Showing posts with label specific heat capacity. Show all posts
Showing posts with label specific heat capacity. Show all posts

Monday, January 19, 2026

13.4 - Specific Heat Capacity of Solids

In the previous section, we saw specific heats of gases. In this section, we will see specific heat capacity of solids.

Details can be written in 4 steps:

1. For a solid atom, there will not be any translation or rotation. There will be vibration only.
• So by applying law of equipartition, We know that:
For each atom at temperature T, this energy will be $\small{K_B\,T}$
• Due to the vibration in all three dimensions, the average energy will be $\small{3K_B\,T}$.

2. In a mole of the solid, there will be $\small{N_A}$ atoms. So the total internal energy (U) of one mole of a solid can be obtained as:
$\small{U\,=\,3 K_B\,T\,N_A\,=\,3 R\,T}$

3. At constant pressure, we know that:
$\small{\Delta Q\,=\,\Delta U\,+\,P \Delta V}$ 
• For a solid, $\small{\Delta V}$ is negligible. So we get:
$\small{\Delta Q\,=\,\Delta U}$   

4. Specific heat is the change in internal energy per unit change in temperature. So we can obtain the specific heat for one mole as:
$\small{C\,=\,\frac{3 R\,T}{T}\,=\,3 R}$


Using the above equation, we can predict the specific heat of different solids. At ordinary temperature, the predicted values are in agreement with the experimental values. However, carbon is an exception. We will see the reason in higher classes.


Specific heat capacity of water

Details can be written in 4 steps:
1. We treat water like a solid. We saw that, for each solid atom, the energy is $\small{3K_B\,T}$. For each water molecule there are three atoms. So for a water molecule, the energy is $\small{9K_B\,T}$.

2. In a mole of the water, there will be $\small{N_A}$ molecules. So the total internal energy (U) of one mole of water can be obtained as:
$\small{U\,=\,9 K_B\,T\,N_A\,=\,9 R\,T}$

3. At constant pressure, we know that:
$\small{\Delta Q\,=\,\Delta U\,+\,P \Delta V}$ 
• Since we treat water as a solid, $\small{\Delta V}$ is negligible. So we get:
$\small{\Delta Q\,=\,\Delta U}$   

4. Specific heat is the change in internal energy per unit change in temperature. So we can obtain the specific heat for one mole as:
$\small{C\,=\,\frac{9 R\,T}{T}\,=\,9 R}$


Using the above equation, we can predict the specific heat of water. The predicted value is in agreement with the experimental value.

• If we use the use the unit “$\small{\text{calorie}\, \text{gram}^{-1} \,\text{K}^{-1} }$”, the specific heat of water is one.
• Let us convert the unit into “$\small{\text{J}\, \text{mol}^{-1} \,\text{K}^{-1} }$”
    ♦ One calorie is 4.179 joules
    ♦ One mole of water is 18 grams.
• So we get:
$\small{1~\text{calorie}\, \text{gram}^{-1} \,\text{K}^{-1}~=~\frac{1(4.179)}{(1/18)}~=~75.222~\text{joule}\, \text{mole}^{-1} \,\text{K}^{-1} }$
• Now, 9R = 9(8.31) = 74.79 $\small{\text{joule}\, \text{mole}^{-1} \,\text{K}^{-1} }$
• So the values are in agreement.


Next we will see an important aspect about the predicted values. It can be written in 4 steps:

1. We have seen the formulas for calculating the specific heats of various substances. In those formulas, temperature is absent. That means, the predicted values are calculated without taking temperature into account.

2. The experimental values have a marked difference from predicted values, when temperature is low. When experiments are done at temperatures close to zero, the specific heats also approach zero.
• This is because, when a substance freeze, the molecules/atoms in it have nearly zero degrees of freedom.

3. The kinetic theory is based on classical physics. For applying classical physics, the degrees of freedom must remain unchanged at all times.

4. However, quantum mechanics can make more accurate predictions. We will see those details in higher classes.


Mean free path

• Molecules in a gas are moving with large speeds. Speeds that are comparable to the speed of sound. But consider the case when cooking gas leaks from a faulty cylinder. The person at the other side of the room will become aware of the leakage, only after a short duration of time. That means, the molecules of the gas did not travel at the speed of sound, all the way to the other side of the room.
• Similar is the case of a cloud of smoke. The top of the cloud retains the shape for a considerable duration of time. If the molecules of the smoke travel at the speed of sound, in imaginary straight lines drawn in all directions, we will be seeing instant dispersal of the smoke.
• Scientists have discovered the reason for such behaviour. They found out that, the molecules of the gas/smoke undergo collisions. Due to the collisions, the molecules cannot move in straight lines. The direction changes continuously.

