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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