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THERMODYNAMICS dynamics – changes thermo heat Laws of Thermodynamics: 0 th , 1 st , 2 nd , 3 rd

THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

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Page 1: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

THERMODYNAMICS

dynamics – changesthermo – heat

Laws of Thermodynamics:0th, 1st, 2nd, 3rd 

Page 2: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Note: Thermodynamics ……..

     is not concerned about rate of changes (kinetics) but the states before and after the change

     does not deal with time

Page 3: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Classical Thermodynamics

Marcoscopic observables T, P, V, …

Statistical Thermodynamics

Microscopic details dipole moment, molecular size, shape

Page 4: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Joule’s experiment

 

  

T mgh adiabatic wall

(adiabatic process)

U (energy change) = W (work) = mgh

w

h

Thermometer

Page 5: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

w

T time interval of heatingU = q (heat)

Conclusion: work and heat has the same effect to system (internal energy change)

FIRST LAW: U = q + W*

Page 59

Page 6: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

U: internal energy is a state function [ = Kinetic Energy (K.E.) + Potential Energy (P.E.) ] q: energy transfer by temp gradient W: force distance E-potential charge surface tension distance pressure volume

First Law: The internal energy of an isolated system is constant

Page 7: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Positive: heat flows into system work done onto systemNegative: heat flows out of system work done by system

Convention:

Pressure-volume Work

P1 = P2

V2V1

MM

d work F dlext M gdhpiston

weight

AAdh

P Adhext

P dVext work P V Vext 2 1

Mg h

Page 8: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

If weight unknown, but only properties of systemare measured, how can we evaluate work?

PV1V2P

MM

Assume the process is slow and steady,

Pint = Pext

Page 9: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Free Expansion:

Free expansion occurs when the external pressure is zero, i.e. there is no opposing force

Page 10: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Reversible change: a change that can be reversed by an infinitesimal modification of a variable. Quasi equilibrium process: Pint = Pext + dP (takes a long time to complete)

infinitesimal at any time

quasi equilibrium process

ò dVPW extò dVPint

Page 11: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

1 2P

V

Example: P1 = 200kPa = P2

V1 = 0.04m3 V2 = 0.1m3

W PdV1 21

2

P V V2 1

200 01 0 04 3kPa m. . 12kJ

what we have consider was isobaric expansion(constant pressure) other types of reversible expansion of a gas: isothermal, adiabatic

*

Page 64-66

Page 12: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Isothermal expansion

remove sand slowlyat the same time maintain temperature by heating slowly

W PdVrev 1

2

nRT

VdV

1

2

nRTdV

V1

2

nRT

V

Vln 2

1

T

VV1 V2

P

area under curve

*

Page 65-66

Page 13: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Ex. V1 = 0.04m3 P1 = 200kPa V2 = 0.1m3

W nRTV

Vrev 1

2

1

ln

PV

V

V1 12

1

ln

200 0 04

01

0 043kPa m. ln

.

.kJ 7.33

PPV

VkPa2

1 1

2

80

Page 14: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Adiabatic Reversible Expansion

For this processPV = constant for ideal gas(proved later)

V1

P1 T1

V2

P2 T2

(slightly larger than 1)

C

Cp

v

W PdVPV dV

V 1 1

1

2

1

2

PV V V1 1 21

11

1

PV PV2 2 1 1

1

Page 15: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Ex. V1 = 0.04m3, P1 = 200kPa, V2 = 0.1m3,

= 1.3

P kPa2

1 3

2000 04

01060 77

.

..

.

W kJ

60 77 01 200 0 04

1 136 41

. . .

..

volume change

|Wa|>|Wb|>|Wc|>|Wd|

W PdV 0

a

db

V

P

200kPaconst

isothermal

adibatic

Page 16: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

State Function Vs Path Function State function: depends only on position in

the x,y plane e.g.: height (elevation)

300200

100mB

AX

Y

1 2

Page 17: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Path Function: depends on which path is taken to reach destination

from 1 2, difference of 300m (state function)but path A will require more effort.Internal energy is a state function, heat and work are path functions

3

2481.13K

192.45K

P

200kPa

V/m30.04 0.1

1

Page 18: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

5 moles of monoatomic gas

C R

U nC T R kJ

W kJ

Q U kJ kJ

W kJ kJ

Q kJ kJ kJ

V

V

3

23

2 289 5 18

12

12 30

7 33 0 7 33

7 33 18 25 33

1 2

1 2

1 3 2

1 3 2

. .

. .

Page 19: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Joule’s second experiment

Energy UU(V,T) ???

