Wednesday, July 7, 2021

Chapter 13.1 - Kinetic Theory of An Ideal Gas

In the previous section, we saw the ideal gas equation PV = 𝝁RT. In this section, we try to explain the gas laws using kinetic theory

Some basics can be written in 4 steps:
1. A sample of a gas (that we consider for the discussions) will consist of the molecules of that gas only. There will not be any impurities like dust particles, water vapour etc.,
2. Molecules are very far apart. So there will not be any forces of attraction or repulsion between them
3. But molecules do collide with each other and with the walls of the container. All those collisions are elastic. There will not be any energy loss due to the collisions
4. What ever be the type of collisions, the total momentum will be conserved


• Based on the above points, let us now analyze the collisions of some gas molecules inside a closed container. Through such an analysis, we can derive an expression for pressure. It can be written in 18 steps:
1. The yellow rectangle in fig.13.1(a) below is a closed cubical container
• It contains N molecules of a gas

Derivation of the pressure exerted by a gas from Kinetic theory
Fig.13.1
2. One molecule is shown as a green sphere
• It travels towards the left along the red dotted line
   ♦ This red dotted line is parallel to the x-axis
3. The molecule hits the left side wall of the container
• This wall is parallel to the y-axis
   ♦ Remember that, the red dotted line is parallel to the x-axis
   ♦ So the molecule will be hitting the wall in a perpendicular direction
4. Let us see how the molecule bounces back:
• Due to the perpendicular collision, the molecule will bounce back along the same red line
• Also, since the collision is elastic, the molecule will bounce back with the same speed (magnitude of velocity)
◼  So we can write about the velocities:
If vx(1) is the initial velocity before collision, the velocity after collision will be -vx(1)
5. Let m be the mass of the molecule. Then the momentum can be calculated as:
   ♦ Initial momentum = mvx(1)
   ♦ Final momentum = -mvx(1)
6. Then change in momentum suffered by the molecule
= (final momentum – initial momentum)
= (-mvx(1) - mvx(1)) = -2mvx(1)
7. We have seen the principle of conservation of momentum in an earlier chapter (Fig.5.16 of section 5.7)
◼  Based on that principle, the change in momentum suffered by the wall will be 2mvx(1)
8. The wall suffers this change in momentum because, the molecule exerts a force on that wall
◼  We know that, force is equal to ‘rate of change of momentum’
   ♦ To find the ‘rate of change of momentum’,
   ♦ we need to divide ‘change of momentum’ by time
• So our next task is to find the time during which this ‘change in momentum’ occurs
9. The change in momentum occurs during the collision. But the duration of a collision is very small. Let it be Δt
• The molecule must hit the wall and bounce back in the interval Δt
• This is possible only if the molecule is within a distance of vx(1) × Δt from the wall
(Recall that, velocity multiplied by time gives distance)
• This distance is marked by the magenta vertical line in fig.b
(In the fig.b, the distance vx(1) × Δt is exaggerated. The magenta vertical line is in fact, very close to the left side wall. It is shown further away, only for clarity)
10. It is clear that, all the molecules (with velocity vx(1)) between the magenta line and the left wall, have a chance of hitting the wall within the duration Δt
• So we need the actual number of molecules (with velocity vx(1)) between the magenta line and the left wall
• For that actual number, we need the volume between the magenta line and the left wall
   ♦ If A is the area of the left wall, that volume will be A × vx(1) × Δt
• If nx(1) is the number of molecules (with velocity vx(1)) in unit volume, then the number of molecules in that volume will be nx(1) × A × vx(1) × Δt
11. All those molecules calculated in (10) have the chance of hitting the left wall
• But we know that, molecules move in random directions. So on the average, only half of those molecules will be hitting the wall
• So we get:
Number of molecules hitting the wall = 12 × nx(1) × A × vx(1) × Δt
12. In (7), we saw that, the change in momentum suffered by the wall due to one molecule = 2mvx(1)
• So the change in momentum (Q) due to 12nx(1)AvxΔt molecules can be obtained as: (2mvx(1))×(12nx(1)AvxΔt)
13. Dividing this change in momentum by Δt, we get the force Fx(1) experienced by the wall due to the collisions
• That is., Fx(1) = (2mvx(1))×(12nx(1)Avx(1)) = nx(1)mAv2x(1)
    ♦ This force is due to the molecules traveling with velocity vx(1)
14. Dividing this force by the area of the wall, we get the pressure P experienced by the wall
• That is., Px(1) = nx(1)mv2x(1)
    ♦ This pressure is due to the molecules traveling with velocity vx(1)
15. But there are molecules (traveling in the x-direction), with other velocities also
• The various velocities in the x-direction can be denoted as:
vx(1), vx(2), vx(3), etc.,
• So we can assume that, all molecules traveling in the x-direction, have an average velocity of $\mathbf\small{\rm{\bar{v}_x }}$
• This $\mathbf\small{\rm{\bar{v}_x }}$ is the average of vx(1), vx(2), vx(3), etc.,
• Then the result in (14) becomes: $\mathbf\small{\rm{P_x=n_xm\bar{v_x^2}}}$
    ♦ Where
        ✰ Px is the pressure due to all molecules traveling in the x-direction
        ✰ nx is the number of molecules (traveling in the x-direction) per unit volume
        ✰ $\mathbf\small{\rm{\bar{v}_x }}$ is the average of vx(1), vx(2), vx(3), etc.,
16. We derived the above result by considering the molecules traveling in the x-direction
• We can apply the same steps to the molecules which travel in the y-direction
    ♦ We will get: $\mathbf\small{\rm{P_y=n_xm\bar{v_y^2}}}$
• We can apply the same steps to the molecules which travel in the z-direction
    ♦ We will get: $\mathbf\small{\rm{P_z=n_xm\bar{v_z^2}}}$
17. A gas sample will be isotropic. So we cannot say that, more molecules travel in any preferred direction
• All directions are equally likely. So we can write: $\mathbf\small{\rm{\bar{v}_x=\bar{v}_y=\bar{v}_z }}$
• Squaring this, we get: $\mathbf\small{\rm{\bar{v_x^2}=\bar{v_y^2}=\bar{v_z^2}}}$
◼  Thus we can write:
In the gas sample, there are three velocities and all three are equal. Their squares are also equal
18. Let us write the role of each velocity:
   ♦ We use $\mathbf\small{\rm{\bar{v_x^2}}}$ to find Px
   ♦ We use $\mathbf\small{\rm{\bar{v_y^2}}}$ to find Py
   ♦ We use $\mathbf\small{\rm{\bar{v_z^2}}}$ to find Pz
19. If we can find the average of $\mathbf\small{\rm{\bar{v_x^2},\bar{v_y^2} \,and \,\bar{v_z^2} }}$, we can use it to find the pressure in a single step
• So our next aim is to find that average. It can be done in 2 steps:
(i) Since they are equal, we can sum them up and divide by 3. No weightage need to be given for any of them
• So the average is: $\mathbf\small{{\frac{\bar{v_x^2}\;+\;\bar{v_y^2}\;+\;\bar{v_z^2}}{3}}}$
(ii) We will denote ($\mathbf\small{{\bar{v_x^2}\;+\;\bar{v_y^2}\;+\;\bar{v_z^2}}}$) as $\mathbf\small{{\bar{v^2}}}$
• So the average is: $\mathbf\small{{\frac{\bar{v^2}}{3}}}$
18. This average is applicable to all molecules. So we do not need to consider nx, ny and nz separately. We can use n. This n is the 'number density' of molecules having the average velocity
• So based on the results in (15) and (16), we can write:
The pressure due to all the molecules is given by:
Eq.13.5: $\mathbf\small{\rm{P=\frac{nm \bar{v^2}}{3}}}$

◼  Two remarks have to be written about the above derivation:
1. We chose a cube as the container. This made it easier to consider the three directions separately
• But in reality, we can choose any arbitrary shape. The reason can be written in 3 steps
(i) We considered the molecules hitting on the left wall of area A
• We need not insist on such perfect areas. A small area ΔA would be sufficient
(ii) This is because, when we find pressure, we divide force by area. Then the area in both numerator and denominator cancel each other
(iii) The time ΔT also gets canceled in this way. So the distance vx(1)Δt is also not important. The container can be of any shape
2. Collisions between molecules
• This can be written in 5 steps
(i) We have considered the collision of molecules with the walls of the container. But we have not considered the collision between molecules
(ii) When molecules collide with each other, their velocities will change
• We considered a molecule with velocity vx(1)
• There is no guarantee that, on it’s way towards the wall, it will not hit another molecule, thereby changing it’s velocity to another value
(iii) However, numerous collisions are taking place in the gas sample
• So velocity lost by one molecule will be gained by another molecule at some other place
(iv) Also, we are taking the average value
(v) So the collisions between molecules will not lead to much error


