1b_ Physical Transformations of Pure Substances.ppt
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Physical Transformations of Pure Substances
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Language: en
Added: Oct 20, 2024
Slides: 21 pages
Slide Content
Chapter 6: Physical Transformations of Pure
Substances
Homework:
Exercises(a only):4, 5, 8, 12, 15
Problems:4, 6,10, 15, 21
Phase Diagrams
Phase - a form of matter that is uniform throughout in chemical
composition and physical state (J. Willard Gibbs)
»Homogeneous - one phase present, e.g., glass of cracked ice (not including
the glass)
»Heterogeneous - more than one phase, e.g., glass of cracked ice with water
Phase transition - spontaneous conversion of one phase to a another
»Occurs at characteristic temperature for a given pressure, transition temperature, T
trs
» At T
trs
, phases are in equilibrium and Gibbs energy minimized
Example ice and water at 0°C
»This says nothing about the rate the transition occurs
Graphite is the stable phase of carbon at R.T., but diamonds exist because rate of
thermodynamically “spontaneous” to low
Such kinetically persistent unstable phases are called metastable phases
Phase Diagram is a P,T plot showing regions of
thermodynamically stable phases
»Lines separating phases are called phase boundaries
Vapor-liquid boundary shows variation of vapor pressure with temperature
Solid-liquid boundary shows variation of sublimation pressure with temperature
Phase Boundaries (cont.)
Boiling Points
»Temperature at which vapor pressure equals external pressure
Normal boiling point (T
b
) external pressure = 1 atm (H
2
O: 100.0°C)
Standard boiling point external pressure = 1 bar (0.987 atm) (H
2O: 99.6°C)
Critical Point
»In closed vessel boiling does not occur. Pressure increases and fluid level drops.
liquid
decreases and
vapor
increase as T increases
At some point
liquid
=
vapor
and boundary disappears: critical temperature
(T
c
),vapor pressure is critical pressure, p
c
Above a single uniform phase exists, supercritical fluid
Highest temperature liquid can exist
Melting Points
»Melting temperature both solid and liquid phases exist.
Equivalent to freezing temperature
Normal freezing(melting) point (T
f
) external pressure = 1 atm (H
2
O: 0°C)
Standard freezing point external pressure = 1 bar (0.987 atm)
Triple Point (T
3
) - place at which 3 phase boundaries meet
»All 3 phases exist simultaneously
»Typically solid, liquid and gas
Lowest pressure and temperature liquid can exist
»Invariant, property of substance (H
2O: 273.15K, 6.11 mbar)
p
c
T
b
1 atm = p
ex
supercritical fluid
Phase Diagrams - Water
Slope of solid-liquid boundary means
large p necessary to significantly change
melting temp.
»Negative slope means T
melt decreases as p
increase
Due to structure of water
Liquid has lower volume than solid
(
liquid
>
solid
)
High pressure phases
»Different crystal structure and density
Ice I (hexagonal); Ice III (Tetragonal)
At -175°C and 1 atm: Ice I (= 0.94 g/cc);
Ice VI (= 1.31 g/cc);
»Can melt at higher temperatures than Ice I
Ice VII melts at 100°C but only exists at
p>25 kbar
8 triple points (6 plotted)
»Only one between solid (Ice I), liquid and
gas
Ice VI,VII, VIII
21 kbar, ~5 °C
Ice VI,VII, liquid
22 kbar, 81.6 °C
Phase Diagrams - Carbon Dioxide
Melting temperature increases a p
increases
»Unlike water& more typical
T
3 > 1 atm
»Liquid CO
2 doesn’t exist at 1 atm
High pressure CO
2 tanks contain liquid
At 25°C (298.15 K) and 67 atm, gas and
liquid co-exist
Phase Diagrams - Helium
Note temperature scale (< 6K)
Solid and gas never in equilibrium
Two liquid phases
»Phase boundary -line (type of phase transition)
»Higher temperature liquid (He-I) is regular
liquid
»Low temperature liquid (He-II) superfluid (zero
viscosity)
It rather than solid exists close to 0K
3
He
4
He
Phase diagram depends on nuclear spin
»
3
H - non-zero spin,
4
H -zero spin
»3
H diagram different than 4
3
H, esp. low
temperature
3
H S
liquid < Ssolid, melting exothermic
Gibbs Energies and Phase Diagrams
Chemical potential (µ) - for one component system µ =Gm
»Measure of the potential of a substance to bring about change
»More detail in Chapters 7 & 9
At equilibrium, µ is the same throughout the system
»Regardless of number of phases
»If µ
1 is chem. potential of phase 1 and µ
2 is chem. potential of phase 2, at
equilibrium µ
1 = µ
2
Consequence of 2
nd
Law of Thermodynamics
If dn is transferred from one location (phase) to another, -µ
1dn, is the
change in Gibbs energy in that phase and µ
2dn is change in free energy in
the second phase.