V1V2

thermometer

At time zero, open valve

adiabatic wall

Page 20: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

After time zero, V1 V1+V2

T=0 Q=0 W=0 no Pext U=0

thermometer

No temperature change

adiabatic wall

Page 21: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

dTCdVV

UdT

T

UdU

V

U

VTV

T

0

0 (for ideal gas)CV is constant volume heat capacity

U=U(T) Energy is only a function of temperature for ideal gas*

Page 22: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

*Enthalpy

Define H = U + PV   state function intensive variables locating the state

Enthalpy is also a state function

H = U + PV + VP

Page 23: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

PPTP

CCdPP

HdT

T

HdH

PTHH

0

,

for ideal gases C C R

C

C

P V

P

V

At constant pressureH = U+PV = U - W = QH = QP constant pressure heating

H is expressed as a functional of T and P

Page 24: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Thermochemistry Heat transferred at constant volume qV = U

Heat transferred at constant pessure qP = H

Exothermic H = -

Endothermic H = +

Page 25: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Standard states, standard conditions do not measure energies and enthalpies absolutely but only the differences, U or H

The choice of standard state is purely a matter of convenience

Page 26: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

The standard states of a substance at a specified temperature is its pure form at 1 atmosphere

What is the standard state ?

Page 27: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

25oC, 1 atmosphere: the most stable forms of elements assign “zero enthalpy”

Ho298 = 0 used for chemical reactions

Page 28: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Standard enthalpy of formation

Standard enthalpy change for the formationof the compound from its elements in their reference states.

Reference state of an element is its most stablestate at the specified temperature & 1 atmosphere

C (s) + 2H2 (g) CH4 (g) Hfo = -75 kJ

289K, 1 atm

From the definition, Hfo for elements 0

Page 29: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Hess’s Law

The standard enthalpy of an overall reaction is the sum of thestandard enthalpies of the individual reactions into which areaction may be divided.

Standard reaction enthalpy is the change in enthalpy when the reactants in their standard states change to products in their standard states.

Page 30: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Hess’ Law

R X Y PH H H 2 3 4

H1

H1 = H2 + H3 + H4 state function

Hess’s law is a simple application of the first law of thermodynamics

Page 31: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

e.g. C (s) + 2H2 (g) CH4 (g) H1o = ?

298K, 1 atm

C (s,graphite) + O2 (g) CO2 (g)

Ho = -393.7 kJ H2 (g) + ½O2(g) H2O (l)

Ho = -285.8 kJ CH4 (g) + 2O2 (g) CO2 (g) + 2H2O (l)

Ho = -890.4 kJ H1

o = -393.7 + 2(-285.8) - (-890.4)

= -75 kJ/mole

Page 32: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Heat of Reaction (Enthalpy of Reaction) Enthalpy change in a reaction, which may be obtained from Hf

o of products and reactants

Reactants Products

products tsreaac

oreactionfR

oprodfp

or HnHnH

tan,,

i foi

productsreac ts

Htan

I stoichiometric coefficient, + products,

- reactantsE.g. CH4 (g) + Cl2 (g) CH3Cl (g) + HCl (g)

Page 33: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Hfo/ kJ

CH3Cl -83.7

HCl -92.0

Cl2 0

CH4 -75.3

Hro = (-83.7-92.0) - (-75.3+0) = -100.4 kJ

Reactants Products

elements elements

n HR f Ro , n Hp f p

o ,

Page 34: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

jfo

jor HH ,

2A + B 3C + D

0 = 3C + D - 2A - B

Generally,0 = J J J

J denotes substances, J are the stoichiometric numbers

*

Page 83

Page 35: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Bond energy (enthalpy)

Assumption – the strength of the bond is independent of the molecular environment in which the atom pair may occur.

C (s,graphite) + 2H2 (g) CH4(g)Ho = -75.4 kJ

H2 (g) 2H (g) Ho = 435.3 kJ

C (s,graphite) C (g) Ho= 715.8 kJ C (s,graphite) + 2H2 (g) C (g) + 4H (g)

Ho = 2(435.3)+715.8 = 1586.5 kJ C (g) + 4H (g) CH4 (g) H = -75.4-1586.5

= -1661.9 kJCH Bond enthalpy = 1661.9/4 kJ = 415.5 kJ

Page 36: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Temperature dependence of Hr

productsreactantsreactants

reaction,products

products, ipiRippipP

T

T

por

Tr

CnCnCC

dTCHHo

CP,R

CP,P

Hro

P

R

HrT

298 T

Page 37: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

What is the enthalpy change for vaporization (enthalpy of vaporization) of water at 0oC?

H2O (l) H2O (g)

Ho = -241.93 - (-286.1) = 44.01 kJmol-1 H2 = Ho + CP(T2-T1) assume CP,i

constant wrt T

H (273) = Ho(298) + CP(H2O,g) - CP (H2O,l)(273-298) = 44.10 - (33.59-75.33)(-25) = 43.0 kJ/mole

Page 38: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Reversible vs IrreversibleNon-spontaneous changes vs Spontaneous

changesReversibility vs Spontaneity

First law does not predict direction of changes,cannot tell which process is spontaneous. Only U = Q + W

Page 39: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Second Law of Thermodynamics

•Origin of the driving force of physical and chemical change

•The driving force: Entropy

•Application of Entropy: • Heat Engines & Refrigerators• Spontaneous Chemical Reactions

•Free Energy

Page 40: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Second Law of Thermodynamics

No process is possible in which the sole result is the absorptionof heat from a reservoir and its complete conversion into work

Hot Reservoir

q

w

Engine

Page 41: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Direction of Spontaneous Change

More Chaotic !!!