Kinetic Interpretation of Temperature

• Based on Eq.13.5, we can find the relation between kinetic energy of the molecules and the temperature of the gas. It can be written in 15 steps:
1. We have Eq.13.5: $\mathbf\small{\rm{P=\frac{nm \bar{v^2}}{3}}}$
• Multiplying both sides by V, we get: $\mathbf\small{\rm{PV=\frac{1}{3}nVm\bar{v^2}}}$
• Multiplying the right side by 22, we get: $\mathbf\small{\rm{PV=\frac{2}{3}\times\frac{1}{2}nVm\bar{v^2}}}$
2. Recall that, n is the 'number density' (number of molecules in unit volume)
• So nV is the total number of molecules (N) in the sample
• Thus we get: $\mathbf\small{\rm{PV=\frac{2}{3}\times\frac{1}{2}Nm\bar{v^2}}}$
3. $\mathbf\small{\rm{\frac{1}{2}m\bar{v^2}}}$ is the average kinetic energy possessed by a single molecule
• So $\mathbf\small{\rm{\frac{1}{2}Nm\bar{v^2}}}$ is the total energy possessed by all the molecules in the sample
4. The total kinetic energy possessed by all the molecules is the internal energy E of the gas sample
• That is., $\mathbf\small{\rm{E=\frac{1}{2}Nm\bar{v^2}}}$
• Thus the result in (2) becomes Eq.13.6: $\mathbf\small{\rm{PV=\frac{2}{3}E}}$
5. But we have the basic equation: PV = 𝝁RT
• Comparing the two, we get: $\mathbf\small{\rm{\mu RT=\frac{2}{3}E}}$
6. In the previous section, we saw that:  𝝁R = NKB
• So the result in (5) becomes: $\mathbf\small{\rm{NK_B T=\frac{2}{3}E}}$
⇒ $\mathbf\small{\rm{\frac{E}{N}=\frac{3}{2}K_B T}}$
7. $\mathbf\small{\rm{\frac{E}{N}}}$ is the kinetic energy of one molecule
• KB is a constant
◼  So we can write:
Kinetic energy of a molecule is proportional to the absolute temperature of the gas
• It is also clear that, the internal energy of a gas depends only on it's temperature
   ♦ Pressure or volume has no effect on the internal energy
8. Next, let us consider a mixture of non-reactive gases
• We will name the gases as A, B, C, . . .
   ♦ Let the average velocity of the molecules of gas A be $\mathbf\small{\rm{\bar{v}_A}}$
   ♦ Let the average velocity of the molecules of gas B be $\mathbf\small{\rm{\bar{v}_B}}$
   ♦ Let the average velocity of the molecules of gas C be $\mathbf\small{\rm{\bar{v}_C}}$ 
so on . . .
• We will write the number densities of molecules also:
   ♦ Let the number density of the molecules of gas A be nA
   ♦ Let the number density of the molecules of gas B be nB
   ♦ Let the number density of the molecules of gas C be nC
so on . . .
9. Then using Eq 13.5, we can write the individual contributions:
   ♦ Contribution of gas A towards the total pressure = $\mathbf\small{\rm{\frac{n_A m_A \bar{v_A^2}}{3}}}$
   ♦ Contribution of gas B towards the total pressure = $\mathbf\small{\rm{\frac{n_B m_B \bar{v_B^2}}{3}}}$
   ♦ Contribution of gas C towards the total pressure = $\mathbf\small{\rm{\frac{n_C m_C \bar{v_C^2}}{3}}}$
so on . . .
10. So the total pressure of the gas will be obtained as:
$\mathbf\small{\rm{p=\frac{n_A m_A \bar{v_A^2}}{3}+\frac{n_B m_B \bar{v_B^2}}{3}+\frac{n_C m_C \bar{v_C^2}}{3}+\, .\, .\, .}}$
11. Now consider the result in (6): $\mathbf\small{\rm{\frac{E}{N}=\frac{3}{2}K_B T}}$
• $\mathbf\small{\rm{\frac{E}{N}}}$ is the kinetic energy per molecule, which is equal to $\mathbf\small{\rm{\frac{1}{2}m \bar{v^2}}}$
• So we can write: $\mathbf\small{\rm{\frac{1}{2}m \bar{v^2}=\frac{3}{2}K_B T}}$
12. Applying this result to individual gases, we get:
   ♦ $\mathbf\small{\rm{\frac{1}{2}m_A \bar{v_A^2}=\frac{3}{2}K_B T}}$
   ♦ $\mathbf\small{\rm{\frac{1}{2}m_B \bar{v_B^2}=\frac{3}{2}K_B T}}$
   ♦ $\mathbf\small{\rm{\frac{1}{2}m_C \bar{v_C^2}=\frac{3}{2}K_B T}}$
so on . . .
• From this, we get:
   ♦ $\mathbf\small{\rm{m_A \bar{v_A^2}=3K_B T}}$
   ♦ $\mathbf\small{\rm{m_B \bar{v_B^2}=3K_B T}}$
   ♦ $\mathbf\small{\rm{m_C \bar{v_C^2}=3K_B T}}$
13. So the result in (10) becomes:
$\mathbf\small{\rm{p=\frac{n_A 3K_B T}{3}+\frac{n_B 3K_B T}{3}+\frac{n_C3K_B T}{3}+\, .\, .\, .}}$
⇒ $\mathbf\small{\rm{P=(n_A+n_B+n_C+\, .\, .\, .)K_BT}}$
⇒ $\mathbf\small{\rm{PV=(n_AV+n_BV+n_CV+\, .\, .\, .)K_BT}}$
⇒ $\mathbf\small{\rm{PV=(n_AVK_B+n_BVK_B+n_CVK_B+\, .\, .\, .)T}}$
⇒ $\mathbf\small{\rm{PV=(N_AK_B+N_BK_B+N_CK_B+\, .\, .\, .)T}}$
14. In the previous section, we saw that:  𝝁R = NKB
• Applying this to individual gases, we get:
   ♦ 𝝁AR = NAKB
   ♦ 𝝁BR = NBKB
   ♦ 𝝁CR = NCKB
so on . . .
15. So the result in (13) becomes:
$\mathbf\small{\rm{PV=(\mu_A R+\mu_B R+\mu_C R+\, .\, .\, .)T}}$
⇒ PV = (𝝁A + 𝝁B + 𝝁C + . . .)RT
◼  This is Dalton's law of partial pressures
• Thus we derived Dalton's law of partial pressures using kinetic theory


• We know that, when temperature increases, the speed of the molecules increases
• For a gas,
   ♦ The internal energy is due to the kinetic energy of the molecules
   ♦ When temperature increases, kinetic energy increases
   ♦ So when temperature increases, internal energy increases
• The kinetic energy depends on speed
• Let us try to calculate the average speed of a molecule in a gas sample. It can be written in 5 steps:
1. In the step (6) above, we obtained: $\mathbf\small{\rm{\frac{E}{N}=\frac{3}{2}K_B T}}$
• $\mathbf\small{\rm{\frac{E}{N}}}$ is the kinetic energy of one molecule
• So we can write: $\mathbf\small{\rm{\frac{1}{2}m\bar{v^2}=\frac{3}{2}K_B T}}$
⇒ $\mathbf\small{\rm{m\bar{v^2} =3K_BT}}$
⇒ $\mathbf\small{\rm{\bar{v}=\left( \frac{3K_BT}{m}\right)^{\frac{1}{2}}}}$
    ♦ Where m is the mass of one molecule 
2. Consider a sample of nitrogen gas
    ♦ One mole of nitrogen gas will have a mass of 28 grams
    ♦ One mole of nitrogen gas will have 6.023 × 1023 molecules
• So one molecule of nitrogen gas will have a mass of $\mathbf\small{\rm{\left( \frac{28 \times 10^{-3}}{6.023 \times 10^{23}}\right)}}$ = 4.65 × 10-26 kg
3. So we have the mass of one molecule
    ♦ Let the sample be at a temperature of 300 K
    ♦ We know the value of KB. It is: 1.38 × 10-23 J K-1
• Substituting these known values in (1), we get:
$\mathbf\small{\rm{\bar{v}=\left( \frac{3 \times 1.38 \times 10^{-23}(J\,K^{-1})\times 300\, (K)}{4.65 \times 10^{-26}(kg)}\right)^{\frac{1}{2}}=517\;(J\;kg^{-1})^{\frac{1}{2}}}}$
⇒ $\mathbf\small{\rm{\bar{v}=517\;(kg\;m\;s^{-2}\;m\;kg^{-1})^{\frac{1}{2}}=517 \; m\;s^{-1}}}$
◼ This speed is comparable to the speed of sound in air
4. We take the root of $\mathbf\small{\rm{\bar{v^2}}}$ to find $\mathbf\small{\rm{\bar{v}}}$
• So $\mathbf\small{\rm{\bar{v}}}$ is called root mean square velocity
    ♦ It's symbol is: vrms
• So the result in (1) can be modified as:
Eq.13.7: $\mathbf\small{\rm{v_{rms}=\left( \frac{3K_BT}{m}\right)^{\frac{1}{2}}}}$
5. Note that, in Eq.13.7, m is in the denominator
• So we can write:
In a mixture of gases, the lighter molecules will have greater vrms


Link to two solved examples based on the above discussion is given below:

Solved example 13.12 and 13.13


In the next section, we will see the Law of equipartition of energy



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Saturday, June 19, 2021

Chapter 13 - Kinetic Theory

In the previous chapter, we completed a discussion on Thermodynamics. In this chapter, we will see Kinetic theory

• Robert Boyle discovered that, if temperature of a gas is kept constant, it’s pressure will be inversely proportional to it’s volume
• This can be demonstrated as follows:
• Consider a gas inside a cylinder fitted with a movable piston
   ♦ If we move the piston downwards, the volume of the gas decreases
         ✰ At the same time, pressure of the gas increases
   ♦ If we move the piston upwards, the volume of the gas increases
         ✰ At the same time, pressure of the gas decreases
◼  This inverse relation is known as Boyle’s Law
• Robert Boyle made this discovery in the seventeenth century. Soon, other laws such as Charles Law, Avogadro's hypothesis etc., were discovered. All those laws were discovered in the seventeenth century. But precise mathematical explanations for those laws could be given only in the nineteenth century
• The mathematical explanations were based on the fact that, matter is made up of atoms and molecules. This fact about matter was not known to the scientists of the seventeenth century
• A sample of a gas is made up of a large number of atoms or molecules
   ♦ Noble gases like neon and argon exist as individual atoms
         ✰ For such gases, atoms and molecules implies the same
   ♦ Ordinary gases like oxygen and nitrogen exist as individual molecules
◼  Except when they are very close to each other, there is practically no interactions between the molecules in a gas sample
• This is because, compared to their sizes, the distances between those molecules are very large
• In this chapter, we will see how precise mathematical explanations can be given for the gas laws


Behavior of gases

• Some basics can be written in 7 steps:
1. Since the interactions between gas molecules are negligible, properties of gases are easier to understand. This is because: 
• In the case of solids and liquids, we will have to deal with equations related to mutual forces between molecules
• But for gases, such equations are absent
2. Consider a gas sample at normal pressure and normal temperature

