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Consequences of the First Law Chapter 5 Advanced Thermodynamics (M2794.007900) Min Soo Kim Seoul National University

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Page 1: Consequences of the First Law - Seoul National University

Consequences of the First Law

Chapter 5

Advanced Thermodynamics (M2794.007900)

Min Soo Kim

Seoul National University

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A.1 Partial Derivatives

Consider a function of three variables, 𝑓 π‘₯, 𝑦, 𝑧 = 0

since only two variables are independent, we can write

π‘₯ = π‘₯ 𝑦, 𝑧 , 𝑦 = 𝑦 π‘₯, 𝑧

Then dπ‘₯ = (πœ•π‘₯

πœ•π‘¦)𝑧𝑑𝑦 + (

πœ•π‘₯

πœ•π‘§)𝑦𝑑𝑧, and

d𝑦 = (πœ•π‘¦

πœ•π‘₯)𝑧𝑑π‘₯ + (

πœ•π‘¦

πœ•π‘§)π‘₯𝑑𝑧

We obtain,

dπ‘₯ = (πœ•π‘₯

πœ•π‘¦)𝑧 (

πœ•π‘¦

πœ•π‘₯)𝑧𝑑π‘₯ + (

πœ•π‘¦

πœ•π‘§)π‘₯𝑑𝑧 + (

πœ•π‘₯

πœ•π‘§)𝑦𝑑𝑧

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A.1 Partial Derivatives

dπ‘₯ = (πœ•π‘₯

πœ•π‘¦)𝑧 (

πœ•π‘¦

πœ•π‘₯)𝑧𝑑π‘₯ + (

πœ•π‘¦

πœ•π‘§)π‘₯𝑑𝑧 + (

πœ•π‘₯

πœ•π‘§)𝑦𝑑𝑧

= (πœ•π‘₯

πœ•π‘¦)𝑧(

πœ•π‘¦

πœ•π‘₯)𝑧𝑑π‘₯ + (

πœ•π‘₯

πœ•π‘¦)𝑧(

πœ•π‘¦

πœ•π‘§)π‘₯ + (

πœ•π‘₯

πœ•π‘§)𝑦 𝑑𝑧

If d𝑧 = 0 and dπ‘₯ β‰  0 ,

𝝏𝒙

ππ’š 𝒛=

πŸππ’š

𝝏𝒙 𝒛

. This expression is known as the reciprocal relation.

If dπ‘₯ = 0 and d𝑧 β‰  0 ,

πœ•π‘₯

πœ•π‘¦ 𝑧

πœ•π‘¦

πœ•π‘§ π‘₯= βˆ’

πœ•π‘₯

πœ•π‘§ 𝑦

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A.1 Partial Derivatives

πœ•π‘₯

πœ•π‘¦ 𝑧

πœ•π‘¦

πœ•π‘§ π‘₯= βˆ’

πœ•π‘₯

πœ•π‘§ 𝑦(previous slide)

πœ•π‘₯

πœ•π‘§ 𝑦=

1πœ•π‘§

πœ•π‘₯ 𝑦

(using reciprocal relation)

Substituting these equations yield,

𝝏𝒙

ππ’š 𝒛

ππ’š

𝝏𝒛 𝒙

𝝏𝒛

𝝏𝒙 π’š= βˆ’πŸ. The cyclical rule, or cyclical relation.

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A.1 Partial Derivatives

Consider a function 𝑒 of three variables x, y, z can be written as a function of only

two variables and those two variables are independent.

𝑒 = 𝑒 π‘₯, 𝑦

Alternatively,

π‘₯ = π‘₯ 𝑒, 𝑦

Then

dπ‘₯ =πœ•π‘₯

πœ•π‘’ 𝑦𝑑𝑒 +

πœ•π‘₯

πœ•π‘¦ 𝑒𝑑𝑦.

If we divide the equation by d𝑧 while holding 𝑒 constant,

πœ•π‘₯

πœ•π‘§ 𝑒=

πœ•π‘₯

πœ•π‘¦ 𝑒

πœ•π‘¦

πœ•π‘§ 𝑒. The chain rule of differentiation.

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5.1 The Gay-Lussac-Joule Experiment

In general, 𝑒 = 𝑒 𝑇, 𝑣

using the cyclical and reciprocal relations,

(πœ•π‘‡

πœ•π‘£)𝑒 = βˆ’

(πœ•π‘’

πœ•π‘£)𝑇

(πœ•π‘’

πœ•π‘‡)𝑣

for a reversible process, 𝑐𝑣 = (πœ•π‘’

πœ•π‘‡)𝑣

∴ (πœ•π‘’

πœ•π‘£)𝑇 = βˆ’π‘π‘£ (

πœ•π‘‡

πœ•π‘£)𝑒

Then how can we keep 𝑒 constant during the expansion?

