p,m
= −(23.8 Torr) × (50.0 L) × (44.0 × 103J mol−1)
(62.364 L Torr K−1mol−1) × (298.15 K) × (75.5 J K−1mol−1) × 250 g
18.02 g mol−1
= −2.7 K
The final temperature will be about 22◦C
P6.9 (a) Follow the procedure in Problem 6.8, but note thatTb= 227.5◦C is obvious from the data
(b) Draw up the following table
θ/◦C 57.4 100.4 133.0 157.3 203.5 227.5
T /K 330.6 373.6 406.2 430.5 476.7 500.7
lnp/Torr 0.00 2.30 3.69 4.61 5.99 6.63
The points are plotted in Fig 6.2 The slope is−6.4 × 103K, so − vapH
R = −6.4 × 103K,
implying that vapH = +53 kJ mol−1
2.0 2.2 2.4 2.6 2.8 3.0 0
2
4
6
Figure 6.2 P6.11 (a) The phase diagram is shown in Fig 6.3.
Liquid
Solid
Vapour
2 0 –2
–4
–6
–8
0 100 200 300 400 500 600
Liquid–Vapour Solid–Liquid
Figure 6.3
Trang 7(b) The standard melting point is the temperature at which solid and liquid are in equilibrium at
1 bar That temperature can be found by solving the equation of the solid–liquid coexistence curve for the temperature
1= p3/bar + 1000(5.60 + 11.727x)x,
So 11 727x2+ 5600x + (4.362 × 10−7− 1) = 0
The quadratic formula yields
x = −5600 ± {(5600)2− 4(11 727) × (−1)}1/2
−1 ±1+4(11 727)
5600 2
1/2
2
11727 5600
The square root is rewritten to make it clear that the square root is of the form{1 + a}1/2, with
a 1; thus the numerator is approximately −1 + (1 + 1
2a) = 1
2a, and the whole expression
reduces to
x ≈ 1/5600 = 1.79 × 10−4
Thus, the melting point is
T = (1 + x)T3= (1.000179) × (178.15 K) = 178.18 K
(c) The standard boiling point is the temperature at which the liquid and vapour are in equilibrium
at 1 bar That temperature can be found by solving the equation of the liquid–vapour coexistence curve for the temperature This equation is too complicated to solve analytically, but not difficult
to solve numerically with a spreadsheet The calculated answer is T = 383.6 K
(d) The slope of the liquid–vapour coexistence curve is given by
dp
dT =
vapH
T vapV− − so vapH−− = T vapV−−dp
dT
The slope can be obtained by differentiating the equation for the coexistence curve
dp
dT = p
d lnp
dT = p
d lnp
dy
dy
dT
dp
dT =
10.418
y2 − 15.996 + 2(14.015)y − 3(5.0120)y2− (1.70) × (4.7224) × (1 − y)0.70
×
p
Tc
At the boiling point,y = 0.6458, so
dp
dT = 2.851 × 10−2bar K−1= 2.851 kPa K−1
and vapH−−= (383.6 K)×
(30.3 − 0.12) L mol−1
1000 L m−3
×(2.851 kPa K−1) = 33.0 kJ mol−1
P6.12 The slope of the solid–vapour coexistence curve is given by
dp
dT =
subH−−
T subV− − so subH−−= T subV−−dp
dT
The slope can be obtained by differentiating the coexistence curve graphically (Fig 6.4)
Trang 850
40
30
20
10
144 146 148 150 152 154 156
Figure 6.4
dp
dT = 4.41 Pa K−1
according to the exponential best fit of the data The change in volume is the volume of the vapour
Vm= RT
(8.3145 J K−1mol−1) × (150 K)
26.1 Pa = 47.8 m3
So
subH−−= (150 K) × (47.8 m3) × (4.41 Pa K−1) = 3.16 × 104J mol−1= 31.6 kJ mol−1
Solutions to theoretical problems
P6.14
∂ G
∂p
T =
∂G
β
∂p
T −
∂G
α
∂p
T = V β − V α
Therefore, ifV β = V α , G is independent of pressure In general, V β α , so that G is nonzero,
though small, sinceV β − V αis small
P6.16 Amount of gas bubbled through liquid= pV RT
(p = initial pressure of gas and emerging gaseous mixture)
Amount of vapour carried away= M m
Mole fraction of vapour in gaseous mixture= m M m
M +RT pV Partial pressure of vapour= p = m M m
M +RT pV × p =
pP V M mRT
mRT
P V M + 1 =
mP A
mA + 1 , A =
RT
P V M