The word ‘normal’ needs to be given importance. The reason can be written in 2 steps:
(i) If the pressure is very high, the volume will be so low that, the molecules come into close contacts with each other
   ♦ Then they will begin to interact with each other
   ♦ In such a situation, our equations will not be valid
(ii) If the temperature is very low, the gases will become liquids
   ♦ The molecules will then be in close contact with each other
   ♦ They will begin to interact with each other
   ♦ Then also, our equations will not be valid

◼  When the pressure and temperature are normal, any given gas sample will satisfy the following relation:
PV = KT
   ♦ Where:
         ✰ P is the pressure
         ✰ V is the volume
         ✰ T is the temperature
3. This relation can be explained in 2 steps:
(i) PV = KT can be rearranged as: $\mathbf\small{\rm{\frac{PV}{T}=K}}$
   ♦ When temperature is T1, let pressure be P1 and volume be V1
   ♦ When temperature is T2, let pressure be P2 and volume be V2
so on . . .
(ii) So the pressure, temperature and volume can vary
• But the combination will always be constant
• That is: $\mathbf\small{\rm{\frac{P_1V_1}{T_1}=\frac{P_2V_2}{T_2}=\frac{P_3V_3}{T_3}=K}}$
4. But this K is constant for the given sample only
• If we take another (larger or smaller in volume) sample of the same gas, it will be having another value of K
• Scientists discovered that, this K is equal to NkB
   ♦ Where:
         ✰ N is the number of molecules of in the sample
         ✰ kB is a constant called Boltzmann constant
         ✰ This kB is same for all gases
5. It is clear that, the variation of K from sample to sample, is due to the difference in N
• We can write: Eq.13.1: PV = (NkB)T
◼  Now we can consider different samples
• Let in the first sample, N be N1
In that sample,
   ♦ When temperature is T1, let pressure be P1 and volume be V1
• Let in the second sample, N be N2
In that sample,
   ♦ When temperature is T2, let pressure be P2 and volume be V2
• Let in the third sample, N be N3
In that sample,
   ♦ When temperature is T3, let pressure be P3 and volume be V3
so on . . .
◼  Then the relation in 3(ii) becomes:
$\mathbf\small{\rm{\frac{P_1V_1}{N_1T_1}=\frac{P_2V_2}{N_2T_2}=\frac{P_3V_3}{N_3T_3}=k_B}}$
6. Based on the above result in (5), we can give a satisfactory explanation for Avogadro's hypothesis. It can be written in steps:
(i) Take two gas samples
• For the first sample, let the P, V and T be P1, V1 and T1 respectively
   ♦ Then we can write: $\mathbf\small{\rm{\frac{P_1V_1}{T_1}=N_1k_B}}$
• For the second sample, let the P, V and T be P2, V2 and T2 respectively
   ♦ Then we can write: $\mathbf\small{\rm{\frac{P_2V_2}{T_2}=N_2k_B}}$
(ii) Suppose that, the two samples are experiencing the same pressure and temperature. Also suppose that, the two samples have the same volume
• Then we can write: P1 = P2, V1 = V2, T1 = T2
(iii) Then N1kB will become equal to N2kB
• It follows that, N1 = N2
• This is Avogadro's hypothesis
7. Avogadro in the seventeenth century said that:
If two samples have the same pressure, volume and temperature, they will be having the same number of particles
• The above steps from (1) to (6) give the mathematical proof


Let us see the practical applications of Avogadro’s hypothesis. It can be written in 7 steps:
1. Taking two samples:
   ♦ The first sample is of gas A
   ♦ The second sample is of another gas B
2. The two samples must contain the same number of molecules
• Here a problem arises. It can be explained in 2 steps:
(i) Labs at some part of the world may prepare the two samples in such a way that, there are 20000 molecules in each of them
(ii) Labs at some other part of the world may prepare the two samples in such a way that, there are 50000 molecules in each of them
◼  In order to avoid such differences, scientists decided to fix up a number
• They said:
Each of the two samples should have exactly one mole of molecules
   ♦ One mole is 6.023 × 1023 numbers
   ♦ It is just like: One dozen is 12 numbers
   ♦ So one mole of molecules is 6.023 × 1023 molecules
• So the problem is solved
3. Next, the two samples must be subjected to the same pressure
• Here also a problem arises. It can be explained in 2 steps
(i) Some labs may subject each of the two samples to a pressure of 3 bar
(ii) Some other labs may subject each of the two samples to a pressure of 500 torr
◼  In order to avoid such differences, scientists decided to fix up a pressure
• They said:
Each of the two samples should be subjected to exactly 1 atm pressure
• So the problem is solved
4. Next, the two samples must be at the same temperature
• Here also a problem arises. It can be explained in 2 steps
(i) Some labs may keep each of the two samples at a temperature of 298 K
(ii) Some other labs may keep each of the two samples at a temperature of 300 K
◼  In order to avoid such differences, scientists decided to fix up a temperature
• They said:
Each of the two samples should exactly be at a temperature of 273 K
• So the problem is solved
5. The S.T.P:
   ♦ The temperature 273 K is accepted world wide as standard temperature
   ♦ The pressure 1 atm is accepted world wide as standard pressure
◼  Together, they are known as: Standard temperature and pressure
   ♦ It is abbreviated as S.T.P
6. So all the samples in all the labs will be:
   ♦ Containing one mole each
   ♦ Subjected to 1 atm pressure
   ♦ At a temperature of 273 K
◼  Now we come to the interesting result about volume:
If the above three conditions are satisfied, each sample will be occupying a volume of 22.4 liters
7. The Avogadro number:
• One mole of gaseous molecules (belonging to any gas oxygen, nitrogen, argon etc.,) at 273 K and 1 atm pressure will be occupying a volume of 22.4 liters
◼  Conversely,
• 22.4 liters of any gas at 273 K and 1 atm pressure, will be containing one mole (6.023 × 1023) of molecules
◼  Since this fact was discovered by the Italian scientist Amedeo Avogadro, the number 6.023 × 1023 is called Avogadro number in his honor
   ♦ The symbol for Avogadro number is NA
• So we can write: NA = 6.023 × 1023


Next we will see the details about the Universal gas constant. It can be written in 7 steps:
1. We have seen that: $\mathbf\small{\rm{\frac{PV}{T}=N\;k_B}}$
• Dividing both sides by NA, we get: $\mathbf\small{\rm{\frac{PV}{T\;N_A}=\left(\frac{N}{N_A} \right)\;k_B}}$
2. But $\mathbf\small{\rm{\left(\frac{N}{N_A} \right)}}$ is the number of moles in the sample
   ♦ We will denote it as 𝝁
• So we get: $\mathbf\small{\rm{\frac{PV}{T\;N_A}=\mu\;K_B}}$
⇒ PV = 𝝁NAkBT
3. Both NA and kB are constants
• So multiplying them will give a new constant. Let us denote this new constant as R
• Then we get: Eq.13.2: PV = 𝝁RT
4. R is called the Universal Gas Constant. Because, it is same for all gases which are at STP
• Let us find the value of R. It can be done in 2 steps:
(i) We have: $\mathbf\small{\rm{R=\frac{PV}{\mu T}}}$
• At STP,
   ♦ P = 1 atm = 101325 N m-2
   ♦ V = 22.4 liters = (22.4 × 103) cm3 = (22.4 × 103 × 10-6) = 22.4 × 10-3 m3
   ♦ T = 273 K
   ♦ 𝝁 = 1 mole
(ii) Substituting these values in (i), we get:
$\mathbf\small{\rm{R=\frac{101325\;(Nm^{-2}) \times 22.4 \times 10^{-3} (m^3)}{1 \; (mole) \times 273 \; (K)}}}$ = 8.314 N m mole-1 K-1 = 8.314 J mole-1 K-1
5. We have seen that, 𝝁 of a sample is equal to $\mathbf\small{\rm{\left(\frac{N}{N_A} \right)}}$
• But it is easier to calculate 𝝁 using the relation: $\mathbf\small{\rm{\mu=\left(\frac{M}{M_0} \right)}}$
   ♦ Where
         ✰ M is the mass of the sample
         ✰ M0 is the molar mass of the gas
• We already know this relation from our chemistry classes
6. The equation PV = 𝝁RT can be written in another form. It can be derived in 2 steps
(i) We have Eq.13.1: PV = (NkB)T
• This can be rearranged as: $\mathbf\small{\rm{P=\left( \frac{N}{V} \right)k_BT}}$
(ii) Now, $\mathbf\small{\rm{\left( \frac{N}{V} \right)}}$ is the number density, that is, the number of molecules per unit volume. We can denote it as n
• Thus we get Eq.13.3: P = kB nT
7. Let us see yet another form. It can be derived in 2 steps:
(i) We have: Eq.13.2: PV = 𝝁RT
• This is same as: $\mathbf\small{\rm{PV=\left( \frac{M}{M_0} \right)RT}}$
This can be rearranged as: $\mathbf\small{\rm{P=\left( \frac{M}{VM_0} \right)RT}}$
(ii) Now, $\mathbf\small{\rm{\left( \frac{M}{V} \right)}}$ is the density. We can denote it as ρ
• Thus we get Eq.13.4: $\mathbf\small{\rm{P=\frac{\rho RT}{M_0}}}$


Next we can discuss about the Kinetic theory of an Ideal gas. Before taking up that discussion, we need to obtain a good understanding about Boyle's Law, Charles Law, Ideal gas equation etc., We have discussed them in some previous chapters in Chemistry. The links are given below:

1. Boyle's Law and Charles law

2. Avogadro's hypothesis and Details about STP

3. Ideal gas equation, Partial pressure and mole fraction

• Now we will see some solved examples. The link is given below:

Solved examples 13.1 to 13.11


In the next section, we will see Kinetic theory of an Ideal gas


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Friday, March 19, 2021

Chapter 12.11 - Solved Examples in Thermodynamics

In the previous section, we saw the second law of thermodynamics applied to heat engine and refrigerator. In this section, we will see some solved examples related to the topics that we saw in this chapter

Solved example 12.11
A geyser heats water flowing at the rate of 3.0 liters per minute from 27 °C to 77 °C. If the geyser operates on a gas burner, what is the rate of consumption of the fuel if its heat of combustion is 4.0 × 104 J/g ?
Solution:
1. Volume of water heated in one minute = 3 liter
2. So mass of water heated in one minute = [3(l)  × 1000 (g l-1)] = 3000 g = 3.0 kg
3. Heat absorbed in one minute =
Mass in one minute × Specific heat capacity × Change in temperature
4. Specific heat capacity of water = 4180 J kg-1 K-1
5. Change in temperature = (77 - 27) = 50 °C
6. Substituting the known values in (3),we get:
Heat absorbed in one minute =
3.0 (kg) × 4180 (J kg-1 K-1 ) × 50 K = 627000 J
7. Given that, one gram of the fuel gives 4.0 × 104 J
So number of grams of fuel required in one minute
= 627000 (J) ÷ 4.0 × 104 (J g-1) = 15.7 g

Solved example 12.12
What amount of heat must be supplied to 2.0 × 10-2 kg of nitrogen (at room
temperature) to raise its temperature by 45 °C at constant pressure ? (Molecular
mass of N2 = 28 g; R = 8.3 J mol-1 K-1)
Solution:
Method 1:
1. We have: Heat required =
Mass × Specific heat capacity × Change in temperature
2. Mass of nitrogen = 2.0 × 10-2 kg
3. From data book, we get:
Specific heat capacity of nitrogen (at constant pressure, cp) = 1040 J kg-1 K-1
4. Change in temperature = 45 °C
5. Substituting the known values in (1),we get:
Heat required =
2.0 × 10-2 (kg) × 1040 (J kg-1 K-1 ) × 45 (K) = 936 J

Method 2:
1. We have: Heat required =
Number of moles × Molar heat capacity × Change in temperature
2. Mass of nitrogen = 2.0 × 10-2 kg
• Molar mass of N2 = 28 gram
    ♦ So number of moles of N2 in 2.0 × 10-2 kg
          = [2.0 × 10-2 (kg) ÷ 28 × 10-3 (kg)] = 0.714 
3. For a diatomic gas, we have:
Molar heat capacity (at constant pressure, cp) = 72 R (We will derive this relation in the next chapter)
• Substituting for R, we get: cp = [72 × 8.3 (J mol-1 K-1)] =
4. Change in temperature = 45 °C
5. Substituting the known values in (1),we get:
Heat required =
0.714 (mol) × [72 × 8.3 (J mol-1 K-1)] × 45 (K) = 933.3 J

Solved example 12.13
A cylinder with a movable piston contains 3 moles of hydrogen at standard temperature and pressure. The walls of the cylinder are made of a heat insulator, and the piston is insulated by having a pile of sand on it. By what factor does the pressure of the gas increase if the gas is compressed to half its original volume ?
Solution:
1. From the description it is clear that, it is an adiabatic process
• We have the relation for adiabatic process: $\mathbf\small{\rm{P_1 V_1^\gamma = P_1 V_2^\gamma}}$
• For a diatomic gas, $\mathbf\small{\rm{\gamma}}$ = 1.4
2. Given that initially, the gas is at STP
    ♦ So P1 = 1 atm
• One mole of any ideal gas will occupy 22.4 L at STP
    ♦ So V1 = (3 × 22.4) L
3. Given that the gas is compressed to half it's original volume
    ♦ So V2 = 0.5V1
4. Substituting the known values in (1), we get:
$\mathbf\small{\rm{1 \; (atm) \times (3 \times 22.4 \; (L))^{1.4} = P_2 \times (0.5 \times 3 \times 22.4 \; (L))^{1.4}}}$
⇒ P2 = 2.64 × P1

Solved example 12.14
In changing the state of a gas adiabatically from an equilibrium state A to another
equilibrium state B, an amount of work equal to 22.3 J is done on the system. If the gas is taken from state A to B via a process in which the net heat absorbed by the system is 9.35 cal, how much is the net work done by the system in the latter case ? (Take 1 cal = 4.19 J)
Solution:
• There are two processes in this problem
    ♦ The first process is an adiabatic process
    ♦ The second process is not adiabatic
1. Let A and B be the initial and final states of the gas. Let W1 be the work done
• For any thermodynamic process, we have: UB = UA + Q - W
• For the first process,
Q = 0 and W1 is positive (since work is done on the gas)
• Thus we get: UB = (UA + W1) = (UA + 22.3 J)
⇒ UB - UA = 22.3 J
2. For the second process, we have:
UB = UA + (9.35 × 4.19) - W2
(Here W2 is negative because, work is done by the gas)
⇒ UB - UA = (9.35 × 4.19 J) - W2
3. What ever be the process, UA and UB will be the same
• So (UA - UB) will also be the same
• Equating the results in (1) and (2), we get:
UB - UA = 22.3 J = (9.35 × 4.19 J) - W2
⇒ W2 = [(9.35 × 4.19 J) - 22.3] = 16.9 J

Solved example 12.15
Two cylinders A and B of equal capacity are connected to each other via a stopcock. A contains a gas at standard temperature and pressure. B is completely evacuated. The entire system is thermally insulated. The stopcock is suddenly opened. Answer the following :
(a) What is the final pressure of the gas in A and B ?
(b) What is the change in internal energy of the gas ?
(c) What is the change in the temperature of the gas ?
(d) Do the intermediate states of the system (before settling to the final equilibrium state) lie on its P-V-T surface ?
Solution:
• For an ideal gas, we have: $\mathbf\small{\rm{\frac{P_1 V_1}{T_1} = \frac{P_2 V_2}{T_2}}}$
• For our present problem, it is given that the entire system is thermally insulated
    ♦ So no heat will enter or leave the system
Part (c): Cylinder B is initially a vacuum
• The gas in A, expands and fills into B. For this, no work is necessary because, the gas is expanding against vacuum
• Since no work is done on/by the gas, the temperature remains the same
    ♦ That is., T1 = T2
    ♦ So change in temperature = (T2 - T1) = 0
Part (a):
• Since T1 = T2, we get: P1V1 = P2V2
• Given that:
    ♦ P1 = 1 atm and V1 = V2
    ♦ So final volume available = 2V1
• So we get: 1 × V1 = P2 × 2V1
⇒ P2 = 0.5 atm
Part (b):
• Since work done is zero and heat exchange is also zero, there will be no change in internal energy
• That is., change in internal energy = 0
Part (d):
• This is a rapid process
• The intermediate P and V values will be fluctuating
• So those values will not lie on the P-V-T surface
(see fig.12.4 in the first section of this chapter)

Solved example 12.16
A steam engine delivers 5.4×108 J of work per minute and services 3.6 × 109 J of heat per minute from its boiler. What is the efficiency of the engine? How much heat is wasted per minute?
Solution:
Part (a):
• Efficiency is given by: $\mathbf\small{\rm{\eta = \frac{Output}{Input}}}$
• Substituting the values, we get:
$\mathbf\small{\rm{\eta = \frac{5.4 \times 10^8 (J)}{3.6 \times 10^9 (J)}}}$ = 0.15 = 15%
Part (b):
Energy wasted = [Input energy - Output work]
= [3.6 × 109 - 5.4×108] = 30.6 ×108 J   

Solved example 12.17
An electric heater supplies heat to a system at a rate of 100 W. If system performs
work at a rate of 75 joules per second. At what rate is the internal energy increasing?
Solution:
1. 100 W is 100 J s-1
• So energy absorbed by the system in one second, Q = 100 J
2. Work done by the system in one second = 75 J
3. We can write: UB = UA + 100 J - 75 J
• Work is given a negative sign because, it is done by the system
4. Thus we get:
Change in internal energy in one second
= (UB - UA) = (100 - 75) = 25 J

Solved example 12.18
A thermodynamic system is taken from an original state to an intermediate state by the linear process shown in Fig. (12.25). Its volume is then reduced to the original value from E to F by an isobaric process. Calculate the total work done by the gas from D to E to F

Internal energy of a system does not depend on the path.
Fig.12.25

Solution:
1. In the initial process, work is done by the gas while expanding from VD to VE
• This work will be equal to:
The area between segment DE and the x-axis
2. In the second process, work is done on the gas while compressing it from VE to VF
• This work is equal to:
The area between segment EF and x-axis
3. So the net work done by the gas is equal to:
The area of the triangle DEF
   ♦ Base of the triangle = (5 - 2) = 3
   ♦ Altitude of the triangle = (600 - 300) = 300
   ♦ So area of the triangle = 12 × 3 (m3) × 300 (N m-2) = 450 J


In the next chapter, we will see kinetic theory


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Thursday, March 18, 2021

Chapter 12.10 - Second Law of Thermodynamics

In the previous section, we saw the COP of the Carnot refrigerator. In this section, we will see the second law of thermodynamics and it's applications in Carnot engine and refrigerator

The Second law of thermodynamics

◼  The second law of thermodynamics states that:
When a spontaneous process occurs, the entropy of the universe always increases
   ♦ So a process will take place only in that direction which causes an increase in entropy
   ♦ Entropy is a measure of randomness or disorder
• Links to detailed notes on entropy and some related topics are given below:

   ♦ Spontaneity

   ♦ Entropy

   ♦ Second law of thermodynamics

   ♦ Gibbs free energy

• Based on the above discussion, we can write the reason for phenomena such as:
   ♦ Heat never flows from a cold object to a hot object
         ✰ Heat always flow from hot object to cold object
         ✰ A hot object has greater entropy than a cold object
   ♦ Water never spontaneously become ice
         ✰ Water has greater entropy than ice

