Thermodynamics
Free E and Phase D
J.D. Price
••Force - the acceleration ofForce - the acceleration of matter (N, kg m/smatter (N, kg m/s22))
••Pressure (Pressure (PP) - a force applied over an area) - a force applied over an area
(N/m(N/m22))
••Work (W) -Work (W) - force multiplied by distance (force multiplied by distance (kgkg
mm22/s/s22, Joule), Joule)
••Energy -Energy - enables work (J)enables work (J)
••Temperature (Temperature (TT) - a measurement relating to the) - a measurement relating to the
kinetic (movement) energy of the system (unitskinetic (movement) energy of the system (units
ºC or K)ºC or K)
••Heat (Q) - an energy form relatable toHeat (Q) - an energy form relatable to
temperature (J, but also calories: 1 g water 1 K,)temperature (J, but also calories: 1 g water 1 K,)
E.B. Watson
step 1: heat ice (-20oC - 0oC)
Q1 = (100g)(0.50 cal/goC)(20oC) = 1.0 kcal
step 2: melt ice at 0oC
Q2 = (100g)(80 cal/g) = 8.0 kcal
step 3: heat water (0oC - 100oC)
Q3 = (100g)(1.0 cal/goC)(100oC) = 10.0 kcal
step 4: boil water at 100oC
Q4 = (100g)(540 cal/g) = 54.0 kcal
step 5: heat vapor to 120oC
Q5 = (100g)(0.48 cal/goC)(20oC)
= 0.96 kcal
Example calculation: How much energy is required to heat 100 g
of ice at -20oC to water vapor at 120oC.
The difference
between Q and W is
always the same.
It is the difference in
internal energy (U)
between the 2 states.
So
U2 - U1 = Q - W
or!U = Q - W
E.B. Watson
Ideally, in a heat engine,
if heat is put into the
system to move from
state 1 to state 2 and the
engine then returns to
state 1, the change in
internal energy of the
system is zero, so
Qin = Wout
E.B. Watson
E.B. Watson
The First LawThe First Law
Energy may be converted from one form to another, butEnergy may be converted from one form to another, but
the total amount of energy is the same.the total amount of energy is the same.
!U = -!Utherm - !Umech
Isolated system
Q - heat gained by the system
W - work done on the system!U = Q - W
Thermodynamics – relating heat, work, and energy
An expression of work can be made
using P and V (the steam engine).
Thermal energy (H)
H = U + PV
Q - system heat transfer Q = Cp (T2 - T1)
Where Cp is heat capacity
W - work done on the system W = P (V2 - V1)
H - Enthalpy, a variable that covers internal energy and
the work term U + PV
!U = U2 - U1 = Q - W
U2 - U1 = Q - P (V2 - V1)
U2 - U1 + P (V2 - V1) = Q
U2 - U1 + PV2 - PV1 = Q
(U2 + PV2 ) - ( U1 + PV1 ) = Q
(H2 - H1) = Cp (T2 - T1)
dH = dU + PdV +VdP
if P is constant
dH = dU + PdV
Reactions
A change in phase(s)
Phases A and B react to make phase C
A + B = C
Reversibility - a slight change causes
the reaction to proceed, and the
opposite change reverses it.
P is constant
Reaction: A + B = C + D
HA = UA + PVA
HB = UB + PVB
HPr = UPr +PVPr
HRe = URe +PVRe
Products - Reactants
HPr - HRe = !H = !U +P!V
!H is the latent heat
Positive is exothermic
Negative is endothermic
What of H2Osolid = H2Oliquid?
!U = 0 = Q – W
Okay, but could you go backwards?
E.B. Watson
The Second LawThe Second Law
Heat flows from warmer to cooler bodies. To goHeat flows from warmer to cooler bodies. To go
backwards requires energy or work.backwards requires energy or work.
The second law is also stated: MechanicalMechanical
energy can be converted 100% into heat, butenergy can be converted 100% into heat, but
heat cannot be converted 100% into mechanicalheat cannot be converted 100% into mechanical
energy.energy.
"You can't break even.""You can't break even."
Thermodynamics – relating heat, work, and energy
Heat cannot be converted 100% intoHeat cannot be converted 100% into
mechanical energymechanical energy
Some of the heat is lost, because it
creates disorder in the system.
Entropy
Thermodynamics – relating heat, work, and energy
!SU = dQ / T (rev) = 0
Entropy - the possible ways to combine the
properties of individual particles to produce
the observable properties of the whole
system.
Solids - low S, Liquids - higher S
!S = dq/T (rev)
!U = T!S - P!V or dU = TdS - PdV
Plausible conclusion: the total entropy of the entire
universe is continually increasing.