For geraniol,M = 154.2 g mol−1, T = 383 K, V = 5.00 L, p = 1.00 atm, and m = 0.32 g, so
A = (8.206 × 10−2L atm K−1mol−1) × (383 K)
(1.00 atm) × (5.00 L) × (154.2 × 10−3kg mol−1) = 40.76 kg−1
Therefore
p = (0.32 × 10−3kg) × (760 Torr) × (40.76 kg−1)
(0.32 × 10−3kg) × (40.76 kg−1) + 1 = 9.8 Torr
Trang 9P6.17 p = p0e−Mgh/RT [Box 1.1]
p = p∗e−χ χ = vapR H ×
1
T −
1
T∗
[6.12]
Let T∗ = Tb the normal boiling point; thenp∗ = 1 atm Let T = Th, the boiling point at the altitudeh Take p0 = 1 atm Boiling occurs when the vapour (p) is equal to the ambient pressure,
that is, whenp(T ) = p(h), and when this is so, T = Th Therefore, sincep0 = p∗, p(T ) = p(h)
implies that
e−Mgh/RT = exp
− vapR H ×
1
Th −T1
b
It follows that 1
Th = 1
Tb + Mgh
T vapH
whereT is the ambient temperature and M the molar mass of the air For water at 3000 m, using
M = 29 g mol−1
1
Th = 1
373 K +(29 × 10−3kg mol−1) × (9.81 m s−2) × (3.000 × 103m)
(293 K) × (40.7 × 103J mol−1)
1.397 × 104K Hence,Th= 363 K (90◦C)
P6.20 Sm = Sm(T , p)
dSm=
∂Sm
∂T
p dT +
∂Sm
∂p
T dp
∂S
m
∂T
p = C p,m
T [Problem 5.7]
∂S
m
∂p
T = −
∂V
m
∂T
p [Maxwell relation]
dqrev= T dSm= C p,mdT − T
∂Vm
∂T
p dp
C S =
∂q
∂T
s = C p,m − T Vmα
∂p
∂T
s = C p,m − αVm× Hm
Vm
[6.7]
P6.22 C(graphite)( ) C(diamond) rG− − = 2.8678 kJ mol−1at TC
We want the pressure at which rG = 0; above that pressure the reaction will be spontaneous.
Equation 5.10 determines the rate of change of rG with p at constant T
(1)
∂ rG
∂p
T = rV = (VD− VG)M
whereM is the molar mas of carbon; VD andVG are the specific volumes of diamond and graphite, respectively
rG(TC, p) may be expanded in a Taylor series around the pressure p−−= 100 kPa at TC.
(2) rG(TC, p) = rG−−(TC, p−−) +
∂
rG− −(TC, p− −)
∂p
T (p − p−−)
+1 2
∂2 rG−−(TC, p−−)
∂p2
T (p − p−−)2+ θ(p − p−−)3
Trang 10We will neglect the third and higher-order terms; the derivative of the first-order term can be calculated with eqn 1 An expression for the derivative of the second-order term can be derived with eqn 1
(3)
∂2 rG
∂p2
T
=
∂VD
∂p
T −
∂VG
∂p
T
M = {VGκ T (G) − VDκ T (D)}M [3.13]
Calculating the derivatives of eqns 1 and 2 at TCandp−−
(4)
∂
rG(TC, p− −)
∂p
T = (0.284 − 0.444) ×
cm3 g
×
12.01 g
mol
= −1.92 cm3mol−1
(5)
∂2 rG(TC, p−−)
∂p2
T
= {0.444(3.04 × 10−8) − 0.284(0.187 × 10−8)}
×
cm3kPa−1
g
×
12.01 g
mol
= 1.56 × 10−7cm3(kPa)−1mol−1
It is convenient to convert the value of rG−−to the units cm3kPa mol−1
rG−−= 2.8678 kJ mol−1
8.315 × 10−2L bar K−1mol−1
8.315 J K−1mol−1
×
103cm3 L
×
105Pa bar
(6) rG−− = 2.8678 × 106cm3kPa mol−1
Settingχ = p − p−−, eqns 2 and 3–6 give
2.8678 × 106
cm3kPa mol−1− (1.92 cm3
mol−1)χ + (7.80 × 10−8cm3kPa−1mol−1)χ2= 0 when rG(TC, p) = 0 One real root of this equation is
χ = 1.60 × 106kPa= p − p−−or
p = 1.60 × 106kPa− 102kPa
= 1.60 × 106kPa= 1.60 × 104bar Above this pressure the reaction is spontaneous The other real root is much higher: 2.3×107kPa
Question What interpretation might you give to the other real root?
... can be found by solving the equation of the liquid–vapour coexistence curve for the temperature This equation is too complicated to solve analytically, but not difficultto solve numerically... root is rewritten to make it clear that the square root is of the form{1 + a}1/2, with
a 1; thus the numerator is approximately...
2a) = 1
2a, and the whole expression
reduces to
x ≈ 1/5600 = 1.79 × 10−4
Thus, the melting point is
T