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5.1 The Gay-Lussac-Joule Experiment

𝑑𝑒 = π›Ώπ‘ž βˆ’ 𝛿𝑀 β‡’ free expansion

𝑇1 = 𝑇0 + 𝑣0𝑣1(

πœ•π‘‡

πœ•π‘£)𝑒 𝑑𝑣, πœ‚ ≑ (

πœ•π‘‡

πœ•π‘£)𝑒 : Joule’s coefficient

From Joule’s experimental result,

πœ‚ =πœ•π‘‡

πœ•π‘£ 𝑒< 0.001 K kilomole mβˆ’3

π’—πŸŽ , π‘»πŸŽ π’—πŸ βˆ’ π’—πŸŽ

thermal insulation

gas

samplediaphragm

vacuum

= 0

(adiabatic)

= 0

(no work)

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5.1 The Gay-Lussac-Joule Experiment

for a Van der Waals gas, (Problem 5-3)

πœ‚ = βˆ’π‘Ž

𝑣2𝑐𝑣

for an ideal gas,

by using the equation 𝑑𝑒 = 𝑇𝑑𝑠 βˆ’ 𝑃𝑑𝑣,

πœ•π‘’

πœ•π‘£ 𝑇= 𝑇

πœ•π‘ 

πœ•π‘£ π‘‡βˆ’ 𝑃 = 𝑇

πœ•π‘ƒ

πœ•π‘‡ π‘£βˆ’ 𝑃 = 𝑇 [

πœ•

πœ•π‘‡

𝑅𝑇

𝑣]𝑣 βˆ’ 𝑃

=𝑅𝑇

π‘£βˆ’ 𝑃 = 0

Then 𝑒 = 𝑒(𝑇)

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5.1 The Gay-Lussac-Joule Experiment

for a real gas,

by using the equation π‘‘π‘ž =πœ•π‘’

πœ•π‘‡ 𝑣𝑑𝑇 +

πœ•π‘’

πœ•π‘£ 𝑇+ 𝑃 𝑑𝑣 divide by the

temperature T,

π‘‘π‘ž

𝑇=

1

𝑇

πœ•π‘’

πœ•π‘‡ 𝑣𝑑𝑇 +

1

𝑇

πœ•π‘’

πœ•π‘£ 𝑇+ 𝑃 𝑑𝑣

πœ•

πœ•π‘£

1

𝑇

πœ•π‘’

πœ•π‘‡=

πœ•

πœ•π‘‡

1

𝑇

πœ•π‘’

πœ•π‘£+ 𝑃

1

𝑇

πœ•2𝑒

πœ•π‘£πœ•π‘‡= βˆ’

1

𝑇2πœ•π‘’

πœ•π‘£+ 𝑃 +

1

𝑇

πœ•2𝑒

πœ•π‘£πœ•π‘‡+

1

𝑇

πœ•π‘ƒ

πœ•π‘‡

πœ•π‘’

πœ•π‘£ 𝑇= 𝑇

πœ•π‘ƒ

πœ•π‘‡ π‘£βˆ’ 𝑃

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5.2 The Joule-Thomson Experiment

Since the process takes place in an insulated cylinder,

Ξ΄π‘ž = 0

specific work done in forcing the gas through the plug, 𝑀1 = 𝑣10𝑃1 𝑑𝑣 = βˆ’π‘ƒ1𝑣1

specific work done by the gas in the expansion, 𝑀2 = 0𝑣2 𝑃2 𝑑𝑣 = 𝑃2 𝑣2

Porous plug

Initial state Final state

π‘·πŸ, π’—πŸ , π‘»πŸπ‘·πŸ, π’—πŸ , π‘»πŸ

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5.2 The Joule-Thomson experiment

The total work, 𝑀 = 𝑀1 + 𝑀2 = 𝑃2 𝑣2 βˆ’ 𝑃1 𝑣1 = 𝑒1 βˆ’ 𝑒2

𝑒1 + 𝑃1 𝑣1 = 𝑒2 + 𝑃2 𝑣2 ⟺ β„Ž1 = β„Ž2

Thus, a throttling process occurs at constant enthalpy.

constant

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5.2 The Joule-Thomson experiment

Joule-Thomson coefficient

πœ‡π½π‘‡ ≑ (πœ•π‘‡

πœ•π‘ƒ)β„Ž

the point where πœ‡π½π‘‡ = 0 is called inversion point.