Page 42: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Entropy (S) is a measurement of the randomness of the system, and is a state function!

S Q S 1 / T

Spontaneous change is usually accompanied by a dispersal of energy into a disorder form, and its consequence is equivalent to heating

Page 43: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

T

dqdS rev

Entropy S

For a reversible process, the change of entropy is defined as

Another expression of the Second Law:

The entropy of an isolated systems increases in the course of aspontaneous change:

Stot > 0

where Stot is the total entropy of the isolated system

(thermodynamic definition of the entropy)

*

Page 122

Page 44: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Entropy S

The entropy of an isolated systems increases in the course of areversible change:

Stot = 0

where Stot is the total entropy of the isolated system

Page 45: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Carnot’s Theoretical Heat Engine

Heat flows from a high temperature reservoirto a low temperature body. The heat can be utilized to generate work.

e.g. steam engine.

Page 46: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

The efficiencies of heat engines

Hot Reservoir

q

w

Engine

S = - |q|/Th < 0 not possible! contrary to the second law

Page 47: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

The Nernst Theorem

The entropy change accompanying any physical or chemical transformation approaches zero as the temperature approaches zero.

S 0 as T0

Page 48: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Third Law of Thermodynamics

If the entropy of each element in its most state is taken as zero at the absolute zero of temperature, every substance has a positive entropy. But at 0K, the entropy of substance may equals to 0, and does become zero in perfect crystalline solids.

Crystalline form: complete ordered, minimum entropy

Implication: all perfect materials have the same entropy (S=0) at absolute zero temperature

Page 49: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Statistical Interpretation of S

S = 0 at 0K for perfect crystals S = k ln

  Boltzmann number of arrangements postulate of entropy Boltzmann constant

Page 50: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Entropy Change of Mixing

one distinguish arrangement

S k S kA B ln!

!, ln

!

!

4

40

4

40

A B

A B

A B

A B

N N

N N

S k

!

! !

ln

8 7 6 5

4 3 2 170

70

number of arrangement increased

Page 51: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

In general mixing NA, NB

!!

!ln

BA

BAmix NN

NNkS

Entropy change of mixingStirling’s approximation: ln N! N ln N + 0(N)

for large N

0

BBAABA

BBAABABA

BBAABABAmix

XXXXNNk

NXNXNNNNk

NNNNNNNNkS

lnln

lnlnln

lnlnln

Page 52: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Extensions of 2nd Law 

TdS dq Clausius Inequality

For adiabatic process,

TdS or dS 0 0

Entropy will always attain maximum in adiabatic processes.

A similar function for other processes?

Page 53: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Define Helmholtz free energyA = U - TS Thermodynamic

State Function dA = dU - TdS - SdTSubstitute into Clausius Inequality

0

0

0

dq TdS

dq dA dU SdT

PdV dA SdTfor isothermal, isochoric (constant volume)process,

0dA

Page 54: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

change in Helmholtz free energy = maximum isothermal work

Example of isothermal, isochoric process: combustion in a bomb calorimeter

O2 +fuel

Temp. bath

O2, CO2,H2O

Higher P heat givenout

Page 55: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Gibbs Free Energy

Define Gibbs free energy G = H - TS Thermodynamic

state function = U + PV -TS dG = dU +PdV + VdP -TdS -SdT

Page 56: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

constant pressure, constant temperature

dG0

G will tend to a minimum value equilibrium spontaneous change

dG 0dG 0

More applications since most processes areisothermal, isobaric

chemical reactions at constant T, PReactants Productsendothermic H is positiveexothermic H is negative

Page 57: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Change of Gibbs free energy with temperature(constant pressure)

ST

G

SdTGG

VdPSdTdG

P

12

0

Page 58: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

dP

dT

H

T V

H

TV

P H

RT

dP

Pd P

H

RTdT

PH

RTconst

P

P

H T T

RT T

vap

vap

vap

vap

vap

vap

sat vap

sat

vap

2

2

2

1

2 1

1 2

ln

ln .

ln1/T

In P

Page 59: THERMODYNAMICS dynamics – changes thermo – heat Laws of Thermodynamics: 0 th, 1 st, 2 nd, 3 rd

Example: What is the change in the boiling point of water at 100oC per torr change in atmospheric pressure?

 Hvap = 9725 cal mol-1

Vliq = 0.019 l mol-1

Vvap = 30.199 l mol-1

dP

dT

H

T V V

calmol l atmcal

K lmol

atmK

torr K

dT

dPK torr

sat

sat

vap

v l

9725 0 04129

37315 30180

0 03566

2710

0 0369

1 1

1

1

1

1

.

. .

.

.

.