dG = -µ
1dn + µ
2dn = (µ
2 - µ
1)dn
If µ
1 > µ
2 dG < 0 and change spontaneous
If µ
1 = µ
2 dG = 0 and system at equilibrium
Transition temperature is that temperature where µ
1 = µ
2
Chemical potentials of phases change with temperature
»At low T and reasonable p, solid has lowest µ and, hence, most stable
»As T raised, µ of other phase may become less than solid(at that temp.) so it
becomes stable phase
T and p Dependence on Melting
Recall, (∂G/∂T)
p
= -S so (∂µ/∂T)
p
= -S
m
»Since S
m
> 0 for all pure substances, (∂µ/∂T)
p
< 0 or a plot of µ
vs. T will have a negative slope
»Because S
m
(gas)> S
m
(liquid)> S
m
(solid)> slopes going from gas
solid increasingly negative
Transitions (melting, vaporization) occur when µ of one phase
becomes greater than another so substances melt when
µ(liquid)>µ(solid)
Phase change means modifying relative values of µ for each phase
Given differences in slopes, change in T easiest way to do it
Similarly, (∂G/∂p)
T = V so (∂µ/∂T)
p = V
m
»Because V
m
increases with p, graph of µ vs. T translates
upward as p increases
For most substances V
m(l)> V
m(s), µ(l) increases more than µ(s),
T
f increases as p increases (a)
Consistent with observations and physical sense higher p retards
movement to lower density
Water exception since V
m(s)> V
m(l), as p increases µ(s) increases
more than µ(l), so T
f decreases as p increases (b)
V
m
(l)> V
m
(s)
V
m
(s)> V
m
(l)
Assessing Effect of Pressure on Melting
Example 6.1
Calculate µ for each state over pressure range, µ (water) p = 1 bar; µ (ice) p = 1 bar
µ (water) = 1.80 J mol
-1
and µ (ice) = 1.97 J mol
-1
J mol
-1
are units of µ just like G
µ (water) < µ (ice), so tendency for ice to melt
Look at Self Test 6.2 (opposite of water)
p
T
V
m,whereV
misthemolarvolume
But,V
mM/,wheredensityandMmolarmass
p
T
M/
Overfinitechangeinpresure
M/dp
p1
p2
M/p
Effect of Pressure on Vapor Pressure
When pressure applied to a condensed phase
(solid or liquid), vapor pressure increases, i.e.,
molecules move to gas phase
»Increase in p can be mechanical or with inert gas
Ignore dissolution of pressurizing gas in liquid
Ignore gas solvation, attachment of liquid molecules
to gas-phase species
»Vapor pressure in equilibrium with condensed
phase is the partial vapor pressure of the
substance, p*
p = p*e
VmP/RT
[1]
Math Moment: e
x
= 1+ x + 1/2x
2
+….