from β„Ž = β„Ž 𝑇, 𝑃 ,

π‘‘β„Ž = (πœ•β„Ž

πœ•π‘‡)𝑃 𝑑𝑇 + (

πœ•β„Ž

πœ•π‘ƒ)𝑇 𝑑𝑃

πœ‡π½π‘‡ ≑ (πœ•π‘‡

πœ•π‘ƒ)β„Ž =

𝑇2βˆ’π‘‡1

𝑃2βˆ’π‘ƒ1 β„Ž

𝑇2 = 𝑇1 βˆ’ πœ‡ 𝑃2 βˆ’ 𝑃1

The gas is cooling when the πœ‡ is positive

and heating when the πœ‡ is negative

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5.2 The Joule-Thomson experiment

Joule-Thomson coefficient

πœ‡π½π‘‡ =πœ•π‘‡

πœ•π‘ƒ β„Ž= βˆ’

πœ•π‘‡

πœ•β„Ž 𝑃

πœ•β„Ž

πœ•π‘ƒ 𝑇=

1

𝐢𝑃𝑇

πœ•π‘£

πœ•π‘‡ π‘ƒβˆ’ 𝑣

for an ideal gas, πœ‡π½π‘‡ = 0,

πœ•β„Ž

πœ•π‘ƒ 𝑇= 0 and β„Ž = β„Ž 𝑇

for a Van der Waals gas, 𝑃 =𝑅𝑇

π‘£βˆ’π‘βˆ’

π‘Ž

𝑣2

πœ‡π½π‘‡ =1

𝑐𝑃

2π‘Žπ‘…π‘‡

1 βˆ’π‘π‘£

2

βˆ’ 𝑏

1 βˆ’2π‘Žπ‘£π‘…π‘‡

1 βˆ’π‘π‘£

2

If πœ‡π½π‘‡ = 0, 𝑇𝑖 =2π‘Ž

𝑏𝑅1 βˆ’

𝑏

𝑣

2

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5.3 Heat engines and the Carnot cycle

Carnot cycle

In (a), work is done on the system and is converted to heat.

In (b), heat is extracted from a reservoir and is converted to mechanical work.

This configuration is not possible.

𝑇

𝑸

𝑾 𝑴

𝑇

𝑸

𝑾𝑴

(a) (b)

Fig. The concept of a heat engine.

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5.3 Heat engines and the Carnot cycle

Carnot cycle

Can the work done by the system be equal to the heat in?

The second law of thermodynamics states unequivocally that it is impossible to

construct a perfect heat engine.

Thus case (b) must be modified as case (c)

𝑇

𝑸

𝑾𝑴

(b) (c)

Fig. The concept of a heat engine.

𝑇𝑏

π‘‡π‘Ž

𝑸𝑯

𝑸𝑳

𝑾𝑴

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5.3 Heat engines and the Carnot cycle

Clausius statement

It is impossible to construct a device that operates in a cycle and whose sole

effect is to transfer heat from a cooler body to a hotter body.

Kelvin-Planck statement

It is impossible to construct a device that operates in a cycle and produces no

other effect than the performance of work and the exchange of heat with a

single reservoir.

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5.3 Heat engines and the Carnot cycle

Carnot cycle

1 – 2 : isothermal expansion

2 – 3 : adiabatic expansion

3 – 4 : isothermal compression

4 – 1 : adiabatic compression

𝑇𝑏

π‘‡π‘Ž

𝑸𝑯

𝑸𝑳

𝑾

Fig. P-V and T-S diagrams of Carnot cycle.

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5.3 Heat engines and the Carnot cycle

The efficiency of the engine,

πœ‚ =π‘Š

𝑄𝐻=

π‘Š

𝑄𝐻=output

input

Applying the first law to the system,

βˆ†π‘ˆ = 𝑄𝐻 + 𝑄𝐿 βˆ’π‘Š = 𝑄𝐻 βˆ’ 𝑄𝐿 βˆ’ π‘Š

Since the system is in a cyclical process, βˆ†π‘ˆ = 0. Then,

π‘Š = 𝑄𝐻 + 𝑄𝐿 or π‘Š = 𝑄𝐻 βˆ’ 𝑄𝐿

Substituting the equations,

πœ‚ =𝑄𝐿+𝑄𝐻

𝑄𝐻= 1 +

𝑄𝐿

𝑄𝐻= 1 βˆ’