Let us try to make a mathematical model for the ‘possibility for collision’. It can be written in 12 steps:
1. Suppose that, the molecules of a gas are spheres of diameter d. Let us concentrate on one such sphere.
• It is the middle sphere in fig.13.3 (a) below. Let it be traveling with the average speed $\small{\bar{v}}$.

Fig.13.3

2. Consider any near by sphere. If the distance between the centers of the two spheres is less than or equal to ‘d’, then there is a possibility for collision.
• In the fig.13.3 above, the middle sphere can collide with any other sphere,
   ♦ whose edge is on the green dashed line   
   ♦ whose edge is between blue and green dashed lines   
   ♦ whose edge is on the red dashed line   
   ♦ whose edge is between blue and red dashed lines   

3. So we can think about a cylinder whose radius is ‘d’. This cylinder is shown in yellow color in the fig.13.3 above. Note that:
   ♦ Diameter of the spheres is ‘d’
   ♦ Radius of the cylinder is also ‘d’
         ✰ This is shown in the diagram shown in fig.13.3(b).
• Then base area of the cylinder will be: $\small{\pi d^2}$

4. Height of the cylinder is equal to the distance traveled by the middle sphere in time $\small{\Delta t}$, which is equal to $\small{\bar{v}\,\Delta t}$
• So volume of the cylinder will be $\small{\pi d^2\,\bar{v}\,\Delta t}$

5. All spheres whose center is on or within the edge of the cylinder, will have a possibility for collision with the middle sphere.

6. If n is the number of spheres per unit volume, then the number of spheres mentioned in (5) will be, n times the volume of the cylinder, which gives: $\small{n\pi d^2\,\bar{v}\,\Delta t}$
• That means, the number of collisions in the time duration of $\small{\Delta t}$ is $\small{n\pi d^2\,\bar{v}\,\Delta t}$

7. So the number of collisions in one second will be: $\small{\Delta t}$ is $\small{n\pi d^2\,\bar{v}}$

8. Let $\small{\tau}$ be the average time between two successive collisions. Then we can write:
$\small{\tau}$  × Number of collisions in one second = one second
Therefore, $\small{\tau~=~\frac{1}{n\pi d^2\,\bar{v}}}$

9. This average time, multiplied by the average speed will give the average distance between two successive collisions. 
• The average distance between two successive collisions is called mean free path ($\small{l}$).
• So we can write:
$\small{l\,=\,\tau\,\bar{v}\,=\,\frac{\bar{v}}{n\pi d^2\,\bar{v}}}$
$\small{\Rightarrow l\,=\,\frac{1}{n\pi d^2}}$  

10. Let us do a dimensional analysis of the equation derived in (9) above.
   ♦ The dimension of $\small{l}$ is $\small{L}$ 
   ♦ 'n' is number per volume. So it's dimensions are: $\small{L^{-3}}$
   ♦ The dimensions of $\small{d^2}$ is $\small{L^2}$ 
So the dimensions of R.H.S is: $\small{\frac{1}{L^{-3}L^2}~=~L}$

11. We derived the equation in (9) by considering the motion of the middle sphere in fig.13.3 above. We assumed that, all other spheres (molecules) are at rest. But in reality, all molecules are in motion.

• So instead of $\small{\bar{v}}$, we need to use $\small{\bar{v}_r}$, which is the average relative velocity.
• Based on this modification, scientists have derived a more accurate equation: $\small{l\,=\,\frac{1}{\sqrt{2}\,n\pi d^2}}$

12. Let us see an example:
We are given one mole of air molecules at STP. We want to find $\small{\tau}$ and the mean free path.
This can be done in steps:
(i) One mole of air molecules is $\small{6.02 ~\times~10^{23}}$ molecules. At STP, this number of molecules will occupy $\small{22.4~\times~10^{-3}~{\rm{m^3}}}$

(ii) So the number of molecules (n) in one cubic meter, can be calculated as:
$\small{n~=~\frac{6.02 ~\times~10^{23}}{22.4~\times~10^{-3}~{\rm{m^3}}}~=~2.7~\times~10^{25}~{\rm{m^{-3}}}}$

(iii) Let
   ♦ d, the diameter of an air molecule = $\small{2~\times~10^{-10}~{\rm{m}}}$
   ♦ $\small{\bar{v}}$, the average velocity of an air molecule = $\small{485~{\rm{m\,s^{-1}}}}$