The "heat death of the universe." At some point, the
universe may run out of heat.
E.B. Watson
The Third Law
The entropy of a perfect crystal at 0 K is zero.
The "Zeroth" Law
Two systems in thermal equilibrium with the
same third system are in thermal equilibrium
with each another.
Thermodynamics – relating heat, work, and energy
Total Energy = bound energy +
free energy
Gibbs Free Energy (G)
G = H - TS -or-
G = U + PV -TS
dG = dU +PdV + VdP - TdS - SdT
G = H - TS
Provided all terms are at the same
conditions!
Since the earth includes a wide range of T
and P (easily measured), and H, S, and V
are often difficult to measure, we would like
to calculate G at different P and T using
steps of H, S, and V.
G = !Hfo - TSo + PVo
Isothermal and Isobaric
dG = dU +PdV - TdS
dG = 0 if reversible
dU = TdS - PdV
dG < 0 if irreversible
dU < TdS - PdV
CaCO3Al2SiO5
Some substituting
Reversible
dG = dU+PdV + VdP - TdS - SdT
dU = TdS - PdV
dGRe = VRedP - SRedT and dGPr = VPrdP - SPrdT
dGRe - dGPr = VRedP - SRedT - VPrdP + SPrdT
!dG = !VdP - !SdT
ddG =G = VVddP P - - SSddTT
!dG = !VdP - !SdT
At equilibrium, !dG = 0
dP/dT = !S/ !V = !H/ (T!V)
Clausius-Clapeyron equation - the
slope of a reaction boundary in P-T
space!!!
Bomb
Reaction Vessel
Calorimeter
The vessel is strong
such that there is
constant P
With a known heat
capacity (Cp) for all
of the calorimeter
parts, we can
determine the energy
of reaction.
!Erxn = -Cp x !TUniv. of Maine
Graphite - Diamond
298 K !Ho
(Kcal/
mole)
So
(cal/
mole K)
!Go
(Kcal/
mole)
Vo
(cm3/
mole)
Graphite 0 1.372 0 5.2982
Diamond 0.453 0.568 0.693 3.4166
Reaction is Cgraphite= Cdiamond
!" = !Hfo
di # !Hfo
gr = 453 - 0 = 453 (cal/mole)
!S = Sodi - S
ogr = 0.568 - 1.372 = -0.804 (cal/mole K)
!V = !Vodi - !Vo
gr = 3.4166 - 5.2982 = -1.881 (cm3/mole)
-1.881 / 41.8 = -0.0450 (cal/mole)
41.8 bar cm3 = 1 calorie
Graphite becomes diamond, !G = 0
!G = 0 = !Ho -T!So + P!Vo
!G = 0 = 453 (cal/mole) - -0.804 (cal/mole K) T - -
0.045 (cal/mole bar) P
P = (!Ho -T!So) / -!Vo
P = (453 (cal/mole) + -0.804 (cal/mole K) T ) / 0.045
(cal/mole bar)
T = 298.15 K {note: this is 25oC}
P = (453 - -0.804(298))/ 0.045 = 15,389 bars
dP/dT = !S/ !V
-0.804 cal/mole K
-1.881 cm3/mole X 41.8 bar cm3/cal
= 17.9 bar/K
{Line: y = mx + b} P = 17.9 T + b
15,389 bars - 17.9 (298.15 K) = b
b = 1.006 kb
Which phase is stable at 1 bar and 25 oC?
G = !Hfo -TSo + PVo
Ggr = 0 - 298.15 K x (1.372 (cal/mole K) ) + 1 bar
(5.2982 / 41.8) (cal/mole bar)
= -408.9 (cal/mole)
Gdi = 453 (cal/mole) - 298.15 K x (0.568
(cal/mole) ) + 1 bar (3.4166 / 41.8) (cal/mole
bar)
= 283.7 (cal/mole)
Which phase is stable at 20 kbar and 25 oC?
G = !Hfo -TSo + PVo
Ggr = 0 - 298.15 K x (1.372 (cal/mole K) ) + 20000
bar (5.2982 / 41.8) (cal/mole bar)
= 2126.0 (cal/mole)
Gdi = 453 (cal/mole) - 298.15 K x (0.568 (cal/mole) )
+ 20000 bar (3.4166 / 41.8) (cal/mole bar)
= 1918.4 (cal/mole)
Phase Diagram
Recall that as you go
into the Earth, both
P and T increase
These two variables
control phase
stability of
compositions in the
earth.
On the left is a map
for phases of carbon
Why the discrepancy between
the three curves?
Phase stability
G = !Hfo - TSo + PVo
!G = !Ho - T!So + P!Vo
dP/dT = !S/ !V