If x<<1, .e ≈ 1 + x
Since(g)(l)atequilibrium,
d(g)d(l)whenadditionalexternalpressuredPappplied
d(l)V
m
(l)dPandd(g)V
m
(g)dP
Foridealgas,V
m
(g)
RT
p
so,
V
m(l)dp
RT
p
dp
IntegratingfromP
1
toP
2
PP
2
P
1 ,
V
m
(l)dp
P1
P2
RT
p
dp
P1
P2
ifnoadditonalpressure,pP
1p*,
withexternalpressure,P,ppP
pPp(effectofpressuresmall),sointegralsbecome
V
m(l)dp
p*
p*P
RT
p
dp
p*
p
V
mPRTln
p
p*
exponetiate
p
p*
e
V
mP
RT
orpp*e
V
mP
RT
Proof
[1] becomes
p = p*(1 + V
m
P/RT)
If V
mP/RT<<1
orpp*
p*
V
mP
RT
Location of Phase Boundaries
Phase boundaries occur when chemical potentials are equal and phases are in
equilibrium, or for phases and :
µ
(p,T) = µ
(p,T)
»Need to solve this equation for p, p= f(T)
»On plot of p vs. T, f(T) is a gives the phase boundary
Slopes of phase boundaries
»Slope is dp/dT
If p and T are changed such that two phases, and , are in equilibrium, dµ
= dµ
But, dµ = -S
mdT + Vdp
So, -S
m,
dT + V
m
dp = -S
m,
dT + V
m
dp
Or (S
m,-S
m,dT + = (V
m
- V
m )dp
But (S
m,- S
m, =
trsS and (V
m - V
m
) =
trsV
This rearranges to:
dp/dT =
trs
S /
trs
V
where and are the entropy and volume of transition
»This is called the Clapeyron Equation
Exact expression for the phase boundary at equilibrium
Can be used to predict appearance of phase diagrams and form of boundaries
µ
=
µ
Solid-Liquid Boundary
For solid-liquid boundary, Clapeyron Equation becomes
dp/dT =
fusS /
fusV
where
fusV is the change in molar volume on melting
fus
S is always positive (except for
3
He) and
fus
V is usually small so dp/dT is large (steep
slope) and positive
Formula for phase boundary comes from integrating Clapeyron equation
dp
fusS
fus
V
dT
recall
trsS
trsH
T
,so
dp
fusH
T
fus
V
dT
Integrating
dp
p*
p
fusH
fusV
1
TT*
T
dT,whereT*ismeltingtemperature@p*
pp*
fusH
fusV
ln
T
T*
IfTclosetoT*,ln
T
T*
ln1
TT*
T
pp*
fusH
fus
V
ln1
TT*
T
Math Moment: ln(1+x) = x - 1/2x
2
+….
If x<<1, ln(1 + x) = x
pp*
fus
H
fusV
ln1
TT*
T*
pp*
fus
H
fusV
TT*
T*
or
pp*
fus
H
fusV
TT*
T*
pp*
fus
H
T*
fusV
TT*
This is straight line of slope
[
fus
H / (T*
fus
V)]
Liquid Vapor Boundary
Again, Clapeyron equation can be used
»
vap
V is large and positive so dp/dT is positive, but smaller than for solid-liquid transition
»
vap
H/T is Trouton’s constant
»Because V
m(gas) >> V
m(liquid),
vapV ≈ V
m(gas)
For ideal gas, V
m
(gas) = RT/p so
vap
V ≈ RT/p
Clapeyron equation becomes
dp
dT
vap
H
T
vap
V
dp
dT
vapH
T
vap
V
vapH
T
RT
p
p
vapH
RT
2
1
p
dp
dT
vapH
RT
2
Recall
dx
x
dlnx
d(lnp)
dT
vapH
RT
2
ClausiusClapeyronEquation
Integrating Clausius-Clapeyron equation gives variation of vapor pressure with temperature
As s umes
v a p
H is in depend ent of T and
p* is v apor pres s ure at T*
and p the vap or pres s ure a t T
»This is a curve, not a line
»Does not extend beyond T
c
pp*e
,
vap
H
R
1
T
1
T*
Solid-Vapor Boundary
Solid-vapor boundary same as
liquid vapor boundary except
use
sub
H instead of
vap
H
Since
sub
H >
vap
H, slope of
curve is steeper
Curves coincide at triple point
along with solid-liquid
boundary
Classification of Phase Transitions
Ehrenfest Clasification
We’ve been talking a lot about the slopes of phase transitions, (∂µ/∂T)