(iv) Then from the equation in (8), we get:
$\small{\tau~=~\frac{1}{(2.7~\times~10^{25}~{\rm{m^{-3}}})\pi (2~\times~10^{-10}~{\rm{m}})^2\,(485~{\rm{m\,s^{-1}}} )}~=~6.1~\times~10^{-10}~{\rm{s}}}$

(v) Also, from the equation in (9), we get:
$\small{l\,=\,\tau\,\bar{v}\,=\,6.1~\times~10^{-10}~{\rm{s}}~\times~485~{\rm{m\,s^{-1}}}~=~2.9~\times~10^{-7}~{\rm{m}}}$

(vi) $\small{2.9~\times~10^{-7}~{\rm{m}}}$ is approximately equal to 1500d
• That means, the air molecule is able to travel 1500 times it's diameter between two successive collisions.


In the next chapter, we will see oscillations.

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Thursday, January 15, 2026

13.3 - Specific Heats of Gases

In the previous section, we saw the law of equipartition of energy. In this section, we will apply the law to predict the specific heats of gases.

First we will see monatomic gases. The details can be written in 5 steps:

1. For a monatomic gas molecule, there will not be any rotation or vibration. So we need to consider the translational kinetic energy only.
• Applying law of equipartition, We get:
For each molecule at temperature T, this energy will be $\small{\frac{3}{2}K_B\,T}$

2. In a mole of the gas, there will be $\small{N_A}$ molecules. So the total internal energy (U) of one mole of a monatomic gas can be obtained as:
$\small{U\,=\,\frac{3}{2}K_B\,T\,N_A\,=\,\frac{3}{2}R\,T}$  

3. Specific heat is the change in internal energy per unit change in temperature. So we can obtain the specific heat for one mole at constant volume as:
$\small{C_v\,\text{monatomic gas}\,=\,\frac{3}{2}R}$

4. For an ideal gas, $\small{C_p\,-\,C_v\,=\,R}$
Where $\small{C_p}$ is the specific heat for one mole at constant pressure. We can write:
$\small{C_p\,=\,R\,+\,C_v\,=\,\frac{5}{2}R}$

5. We can write the ratio of specific heats also:
$\small{\gamma\,=\,\frac{C_p}{C_v}\,=\,\frac{5}{3}}$


Next we will see diatomic gases whose molecules are rigid. The details can be written in 5 steps:

1. For a diatomic gas molecule, assuming that it is rigid, there will not be any vibration. So we need to consider the translational and rotational kinetic energies only.
• Applying law of equipartition, We get:
For each molecule at temperature T, this energy will be $\small{5\times \frac{1}{2}K_B\,T~=~\frac{5}{2}K_B\,T}$

2. In a mole of the gas, there will be $\small{N_A}$ molecules. So the total internal energy (U) of one mole of a diatomic gas can be obtained as:
$\small{U\,=\,\frac{5}{2}K_B\,T\,N_A\,=\,\frac{5}{2}R\,T}$  

3. Specific heat is the change in internal energy per unit change in temperature. So we can obtain the specific heat for one mole at constant volume as:
$\small{C_v\,\text{rigid diatomic gas}\,=\,\frac{5}{2}R}$

4. For an ideal gas, $\small{C_p\,-\,C_v\,=\,R}$
Where $\small{C_p}$ is the specific heat for one mole at constant pressure. We can write:
$\small{C_p\,=\,R\,+\,C_v\,=\,\frac{7}{2}R}$

5. We can write the ratio of specific heats also:
$\small{\gamma\,=\,\frac{C_p}{C_v}\,=\,\frac{7}{5}}$


Next we will see diatomic gases whose molecules are not rigid. The details can be written in 5 steps:

1. For a diatomic gas molecule, if it is not rigid, there will be vibration.
• Applying law of equipartition, We get:
For each molecule at temperature T, this energy will be $\small{5\times \frac{1}{2}K_B\,T\,+\,K_B\,T~=~\frac{7}{2}K_B\,T}$

2. In a mole of the gas, there will be $\small{N_A}$ molecules. So the total internal energy (U) of one mole of a diatomic gas can be obtained as:
$\small{U\,=\,\frac{7}{2}K_B\,T\,N_A\,=\,\frac{7}{2}R\,T}$  

3. Specific heat is the change in internal energy per unit change in temperature. So we can obtain the specific heat for one mole at constant volume as:
$\small{C_v\,\text{non-rigid diatomic gas}\,=\,\frac{7}{2}R}$