• Application of second law to heat engines gives the explanation for why no heat engine can have 100 % efficiency
• Application of second law to refrigerator gives the explanation for why no refrigerator can have a COP of infinity

 

Application to Carnot Engine

• Let us find the entropy changes in a Carnot engine
    ♦ For that, we consider one complete cycle of the engine
    ♦ There are two isothermal processes and two adiabatic processes in one complete cycle
• The PV diagram is shown again below:

• There is no exchange of heat during the adiabatic processes
    ♦ So there is no entropy changes during the adiabatic processes
• We need to consider the isothermal processes only. We can write it in 9 steps:
1. First isothermal process AB:
(i) In the first isothermal process, the hot reservoir gives away some heat
   ♦ Let this heat given away be Qh
   ♦ Let Qi(HR) be the initial heat content of the hot reservoir
   ♦ Let Qf(HR) be the final heat content of the hot reservoir
• Then Qh = Qf(HR) – Qi(HR)
• This Qh will be a negative quantity because, Qf(HR) will be less than Qi(HR)
◼  So the entropy change suffered by the hot reservoir = $\mathbf\small{\rm{-\frac{Q_h}{T_1}}}$
(ii) The same heat content Qh is gained by the gas
   ♦ Let Qi(HG) be the initial heat content of the hot gas
   ♦ Let Qf(HG) be the final heat content of the hot gas
   ♦ Then Qh = Qf(HG) – Qi(HG)
• This Qh will be a positive quantity because, Qf(HG) will be greater than Qi(HG)
◼  So the entropy change suffered by the hot gas = $\mathbf\small{\rm{+\frac{Q_h}{T_1}}}$
2. Second isothermal process AB:
(i) In the second isothermal process, the cold reservoir receives some heat
   ♦ Let this received heat be Qc
   ♦ Let Qi(CR) be the initial heat content of the cold reservoir
   ♦ Let Qf(CR) be the final heat content of the cold reservoir
• Then Qc = Qf(CR) – Qi(CR)
• This Qc will be a positive quantity because, Qf(CR) will be greater than Qi(CR)
◼  So the entropy change suffered by the cold reservoir = $\mathbf\small{\rm{+\frac{Q_c}{T_2}}}$
(ii) The same heat content Qc is lost by the gas
   ♦ Let Qi(CG) be the initial heat content of the cold gas
   ♦ Let Qf(CG) be the final heat content of the cold gas
   ♦ Then Qc = Qf(CG) – Qi(CG)
• This Qc will be a negative quantity because, Qf(CG) will be less than Qi(CG)
◼  So the entropy change suffered by the cold gas = $\mathbf\small{\rm{-\frac{Q_c}{T_2}}}$
3. So now we have four entropy changes:
(i) Entropy change suffered by the hot reservoir, $\mathbf\small{\rm{-\frac{Q_h}{T_1}}}$. This we calculated in 1(i)
(ii) Entropy change suffered by the hot gas, $\mathbf\small{\rm{\frac{Q_h}{T_1}}}$. This we calculated in 1(ii)
(iii) Entropy change suffered by the cold reservoir, $\mathbf\small{\rm{+\frac{Q_c}{T_2}}}$. This we calculated in 2(i)
(iv) Entropy change suffered by the cold gas, $\mathbf\small{\rm{-\frac{Q_c}{T_2}}}$. This we calculated in 2(ii)
4. We have the basic equation:
Entropy change suffered by the universe
= Entropy change suffered by the system + Entropy change suffered by the surroundings
5. Let us calculate each item on the right side of the above equation:
(i) Entropy change suffered by the system
= Entropy change suffered by the gas = Item 3(ii) + Item 3(iv)
= $\mathbf\small{\rm{\frac{Q_h}{T_1}-\frac{Q_c}{T_2}}}$
(ii) Entropy change suffered by the surroundings
= Entropy change suffered by the reservoirs = Item 3(i) + Item 3(iii)
= $\mathbf\small{\rm{-\frac{Q_h}{T_1}+\frac{Q_c}{T_2}}}$
6. Consider the Eq.12.15 that we derived in section 12.8:
$\mathbf\small{\rm{\frac{Heat \;Rejected}{Heat \; Absorbed} =  \frac{T_2}{T_1}}}$
This is same as: $\mathbf\small{\rm{\frac{Q_c}{Q_h} =  \frac{T_2}{T_1} }}$
⇒ $\mathbf\small{\rm{\frac{Q_c}{T_2} =  \frac{Q_h}{T_1} }}$
• Based on this result,
   ♦ 5(i) will become zero
   ♦ 5(ii) will also become zero
7. So we can write:
◼  Entropy change suffered by the system = 0
◼  Entropy change suffered by the surroundings = 0
• So the result in (4) becomes:
◼  Entropy change suffered by the universe = 0
• That means, when one cycle of the Carnot engine is complete, the universe suffers zero entropy change
8. This is an ideal situation
• It shows that, the Carnot engine is most efficient
• All real engines will cause the universe to suffer a positive entropy change
• This is because, all real engines dump some net heat (caused due to friction) into the surroundings
• The Carnot engine is a theoretical engine. We assume that, there is no friction
9. Now let us see if we can attain 100 % efficiency. It can be written in 6 steps:
(i) If there is to be 100% efficiency, Qc must be zero
• That is., there should be no heat exchange with a cold reservoir
• This condition of 'no heat exchange with cold reservoir' can be easily seen from the schematic diagram of a heat engine that we saw in a previous section. It is shown again below:

For 100% efficiency in Carnot engine, Qc must be zero


• It is clear that, for 100% efficiency, Qc must be zero
(ii) If Qc is not to be given, the cold reservoir will be absent in the engine
• So there will not be any need for the three segments BC, CD and DA
• All the heat received from the hot reservoir will be converted into work
(iii) In such a situation,
    ♦ Entropy change suffered by the surroundings (hot reservoir) = $\mathbf\small{\rm{-\frac{Q_h}{T_1}}}$
    ♦ Entropy change suffered by the gas (system) = $\mathbf\small{\rm{\frac{Q_h}{T_1}}}$
(iv) Here also, the net entropy change of system and surroundings is equal to zero
• That means, the entropy change suffered by the universe is zero
• This does not violate the second law
(v) So we are inclined to adopt such an engine, where all heat is converted into work
• But such an engine can perform work only in one segment AB
• It will not return to it's original state
(If we try to return along the same path BA, the same work will have to be done on the gas, resulting in zero net work)
◼ So it cannot perform the next cycle. We can obtain continuous work only if the engine operates in cycles
(vi) Thus it is clear that, to obtain a cyclic process, some heat has to be definitely given to the cold reservoir
• When some heat is given to the cold reservoir, efficiency will become less than 100 %
• That is why, we cannot obtain 100 % efficiency


Application to Carnot Refrigerator

• Let us find the entropy changes in a Carnot refrigerator
    ♦ For that, we consider one complete cycle of the refrigerator
    ♦ There are two isothermal processes and two adiabatic processes in one complete cycle
• The PV diagram is shown again below:

• There is no exchange of heat during the adiabatic processes
    ♦ So there is no entropy changes during the adiabatic processes
• We need to consider the isothermal processes only
• Those isothermal processes are just the reverse of what we saw in the engine
• So it is easy to prove that, in the case of refrigerator also, the entropy change suffered by the universe is zero
   ♦ The steps are left to the reader
• Our next aim is to check whether it is possible to make a refrigerator with COP infinity. It can be written in 6 steps:
(i) If there is to be infinite COP, W must be zero
• That is., there should be zero work requirement
    ♦ The cooling must be accomplished with out external work
• This condition can be easily seen from the schematic diagram of a refrigerator that we saw in a previous section. It is shown again below:

For the refrigerator to have infinite coefficient of performance (COP), W must be zero

• It is clear that, for infinite COP, W must be zero
(ii) If W is not to be given, the segments CB and BA will be absent in the PV diagram below
   ♦ Because, W is applied during those segments
   ♦ The gas gets compressed during those segments
(iii) If those two segments are absent, entropy changes occur only during DC
    ♦ During DC, the entropy change suffered by the surroundings (hot reservoir) = $\mathbf\small{\rm{-\frac{Q_c}{T_2}}}$
    ♦ During DC, the entropy change suffered by the gas (system) = $\mathbf\small{\rm{\frac{Q_c}{T_2}}}$
(iv) Here also, the net entropy change of system and surroundings is equal to zero
• That means, the entropy change suffered by the universe is zero
• This does not violate the second law
(v) So we are inclined to adopt such a refrigerator, where no external work is required
(vi) But, if we avoid paths CB and BA, the gas cannot reach the hot temperature T1
• It is essential to reach the hot reservoir temperature T1 to dump the heat
• If we decide to retrace the path CD, the absorbed heat will be given back to the  cold reservoir
   ♦ This will not effect cooling
◼ We can obtain continuous extraction of heat only if the refrigerator operates in cycles
(vi) Thus it is clear that, to obtain a cyclic process, some work has to be definitely done
• When some work is done, COP will become less than infinity
• That is why, we cannot obtain infinite COP

We have completed our present discussion on thermodynamics. In the next section, we will see some solved examples related to the various topics that we saw in this chapter



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Tuesday, March 16, 2021

Chapter 12.9 - COP of a Carnot Refrigerator

In the previous section, we saw the efficiency of the Carnot engine. In this section, we will see details about the Carnot refrigerator

• A Carnot engine can be operated in the reverse direction to work as a Carnot refrigerator
• The four segments in the PV diagram will reverse their directions. This is shown in fig.6.24 below:

Carnot refrigerator is the reverse of Carnot engine
Fig.12.24

The basic working can be explained in 4 steps:
1. The cycle begins at point D. The first segment is DC
    ♦ The engine is placed in contact with the cold reservoir of temperature T2
    ♦ The engine extracts heat from the cold reservoir and expands isothermally
2. The second segment is CB
    ♦ The engine is placed inside an insulator
    ♦ The gas is compressed adiabatically
    ♦ The temperature increases to T1
3. The third segment is BA
    ♦ The engine is placed in contact with the hot reservoir of temperature T1
    ♦ The gas is compressed isothermally
    ♦ During this compression, the gas rejects some heat into the hot reservoir
4. The fourth segment is AD
    ♦ The engine is placed inside an insulator
    ♦ The gas is allowed to expand adiabatically
    ♦ The temperature falls to T2
• Thus the initial point D is reached, completing one cycle
Next we will calculate the work done in each segment:

First segment from D to C
• In this segment, the gas place in contact with T2 and subjected to an isothermal expansion
    ♦ Volume increases from VD to VC
    ♦ Pressure decreases from PD to PC
    ♦ Temperature remains constant at T2
• We know that, the work done by the ideal gas during the isothermal expansion will be equal to: $\mathbf\small{\rm{n R T_2\,\,ln \frac{V_C}{V_D}}}$ (see Eq.12.3 at end of section 12.2)

Second segment from C to B
• In this segment, the gas is subjected to an adiabatic compression
    ♦ Volume decreases from VC to VB
    ♦ Pressure increases from PC to PB
• We know that, the work done by the ideal gas during the adiabatic expansion will be equal to: $\mathbf\small{\rm{\frac{nR(T_1 \, - \, T_2)}{\gamma\, - \,1}}}$ (see Eq.12.6 at end of section 12.3)

Third segment from B to A
• In this segment, the gas is subjected to an isothermal compression
    ♦ Volume decreases from VB to VA
    ♦ Pressure increases from PB to PA
    ♦ Temperature remains constant at T1
• We know that, the work done on the ideal gas during the isothermal compression will be equal to: $\mathbf\small{\rm{n R T_1\,\,ln \frac{V_B}{V_A}}}$

Fourth segment from A to D
• In this segment, the gas is subjected to an adiabatic expansion
    ♦ Volume increases from VA to VD
    ♦ Pressure decreases from PA to PD
• We know that, the work done by the ideal gas during the adiabatic compression will be equal to: $\mathbf\small{\rm{\frac{nR(T_1 \, - \, T_2)}{\gamma\, - \,1}}}$


Now we can find the coefficient of performance (COP) of the Carnot refrigerator. It can be written in steps:
1. Net work, W = Work done by the gas - Work done on the gas
   ♦ Work done by the gas = Work done during segments one and four
   ♦ Work done on the gas = Work done during segments two and three
• Thus we get:
W = $\mathbf\small{\rm{\left (n R T_2\,\,ln \frac{V_C}{V_D}+\frac{nR(T_1 \, - \, T_2)}{\gamma\, - \,1}\right )- \left ( \frac{nR(T_1 \, - \, T_2)}{\gamma\, - \,1}+n R T_1\,\,ln \frac{V_B}{V_A} \right)}}$
⇒ W = $\mathbf\small{\rm{\left (n R T_2\,\,ln \frac{V_C}{V_D}-n R T_1\,\,ln \frac{V_B}{V_A} \right)}}$


• An interesting comparison:
    ♦ In the previous section for the engine, we obtained the net work as:
          $\mathbf\small{\rm{\left (n R T_1\,\,ln \frac{V_B}{V_A}- n R T_2\,\,ln \frac{V_C}{V_D} \right)}}$
    ♦ In this section for the refrigerator, we obtain the net work as:
          $\mathbf\small{\rm{\left (n R T_2\,\,ln \frac{V_C}{V_D}-n R T_1\,\,ln \frac{V_B}{V_A} \right)}}$
    ♦ Both are equal in magnitude but opposite in sign
◼ That means:
    ♦ In the engine, work is done by the gas
    ♦ In the refrigerator (reversed engine), the same work is done on the gas


2. We know that, COP of a refrigerator is given by:
$\mathbf\small{\rm{\alpha = \frac{Heat \; Absorbed \; from \; cold \; reservoir}{Net \; Work}}}$ (see Eq.12.12 in section 12.6)
3. Also, we have derived another form of the above equation:
$\mathbf\small{\rm{\alpha = \frac{Heat \; Absorbed \; from \; cold \; reservoir}{Net \; Heat}}}$ (see Eq.12.13 in section 12.6)
• It is easier to find COP using this equation
4. So our next task is to find the 'Heat absorbed' and the 'Heat rejected'
• It can be done in steps:
(i) We know that, heat absorption takes place only during the first segment
• It is an isothermal process
• In an isothermal process, Heat absorbed/rejected is equal to the work done during that process
• So we get: Heat absorbed = $\mathbf\small{\rm{n R T_1\,\,ln \frac{V_C}{V_D}}}$
(ii) We know that, heat rejection takes place only during the third segment
• It is an isothermal process
• In an isothermal process, Heat absorbed/rejected is equal to the work done during that process
• So we get: Heat rejected = $\mathbf\small{\rm{n R T_2\,\,ln \frac{V_B}{V_A}}}$
5. So the result in (3) becomes: $\mathbf\small{\rm{\alpha = \frac{n R T_2\,\,ln \frac{V_C}{V_D}}{n R T_1\,\,ln \frac{V_B}{V_A}-n R T_2\,\,ln \frac{V_C}{V_D}}}}$
6. In the previous section, we compared the two adiabatic segments, and proved that: $\mathbf\small{\rm{\left (\frac{V_C}{V_D} \right )=\left (\frac{V_B}{V_A} \right )}}$
• So the result in (5) becomes:
$\mathbf\small{\rm{\alpha = \frac{n R T_2\,\,ln \frac{V_C}{V_D}}{n R T_1\,\,ln \frac{V_C}{V_D}-n R T_2\,\,ln \frac{V_C}{V_D}}}}$
⇒ $\mathbf\small{\rm{\alpha = \frac{n R T_2\,\,ln \frac{V_C}{V_D}}{n R \,\,ln \frac{V_C}{V_D}(T_1 - T_2)}}}$
• Thus we get:
Eq.12.16: $\mathbf\small{\rm{\alpha = \frac{T_2}{T_1 - T_2}}}$
7. Two expressions for COP:
   ♦ The above Eq.12.16 gives us an expression for COP
   ♦ Step (3) also gives us an expression for COP
• So we can equate the two. We get Eq.12.17:
$\mathbf\small{\rm{\frac{Heat \; Absorbed \; from \; cold \; reservoir}{Net \; Heat}=\frac{T_2}{T_1 - T_2}}}$

Let us see a solved example
Solved example 12.11
A refrigerator is to maintain eatables kept inside at 9 C. If room temperature is 36 C, Calculate the coefficient of performance
Solution:
1. Given that:
   ♦ Temperature of the hot reservoir T1 = 36 C = (273 + 36) = 309 K
   ♦ Temperature of the cold reservoir T2 = 9 C = (273 + 9 ) = 282 K
2. We have Eq.12.16: $\mathbf\small{\rm{\alpha = \frac{T_2}{T_1 - T_2}}}$
• Substituting the values, we get:
$\mathbf\small{\rm{\alpha = \frac{282}{309 - 282}}}$ = 10.44


In the next section, we will see the second law of thermodynamics and it's application to heat engines and refrigerators


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Chapter 12.8 - Efficiency of a Carnot Engine

In the previous section, we saw the basic processes in a Carnot engine. In this section, we will see the work done during each of those processes. For easy reference, the final PV diagram is shown below:

PV Diagram for a Carnot Engine showing various steps
Fig.12.23

First segment from A to B
• In this segment, the gas is subjected to an isothermal expansion
• We know that, the work done by the ideal gas during the isothermal expansion will be equal to: $\mathbf\small{\rm{n R T_1\,\,ln \frac{V_B}{V_A}}}$ (see Eq.12.3 at end of section 12.2)

Second segment from B to C
• In this segment, the gas is subjected to an adiabatic expansion
• We know that, the work done by the ideal gas during the adiabatic expansion will be equal to: $\mathbf\small{\rm{\frac{nR(T_1 \, - \, T_2)}{\gamma\, - \,1}}}$ (see Eq.12.6 at end of section 12.3)

Third segment from C to D
• In this segment, the gas is subjected to an isothermal compression
• We know that, the work done on the ideal gas during the isothermal compression will be equal to: $\mathbf\small{\rm{n R T_2\,\,ln \frac{V_C}{V_D}}}$

Fourth segment from D to A
• In this segment, the gas is subjected to an adiabatic compression
• We know that, the work done by the ideal gas during the adiabatic compression will be equal to: $\mathbf\small{\rm{\frac{nR(T_1 \, - \, T_2)}{\gamma\, - \,1}}}$