p
or (∂µ/∂V)
T
»Transitions are accompanied by changes in entropy and volume
At transition from a phase, , to another phase,
(∂µ
/∂T)
p - (∂µ
/∂T)
p = -S
,m + S
,m = - S
trs = -
trsH/T
(∂µ
/∂p)
T - (∂µ
/∂p)
T = V
,m - V
,m = -
trsV
1st Order Transitions (e.g., melting, vaporization)
»Since
fus
H,
vap
H and
fus
V,
vap
V are non-zero, the changes in µ {(∂µ/∂T)
p
or (∂µ/∂p)
T
} as you
approach the transition are different.
There is a discontinuity at the transition
A transition in which the slope of µ, (∂µ/∂T)
p , is discontinuous is called a 1st order
transition
C
p
is slope of plot of H vs. T (∂H/∂T)
p
at 1st order transition is infinite
Infinitesimal change in T produces finite change in H
T
trs
V,
H.
S
T
trs
µ
T
trs
C
p
Classification of Phase Transitions
Ehrenfest Classification (continued)
2nd Order Transition (glass transition, superconducting to conducting transition)
»(∂µ/∂T)
p
, is continuous
Volume and entropy don’t change at transition
»(∂
2
µ/∂T
2
)
p
is discontinuous
»Heat capacity is discontinuous, but not infinite
T
trs
C
p
T
trs
µ
T
trs
V,
S,
H
-Transition (
4
He super-fluid to liquid transition,
order-disorder transition in -brass)
»Not 1st order, (∂µ/∂T)
p
, is continuous
»Heat capacity is discontinuous, and infinite at
transition temperature
Liquid Surfaces
Surface effects can be expressed in terms of thermodynamic functions since
work is required to change the surface area of a liquid
»If is the surface area of a liquid, d is its infinitesimal change when an amount of
work, dw is done
»dw is proportional to the surface area of the liquid, i.e.,
dw = d
the proportionality constant is defined as the surface tension
Dimensions of : energy/area (J/m
2
or N/m)
To calculate the work needed to create or change a surface by a particular area increment
you only need to calculate the area since is a constant
Look at Self Test 6.4
At constant volume and temperature the work is the Helmholtz energy (A)
dA = d
»As d decreases the Helmholtz energy minimizes
This is the direction of spontaneous change so surfaces of liquids tend to contract
Often minimizing of dA results in curved surfaces
Curved Liquid Surfaces
Bubble - a region in which vapor (+ air) is trapped by thin
film
»Bubbles have 2 surfaces one on each side of the film
»Cavity is a vapor-filled hole in liquid (commonly called
bubbles) but 1/2 the surface area
»Droplet - small volume of liquid surrounded by vapor (+air)
Pressure inside a concave surface (p
in
) is always greater
than pressure outside (p
out
)
»Difference depends on surface area and surface tension
p
in = p
out + 2/r Laplace
eqn
forspheretheoutwardforceis
p
inarea4r
2
p
in
theinwardforcecomesfrom
Fexternalpressure Fsurfacetension
sufacetension
dwd
d4rdr
2
4r
2
d4r
2
2rdrdr
2
2
4r
2
d8rdr4dr
2
Ignore4dr
2
(small)sod8rdr
dw8rdr
SincewFdorFw
d
F
in
surfacetension
dw
dr
8r
externalpressure
F
inpressure 4r
2
p
out
Atequilibrium,F
outF
inor
4r
2
p
in4r
2
p
out8r
rp
in
rp
out
2
p
inp
out
2
r
Laplaceequation
As r ∞ (flat surface), p
in
= p
out
As r small(small bubbles), 2/r
important
»Earlier we saw, the vapor pressure in the presence of external pressure p is