𝑄𝐿

𝑄𝐻

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5.3 Heat engines and the Carnot cycle

for an ideal gas, 𝑃𝑣 = 𝑅𝑇 , 𝑒 = 𝑒 𝑇 ,

for isothermal process, 𝑄𝐻 = π‘Š12 = 𝑛 ഀ𝑅 𝑇𝑏 ln𝑉2

𝑉1

𝑄𝐿 = π‘Š34 = 𝑛 ഀ𝑅 π‘‡π‘Ž ln𝑉4

𝑉3

⇒𝑄𝐻

𝑄𝐿= βˆ’

𝑇𝑏

π‘‡π‘Ž

for adiabatic process, 𝑃𝑉𝛾 = π‘π‘œπ‘›π‘ π‘‘π‘Žπ‘›π‘‘ ,

𝑇𝑏 𝑉2π›Ύβˆ’1 = π‘‡π‘Ž 𝑉3

π›Ύβˆ’1

𝑇𝑏 𝑉1π›Ύβˆ’1 = π‘‡π‘Ž 𝑉4

π›Ύβˆ’1

⇒𝑉2

𝑉1=

𝑉3

𝑉4

The efficiency of the Carnot cycle, πœ‚ = 1 +𝑄𝐿

𝑄𝐻= 1 βˆ’

π‘‡π‘Ž

𝑇𝑏

𝑠2 βˆ’ 𝑠1 = 𝑐𝑣ln𝑇2𝑇1

+ 𝑅ln𝑣2𝑣1

= 𝑐𝑝ln𝑇2𝑇1

βˆ’ 𝑅ln𝑃2𝑃1

= 0

𝑐𝑣 =1

πœ… βˆ’ 1𝑅, 𝑐𝑝 =

πœ…

πœ… βˆ’ 1𝑅

𝑃2𝑃1

=𝑣2𝑣1

πœ…

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5.3 Heat engines and the Carnot cycle

Carnot engine has the maximum efficiency for any engine that one might design.

1. Carnot engine operates between two reservoirs and that it is reversible.

2. If a working substance other than an ideal gas is used, the shape of curves in

the P-V diagram will be difference.

3. The efficiency would be 100 percent if we were able to obtain a low temperature

reservoir at absolute zero. β†’However this is forbidden by the third law.

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5.3 Heat engines and the Carnot cycle

Carnot refrigerator

Reverse process of Carnot engine

Coefficient of performance(COP)

COP ≑ βˆ’π‘„πΏπ‘Š

=π‘„πΏπ‘Š

=𝑄𝐿

𝑄2 βˆ’ 𝑄𝐿=

𝑇1𝑇2 βˆ’ 𝑇1

We introduce a minus sign in order to make the COP a positive quantity :

The heat 𝑄𝐿 is extracted from the low temperature reservoir and W is the work done

on the system. 𝑄𝐿 is positive (heat flow into the system) and W is negative (work

done on the system)

𝑇𝑏

π‘‡π‘Ž

𝑸𝑯

𝑸𝑳

𝑾

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5.3 Heat engines and the Carnot cycle

Typical refrigerator

1. The refrigerant is a substance chosen to be a saturated liquid at the pressure and

temperature of condenser.

2. The liquid undergoes a throttling process in which it is cooled and is partially

vaporized.

Condenser

Evaporator

𝑸𝑯

𝑸𝑳

𝑾

Com

pre

ssor

Expansion

valve

low

pressure

liquid/

vapor

low

pressure

vapor

high

pressure

vapor

high

pressure

liquid

(heat out to surrounding)

(heat in from refrigerator space)

refrigerant

(e.g. freon)

long capillary tube

Fig. Schematic diagram of a typical refrigerator

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5.3 Heat engines and the Carnot cycle

Condenser

Evaporator

𝑸𝑯

𝑸𝑳

𝑾

Com

pre

ssor

Expansion

valve

low

pressure

liquid/

vapor

low

pressure

vapor

high

pressure

vapor

high

pressure

liquid

(heat out to surrounding)

(heat in from refrigerator space)

refrigerant

(e.g. freon)

long capillary tube

Fig. Schematic diagram of a typical refrigerator

Typical refrigerator

3. The vaporization is completed in the evaporator: the heat is absorbed by the

refrigerant from the low temperature reservoir (the interior refrigerator space).

4. The low pressure vapor is then adiabatically compressed and isobarically cooled

until it becomes a liquid once again.

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5.3 Heat engines and the Carnot cycle

Typical refrigerator

Refrigerator are designed to extract as much heat as possible from a cold reservoir

with small expenditure of work.

The coefficient of performance of a household refrigerator is in the range of 5 to 10.