Now we can find the efficiency of the Carnot engine. It can be written in 9 steps:
1. Net work, W = Work done by the gas - Work done on the gas
   ♦ Work done by the gas = Work done during segments one and two
   ♦ Work done on the gas = Work done during segments three and four
• Thus we get:
W = $\mathbf\small{\rm{\left (n R T_1\,\,ln \frac{V_B}{V_A}+\frac{nR(T_1 \, - \, T_2)}{\gamma\, - \,1}\right )- \left ( n R T_2\,\,ln \frac{V_C}{V_D}+\frac{nR(T_1 \, - \, T_2)}{\gamma\, - \,1} \right)}}$
⇒ W = $\mathbf\small{\rm{\left (n R T_1\,\,ln \frac{V_B}{V_A}- n R T_2\,\,ln \frac{V_C}{V_D} \right)}}$
2. We know that, efficiency of a heat engine is given by:
$\mathbf\small{\rm{\eta = \frac{Net \; Work}{Heat \; Absorbed}}}$ (see Eq.12.9 in section 12.5)
3. Also, we have derived another form of the above equation:
$\mathbf\small{\rm{\eta = 1-\frac{Heat \;Rejected}{Heat \; Absorbed}}}$ (see Eq.12.10 in section 12.5)
• It is easier to find efficiency using this equation
4. So our next task is to find the 'Heat absorbed' and the 'Heat rejected'
• It can be done in steps:
(i) We know that, heat absorption takes place only during the first segment
• It is an isothermal process
• In an isothermal process, Heat absorbed/rejected is equal to the work done during that process
• So we get: Heat absorbed = $\mathbf\small{\rm{n R T_1\,\,ln \frac{V_B}{V_A}}}$
(ii) We know that, heat rejection takes place only during the third segment
• It is an isothermal process
• In an isothermal process, Heat absorbed/rejected is equal to the work done during that process
• So we get: Heat rejected = $\mathbf\small{\rm{n R T_2\,\,ln \frac{V_C}{V_D}}}$
5. So the result in (3) becomes: $\mathbf\small{\rm{\eta = 1-\frac{n R T_2\,\,ln \frac{V_C}{V_D}}{n R T_1\,\,ln \frac{V_B}{V_A}}}}$
⇒ $\mathbf\small{\rm{\eta = 1- \left (\frac{T_2}{T_1} \right ) \left (\frac{ln \frac{V_C}{V_D}}{ln \frac{V_B}{V_A}}\right )}}$
6. We see that, the right side of the above equation involves temperatures and volumes. So our next task is to find the relations between them
• For that, we consider the two adiabatic processes in the cycle. It can be written in two steps:
(i) For the  adiabatic process BC, we have the relation:
$\mathbf\small{\rm{\left (\frac{V_C}{V_B} \right )^{\gamma - 1}=\left (\frac{T_1}{T_2} \right )}}$
(see Eq.12.7 of section 12.3)
(ii) Similarly, for the adiabatic process DA, we have the relation:
$\mathbf\small{\rm{\left (\frac{V_D}{V_A} \right )^{\gamma - 1}=\left (\frac{T_1}{T_2} \right )}}$
(iii) The right sides in (i) and (ii) are the same. So we get:
$\mathbf\small{\rm{\left (\frac{V_C}{V_B} \right )^{\gamma - 1}=\left (\frac{V_D}{V_A} \right )^{\gamma - 1}}}$
⇒ $\mathbf\small{\rm{\left (\frac{V_C}{V_B} \right )=\left (\frac{V_D}{V_A} \right )}}$
⇒ $\mathbf\small{\rm{\left (\frac{V_C}{V_D} \right )=\left (\frac{V_B}{V_A} \right )}}$
7. We see the above result in (5)
So the result in (5) becomes:
Eq.12.14: $\mathbf\small{\rm{\eta = 1- \left (\frac{T_2}{T_1} \right )}}$
8. Two expressions for efficiency:
   ♦ The above Eq.12.14 gives us an expression for efficiency
   ♦ Step (3) also gives us an expression for efficiency
• So we can equate the two:
$\mathbf\small{\rm{1-\frac{Heat \;Rejected}{Heat \; Absorbed} = 1- \left (\frac{T_2}{T_1} \right )}}$
• Thus we get Eq.12.15:
$\mathbf\small{\rm{\frac{Heat \;Rejected}{Heat \; Absorbed} =  \left (\frac{T_2}{T_1} \right )}}$

⇒ $\mathbf\small{\rm{\frac{Heat \;Rejected}{Heat \; Absorbed} =  \left (\frac{Temperature \; of \; cold \; reservoir}{Temperature \; of \; hot \; reservoir} \right )}}$
9. Let us use try the results in (1) and (2) to find efficiency. it can be written in 3 steps:
(i) Using the result in (6), the result in (1) becomes:
W = $\mathbf\small{\rm{n R \,ln \frac{V_B}{V_A}\left ( T_1\,- T_2 \right)}}$
(ii) Using the result in 4(i), we have:
Heat absorbed = $\mathbf\small{\rm{n R T_1\,\,ln \frac{V_B}{V_A}}}$
(iii) Applying the above two results into (2), we get:
$\mathbf\small{\rm{\eta = \frac{n R \,ln \frac{V_B}{V_A}\left ( T_1\,- T_2 \right)}{n R T_1\,\,ln \frac{V_B}{V_A}}=\frac{T_1 - T_2}{T_1}}}$
⇒ $\mathbf\small{\rm{\eta =1-\left (\frac{T_2}{T_1} \right )}}$
This is the same result as in Eq.12.14


Let us see a solved example
Solved example 12.10
Three heat engines operate between the following temperature differences
    ♦ Engine A: T1 = 1000 K, T2 = 700 K
    ♦ Engine A: T1 = 800 K, T2 = 500 K
    ♦ Engine A: T1 = 600 K, T2 = 300 K
• Which is the most efficient engine?
• Which is the least efficient engine?
Solution:
1. Efficiency of a heat engine is given by Eq.12.14: $\mathbf\small{\rm{\eta = 1- \left (\frac{T_2}{T_1} \right )}}$
• So we get:
    ♦ Efficiency of Engine A = $\mathbf\small{\rm{\eta = 1- \left (\frac{700}{1000} \right )}}$ = 0.3
    ♦ Efficiency of Engine B = $\mathbf\small{\rm{\eta = 1- \left (\frac{500}{800} \right )}}$ = 0.375
    ♦ Efficiency of Engine C = $\mathbf\small{\rm{\eta = 1- \left (\frac{300}{600} \right )}}$ = 0.5
2. We can write:
    ♦ Engine C is the most efficient
    ♦ Engine A is the least efficient
3. Dependence of efficiency on temperature:
    ♦ We see that, the temperature difference is the same for all three engines
    ♦ In such a situation, the engine with the smallest T2 has the most efficiency 


In the next section, we will see Carnot refrigerator


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Sunday, March 14, 2021

Chapter 12.7 - The Carnot Engine

In the previous section, we saw the basics about refrigerator. In this section, we will see the Carnot engine

Carnot Engine

The basic processes involved in the working of a Carnot engine can be written in 14 steps:
1. A Carnot engine is an ideal engine
• To make it ideal, two restrictions are imposed:
(i) Every process that occur during the working of a Carnot engine must be reversible
(ii) The working gas inside the engine must be an ideal gas
2. We have seen the details about reversible process in the first section of this chapter (see fig.12.4 of the first section)
• Based on that, we can write:
    ♦ At any instant during the working of a Carnot engine, the gas inside the engine will have the same temperature as the surroundings
    ♦ We can change the direction of the reversible process any time we want
    ♦ A reversible process can proceed only very slowly
   ♦ So the Carnot engine will be very slow. But it gives us a base to study other real irreversible engines
3. Initially, the gas is at state A
• For the engine to start operating, we have to supply heat
   ♦ So the cylinder is placed in contact with a hot reservoir
   ♦ This is shown in fig. 12.19(a) below
   ♦ The temperature of this hot reservoir is maintained at T1 K
• So at this state, the V, P, T values of the gas will be: (VA, PA, TA)
    ♦ Where TA = T1

Step 1 in the carnot engine involves isothermal expansion
Fig.12.19
4. The gas absorbs heat and expands. Thus work is done on the piston
• This expansion process should be isothermal
• Processes like isobaric, isochoric or adiabatic cannot be used
    ♦ The reason can be seen here
• At the end of this isothermal process, the gas reaches state B
    ♦ Pressure PA decreases to a lower value PB
    ♦ Volume VA increases to a higher value VB
    ♦ Temperature remains the same because it is an isothermal process
• So at this state, the V, P, T values of the gas will be: (VB, PB, TB)
    ♦ Where TB = T1
• This process is represented by the red curve AB in fig.12.19(b)
• The first segment of the cycle is complete
5. Next we will see not the second segment, but another important segment
• Some quantity of heat is to be dumped into a cold reservoir
• Only then, can the gas return to the initial state and become ready for the next cycle
   ♦ For that, we place the cylinder in contact with a cold reservoir
   ♦ This is shown in fig.12.20(a) below
   ♦ The temperature of the cold reservoir is maintained at T2 K
• So at this state, the V, P, T values of the gas will be: (VC, PC, TC)
    ♦ Where TC = T2

Step 3 in Carnot engine involves isothermal compression
Fig.12.20

6. The gas is compressed isothermally. Thus work is done on the gas
• Processes like isobaric, isochoric or adiabatic cannot be used
    ♦ The reason is same (but in reverse order)as that we saw for the first segment
    ♦ The discussion can be seen here
• At the end of this isothermal process, the gas reaches state D
    ♦ Pressure PC increases to a higher value PD
    ♦ Volume VC decreases to a lower value VD
    ♦ Temperature remains the same because it is an isothermal process
• So at this stage, the V, P, T values of the gas will be: (PD, VD, TD)
    ♦ Where TD = T2
• This process is represented by the red curve CD in fig.12.20(b)
• This segment of the cycle is complete
7. The two segments mentioned above are important and inevitable segments
• During AB, the gas absorbs heat and does useful work
• But the gas has to return to it's initial state to start the next cycle
   ♦ For that, it has to dump the heat
   ♦ This dumping is done during CD
8. But we see a problem. It can be explained in 2 steps:
(i) The curve AB is separated away from curve CD
• This is obvious because, they are isotherms
    ♦ Every point in AB will be at temperature T1
    ♦ Every point in CD will be at temperature T2
    ♦ Two isotherms will never meet
(ii) So our problem is this:
How to reduce the temperature of the gas from T1 (at state B) to T2 (at state C)
9. Just after state B, we must subject the gas to a suitable process so that, the temperature falls to T2
◼ Which process is suitable?
• An adiabatic process is the only suitable process
• Processes like isobaric, isochoric or isothermal cannot be used
    ♦ The reason can be seen here
10. An adiabatic process is most suitable for achieving our goal
• Just after state B, the cylinder is placed in a thermal insulator
This is shown in fig.6.21 below:

Step 2 in Carnot engine involves adiabatic expansion
Fig.6.21

• The gas is then allowed to expand adiabatically
   ♦ So no heat will be lost or gained
• The gas will use it's own internal energy to expand
   ♦ This results in the decrease in temperature of the gas from TB to TC (T1 to T2)
• Thus we successfully established the connection between the first and third segments
11. Next we want to establish the connection between the third and first segments
• That is., between points D and A
• During the process from D to A,
    ♦ The volume decreases from VD to VA
    ♦ The pressure increases from PD to PA
    ♦ Temperature increases from T2 to T1
• So our problem is this:
How to increase the temperature of the gas from T2 (at state D) to T1 (at state A)
12. Just after state D, we must subject the gas to a suitable process so that, the temperature rises to T1
◼ Which process is suitable?
• An adiabatic process is the only suitable process
• Processes like isobaric, isochoric or adiabatic cannot be used
    ♦ The reason is same (but in reverse order)as that we saw for the second segment
    ♦ The discussion can be seen here
13. An adiabatic process is most suitable for achieving our goal
• Just after state C, the cylinder is placed in a thermal insulator
This is shown in fig.6.22 below:

Step 4 in Carnot engine involves adiabatic compression
Fig.6.22

• The gas is then compressed adiabatically
   ♦ This results in the increase in temperature of the gas from TD to TA (T2 to T1)
• Thus we successfully established the connection between the third and first segments
• The cycle is now complete
14. Let us write a summary. It can be written in 4 steps:
(i) We supply energy to the gas during the first segment
    ♦ During this segment, the gas expands and does useful work
    ♦ The supply of energy is stopped at the end of the first segment
(ii) During the second segment also, useful work is done by the gas
    ♦ But this time, the gas expands using it's internal energy
    ♦ The temperature falls to T2 during this segment
(iii) The gas has to return to it's original state so that another cycle can begin
    ♦ So in the third and fourth segments, the gas undergoes compression
    ♦ In the third segment, the compression is carried out at a lower temperature T2
        ✰ So it is easier to achieve compression
(iv) In the fourth segment, the temperature rises back to T1
    ♦ This is because, no heat is allowed to escape during the compression


• So now we know the four processes involved in the Carnot cycle
• Next we want to calculate the work done in each of the four segments in the cycle
• We will see it in the next section


Discussion on the notes can be started here

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Saturday, January 23, 2021

Chapter 12.6 - The Refrigerator

In the previous section we saw the details about heat engine. In this section, we will see the reverse of the heat engine cycle

• In the heat engine, we denoted the cycle as A-B-A. So the reverse cycle will be: B-A-B.
• However, to avoid confusion, we will use the letters M and N instead of A and B
• The basics of the reverse cycle can be written in 12 steps:
1. Consider fig.12.17 below
• It shows a cyclic process M-N-M
    ♦ The forward process M-N is along the green curve
    ♦ The backward process N-M is along the red curve

Thermodynamic cycles of refrigeration. It is the reverse of the cycles in heat engine.
Fig.12.17

2. In the forward process, volume of the gas decreases from VM to VN
    ♦ We can consider this as the downward motion of the piston
    ♦ So work is done on the gas during the forward process
3. In the backward process, volume of the gas increases from VN to VM
    ♦ We can consider this as the upward motion of the piston
    ♦ So work is done by the gas during the backward process
4. We can write:
    ♦ The piston starts from the extreme high point M
    ♦ Lowers down to the extreme low point N
    ♦ Returns to the extreme high point M
• This completes one cycle
5. Consider the forward process M-N
    ♦ Let the heat released by the gas during this process be QMN
    ♦
Let the work done on the gas during this process be WMN

• Then we get: UN = UM - QMN + WMN
⇒ UN - UM = -QMN + WMN

6. Consider the backward process N-M
    ♦ Let the heat absorbed by the gas during this process be QNM
    ♦
Let the work done by the gas during this process be WNM
• Then we get: UM = UN + QNM - WNM
⇒ UM - UN = QNM - WNM
7. Consider the results in (5) and (6)
• The left sides are numerically equal. Only difference is in the signs
8. Let us multiply both sides of (5) by '-1'
• We get: UM - UN = QMN - WMN
9. Now the left sides in (6) and (8) are the same
• So the right sides must be equal. We get:
QNM - WNM = QMN - WMN
⇒ WNM - WMN = QNM - QMN
Multiplying both sides by -1, we get:
WMN - WNM = QMN - QNM
10. Consider the left side of the result in (9):
    ♦ WMN is the work done on the gas when the piston moves down
    ♦
WNM is the work done by the gas when the piston moves up
• So (WMN - WNM) is the net work done on the gas
    ♦ We will denote this net work as W
    ♦ So we can write: W = WMN - WNM
11. Consider the right side of the result in (9):
    ♦ QMN is the heat released by the gas when the piston moves down
    ♦
QNM is the heat absorbed by the gas when the piston moves up
• So (QMN - QNM) is the net heat absorbed by the gas
12. From (9), we get Eq.12.11: W = QMN - QNM
• W is the net work done
• So it is clear that, the net work done is same as the net heat absorbed
 

Refrigerators

• We saw that, the gas receives a net work (W) and absorbs a net heat
• The 'net heat absorbtion' occurs when the piston completes one cycle
• If the cycle repeats continuously, we will get 'continuous absorbtion of heat'
• Such an arrangement which can produce 'continuous heat absorbtion' by receiving external work is called a refrigerator 

The main features of the refrigerator can be written in 6 steps:
1. In the refrigerator, all the molecules of the gas together form the ‘system’
2. We need to do work on this system. It can be done by compressing the gas using the piston
3. As a result of the work, the gas gives off heat (QMN) and becomes a liquid-vapour mixture
    ♦ Note that a suitable gas like freon must be used
    ♦ Such gases are called refrigerants
• QMN is given off into a hot reservoir which is kept at a temperature T1
(In practice, this hot reservoir is the 'space outside the refrigerator'. This space will be at room temperature)
4. When the downward motion of the piston is complete, ‘half of the first cycle’ is complete. We reach the point N
• Next we need to bring the piston to the original higher position M. Only then , can the gas be compressed in the next cycle
5. For that, the cylinder is placed in contact with the object to be cooled
• This object is called the 'cold reservoir'. It is at a temperature T2
• Heat QNM flows from this cold reservoir into the gas
• As a result, the gas expands and reaches the initial point M
• Now the piston is ready for the second cycle
(It is called the cold reservoir because, objects inside the refrigerator will be at a lower temperature. Even though the objects inside the refrigerator are cool, outside heat will penetrate through the walls of the refrigerator and try to warm the objects. We have to remove that heat which reaches the interior of the refrigerator)
6. The above steps can be schematically represented as shown in fig.12.18 below:

Schematic diagram of refrigerator or heat pump
Fig.12.18


 We see that:
    ♦ two items enter the system. They are: W and QNM
    ♦ one item leaves the system. It is: QMN
So QMN must be equal to (W + QNM)
Indeed, by rearranging Eq.12.11, we get: W + QNM = QMN
This implies that:
    ♦ The external work done (W)
    ♦ Plus
    ♦ The heat (QNM) removed from the 'object to be cooled'
    ♦ Gets dumped into the space surrounding the refrigerator
          ✰ When it is dumped, the system (gas) becomes ready for the next cycle

Coefficient of performance of a refrigerator

This can be explained in 3 steps:
1. If we can absorb 'more heat (QNM)' by doing a 'less net work (W)', we can say that, the coefficient of performance of the refrigerator is high
2. This coefficient is denoted using the symbol 𝛂
• Mathematically, we can write Eq.12.12: $\mathbf\small{\rm{\alpha=\frac{Q_{NM}}{W}}}$
• It is clear that, if QNM is high and W is low, 𝛂 will be high
3. Let us see the possible values of 𝛂:
It can be written in 4 steps:
(i) We have Eq.12.11: W = QMN - QNM
• This can be rearranged as: QNM = QMN - W
• So it is clear that W will be always less than QNM
• So $\mathbf\small{\rm{\frac{Q_{NM}}{W}}}$ will be always greater than 1
(ii) If the denominator W becomes smaller and smaller, the coefficient will become larger and larger
• If W becomes zero, the coefficient will become infinity. Such a refrigerator is not possible. We will see the reason in the next section
Since W cannot become zero, we can write:
It is impossible to remove heat from a body without doing external work W
(iii) We can derive another expression for 𝛂:
• Dividing both sides of Eq.12.11 by W, we get:
$\mathbf\small{\rm{1=\frac{Q_{MN}}{W}-\alpha}}$
⇒ $\mathbf\small{\rm{\alpha=\frac{Q_{MN}}{W}-1\;\;\;\;=\frac{Q_{MN}}{Q_{MN}-Q_{NM}}-1\;\;\;\;=\frac{Q_{MN}-Q_{MN}+Q_{NM}}{Q_{MN}-Q_{NM}}}}$
• Thus we get Eq.12.13: $\mathbf\small{\rm{\alpha=\frac{Q_{NM}}{Q_{MN}-Q_{NM}}}}$

Heat pump

Heat pumps are devices used to heat up the interior of a room when the surroundings of the room is cold
Heat pumps work in the same way as the refrigerators
A comparison can be written in 4 steps:
1. From where the heat is received:
In a refrigerator, system receives heat (QNM) from a cold body
    ♦ This cold body is the object to be cooled
In a heat pump also, the system receives heat (QNM) from a cold body
    ♦ This cold body is the surroundings of the room
2. Upon which the work is done:
In a refrigerator, external work (W) is done on the system
In a heat pump also, external work (W) is done on the system
3. To where the heat is dumped:
In a refrigerator, the ‘QNM + W’ is dumped into the surroundings of the refrigerator
In a heat pump, the ‘QNM + W’ is dumped into the interior of the room
4. Calculation of 𝛂:
In a refrigerator, the benefit that we receive, is the QNM removed from the body
    ♦ So we use the equation: $\mathbf\small{\rm{\alpha=\frac{Q_{NM}}{W}}}$
In a heat pump, the benefit that we receive, is the QMN available to heat the room
    ♦ So we use the equation: $\mathbf\small{\rm{\alpha=\frac{Q_{MN}}{W}}}$


In the next section, we will see the Carnot engine.

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