p = p*e
VmP/RT
So, for bubble since p = 2/r
p = p*e
2Vm/rRT
Kelvin Equation (bubble)
In a cavity, p
out < p
in, so sign of exponential term is reversed
p = p*e
-2Vm/rRT
Kelvin Equation (cavity)
Nucleation, Superheating &Supercooling
Nucleation
»For water droplets
r =1µm; @25°C, p/p* = 1.001
Small effect but mat have important consequences
r =1nm; @25°C, p/p* = 3
»Clouds form when water droplets condense. Warm moist air rises, condenses at colder altitude
Initial droplets small so Kelvin equation tells us vapor pressure of droplet increases
Small droplets tend to evaporate
Unless large numbers of molecules congregate (spontaneous nucleation)
Air becomes supersaturated and thermodynamically unstable
Nucleation centers (dust particles, sea salt) allow clouds to form by allowing condensation
to occur on larger surfaces
Superheating - liquids persist above boiling point
»Vapor pressure inside a small cavity in liquid is low so cavities tend to collapse
Spontaneous nucleation causes larger more stable cavities (and bumping!)
Nucleation centers allow for stabilization of cavity
Basis of bubble chamber
»Supercooling, persistence of liquids past freezing point, is analogous
Capillaries
Capillary action - tendency of liquids to rise up/fall in narrow
bore (capillary) tubes
Capillary rise/fall
»If liquid has tendency to adhere to the tube walls (e.g. water),
energy lowest when most surface is covered
Liquid creeps up wall (concave meniscus)
Pressure beneath curve of meniscus is lower than atmosphere
by 2/r, where r is radius (Kelvin equation, cylindrical tube)
Pressure at flat surface = atmospheric pressure (r ∞)
»Liquid rises in capillary until hydrostatic equilibrium is reached
As liquid rises p increases by gh ( = density; h= height)
At equilibrium, p
capillary
= p
external
or
2/r = gh
Height of capillary rise h = 2/gr
As tube gets smaller, h gets higher
Can be used to measure surface tension of liquids
is temperature dependent
»If liquid has a tendency not to adhere (e.g. Hg) liquid will fall in
capillary because pressure less under meniscus
Treatment the same, except sign reversed
Contact Angle
Contact angle is the angle between edge of meniscus and wall
»If
c ≠ 0, then the equation for capillary rise becomes
h = 2Cosc/gr
Arises from balance of forces at the point of contact between liquid and solid
»The surface tension is essentially the energy needed to create a unit area of each of the interfaces
sg
= Energy to create unit area at gas-solid interface
lg = Energy to create unit area at gas-liquid interface
sl = Energy to create unit area at solid-liquid interface
»At equilibrium, the vertical forces in capillary are in balance so
sg
=
sl
+ Cos(
c
)
lg
Or Cos(
c
) =(
sg
-
sl
)/
lg
See diagram
»
Work of adhesion (w
ad
) of liquid to solid is
sg
+
lg -
sl
»
So Cos(
c
) =(
sg
-
sl
)/
lg
=(w
ad
-
lg
)/
lg =(w
ad
/
lg
) - 1
If liquid wets surface 0° <
c < 90° , 1> Cos(
c) 0 so 1< (wad / lg ) 2
If liquid doesn’t wet surface 90° <
c
< 180° , 0> Cos(
c
) -1 so 1> (wad / lg ) 0
Takes more work to overcome cohesive forces in liquid
“wets”
“doesn’t wet”