4. For an ideal gas, $\small{C_p\,-\,C_v\,=\,R}$
• We can write:
$\small{C_p\,=\,R\,+\,C_v\,=\,\frac{9}{2}R}$

5. We can write the ratio of specific heats also:
$\small{\gamma\,=\,\frac{C_p}{C_v}\,=\,\frac{9}{5}}$


Next we will see polyatomic gases. The details can be written in 5 steps:

1. In general, a polyatomic molecule has:
    ♦ 3 translational degrees of freedom
    ♦ 3 rotational degrees of freedom
    ♦ $\small{f}$ number of vibrational modes

• Applying law of equipartition, We get:
For each molecule at temperature T, this energy will be $\small{3\times \frac{1}{2}K_B\,T\,+\,3\times \frac{1}{2}K_B\,T\,+f\,\,K_B\,T~=~(3+f)K_B\,T}$

2. In a mole of the gas, there will be $\small{N_A}$ molecules. So the total internal energy (U) of one mole of a polyatomic gas can be obtained as:
$\small{U\,=\,(3+f)K_B\,T\,N_A\,=\,(3+f)R\,T}$  

3. Specific heat is the change in internal energy per unit change in temperature. So we can obtain the specific heat for one mole at constant volume as:
$\small{C_v\,\text{polyatomic gas}\,=\,(3+f)R}$

4. For an ideal gas, $\small{C_p\,-\,C_v\,=\,R}$
• We can write:
$\small{C_p\,=\,R\,+\,C_v\,=\,(4+f)R}$

5. We can write the ratio of specific heats also:
$\small{\gamma\,=\,\frac{C_p}{C_v}\,=\,\frac{4+f}{3+f}}$


Using the above equations, we can predict the specific heats of different types of gases. Two examples are given below. In those examples, vibrational modes are ignored:

Example 1:
• Predicted value of $\small{C_v}$ and $\small{C_p}$ for monatomic gas are 12.5 J mol−1 K−1 and 20.8 J mol−1 K−1 respectively.
• Experimental value of $\small{C_v}$ and $\small{C_p}$ for the monatomic gas helium are 12.5 J mol−1 K−1 and 20.8 J mol−1 K−1 respectively.

Example 2:
• Predicted value of $\small{C_v}$ and $\small{C_p}$ for diatomic gas are 20.8 J mol−1 K−1 and 29.1 J mol−1 K−1 respectively.
• Experimental value of $\small{C_v}$ and $\small{C_p}$ for the diatomic gas oxygen are 21.0 J mol−1 K−1 and 29.3 J mol−1 K−1 respectively.

If vibrational modes are included in the calculations, the predicted values become closer to the experimental values.

Now we will see some solved examples.

Solved example 13.14
A cylinder of fixed capacity 44.8 litres contains helium gas at standard temperature and pressure. What is the amount of heat needed to raise the temperature of the gas in the cylinder by 15.0 °C ? (R = 8.31 J mol−1 K−1)
Solution
:
1. Helium is a monatomic gas.
• So $\small{C_v\,=\,\frac{3}{2} R}$ and $\small{C_p\,=\,\frac{5}{2} R}$
• Given that, cylinder is of fixed capacity. That means, volume is constant. So we have to use $\small{C_v}$.

2. Heat required
= $\small{C_v~\times~\text{no. of moles}~\times~\text{rise in temperature}}$

3. So our next task is to find the number of moles of helium present in the cylinder.
• Given that, the gas is at STP. We know that, at STP, one mole of an ideal gas will have a volume of 22.4 litres.
• In our present case, the volume is 44.8 litres. So there are two moles.

4. Thus from (2), we get:
Heat required
= $\small{\frac{3}{2} R~\times~2~\times~15}$

= $\small{\frac{3}{2} \left(8.31 \text{J}\, \text{mol}^{-1} \,\text{K}^{-1} \right)~\times~2(\text{mol})~\times~15\left(\text{K} \right)}$

= $\small{373.95 \,\text{J}}$


In the next section, we will see specific heat capacity of solids.

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Sunday, November 29, 2020

Chapter 11.3 - Specific Heat Capacity

In the previous section we saw thermal stress. In this section we will see specific heat capacity

To learn the basics about specific heat capacity, we do three experiments. They can be explained in 18 steps:
1. A schematic representation of the first experiment is shown in fig.11.8 below:

Factors on which specific heat capacity depends
Fig.11.8

• Based on the first fig., we can write 3 steps:
(i) Heat m kg of water so that, it’s temperature rises by 20 oC
    ♦ Note down the time required for this 20 oC rise in temperature. Let it be t
(ii) Heat another m kg of water so that it’s temperature rises by 40 oC
    ♦ Use the same source of heat
    ♦ Note down the time required for this 40 oC rise in temperature
          ✰ This time will be about 2t
(iii) Remember that, we used the same source of heat
• So, since the time is doubled, we can write:
If Q units of heat energy is supplied in the first case, 2Q units of heat energy is supplied in the second case
■ It is clear that, the quantity of heat energy depends on the rise in temperature, ΔT
2. A schematic representation of the second experiment is also shown in fig.11.8 above
Based on the second fig., we can write 3 steps:
(i) Heat m kg of water so that, it’s temperature rises by 20 oC
    ♦ Note down the time required for this 20 oC rise in temperature. Let it be t
(ii) Heat 2m kg of water so that it’s temperature rises by 20 oC
    ♦ Use the same source of heat
    ♦ Note down the time required for this 20 oC rise in temperature
          ✰ This time will be about 2t
(iii) Remember that, we used the same source of heat
• So, since the time is doubled, we can write:
If Q units of heat energy is supplied in the first case, 2Q units of heat energy is supplied in the second case
■ It is clear that, the quantity of heat energy depends on the mass of the sample
3. A schematic representation of the third experiment is also shown in fig.11.8 above
• Based on the third fig., we can write 3 steps:
(i) Heat m kg of water so that, it’s temperature rises by 20 oC
    ♦ Note down the time required for this 20 oC rise in temperature. Let it be t
(ii) Heat m kg of oil so that it’s temperature rises by 20 oC
    ♦ Use the same source of heat
    ♦ Note down the time required for this 20 oC rise in temperature
          ✰ This time will be different from t
(iii) Remember that, we used the same source of heat
• So, since the time is different, we can write:
If Q units of heat energy is supplied in the first case, Q’ units of heat energy is supplied in the second case
■ It is clear that, the quantity of heat energy depends on the nature of the sample
4. So the ‘quantity of heat required’ to warm a substance depends on three items:
    ♦ Mass of the substance, m
    ♦ Change in temperature, ΔT
    ♦ Nature of the substance
5. To show the 'dependence on the three items mathematically', we introduce two quantities: Heat capacity and Specific heat capacity
6. Heat capacity can be described in 3 steps
(i) Q units of heat is supplied to a sample
(ii) The temperature of the sample increases by ΔT oC
(iii) So the heat required to increase the temperature by 1 oC will be equal to $\mathbf\small{\rm{\frac{Q}{\Delta T}}}$
• This heat is called heat capacity of the sample. It’s symbol is S
• So we get Eq.11.6: $\mathbf\small{\rm{S=\frac{Q}{\Delta T}}}$
7. Let us see the practical application of heat capacity. It can be written in 4 steps:
(i) We take various samples containing various substances
(ii) Heat each sample to increase the temperature by ΔT
• This ΔT need not be same for the samples
• If it is difficult to increase the temperature of a sample, a smaller ΔT can be adopted
(iii) Note down the Q required for achieving the ΔT for each sample
(iv) Then all we need to do is: Apply Eq.11.6 for each sample
• Thus we can obtain heat capacity (S value) of any sample
8. In calculating the S values in this way,
    ♦ we are not considering mass of substance
    ♦ we are not considering nature of substance
• Various samples will be having different S values
• The difference in S values may be due to either one or both of the two factors below:
    ♦ Difference in masses of the samples
    ♦ Difference in nature of the samples
9. So we need to be more accurate. For that, we introduce the quantity: Specific heat capacity
It can be explained in steps
(i) Q units of heat is supplied to a sample
(ii) The temperature of the sample increases by ΔT oC
(iii) So the heat required to increase the temperature by 1 oC will be equal to $\mathbf\small{\rm{\frac{Q}{\Delta T}}}$
(iv) So the heat required to increase the temperature of 1 kg of the substance by 1 oC will be equal to $\mathbf\small{\rm{\frac{Q}{m \Delta T}}}$
(m is the mass of the sample. It should be measured in kg) 
• This heat is called specific heat capacity of the sample. It’s symbol is s
• So we get Eq.11.7: $\mathbf\small{\rm{s=\frac{Q}{m \Delta T}}}$
10. Let us see the practical application of specific heat capacity. It can be written in 4 steps:
(i) We take various samples containing various substances
(ii) Heat each sample to increase the temperature by ΔT
• This ΔT need not be same for the samples
• If it is difficult to increase the temperature of a sample, a smaller ΔT can be adopted
(iii) Note down the Q required for achieving the ΔT for each sample
(iv) Then all we need to do is: Apply Eq.11.7 for each sample
• While reporting the results, write the name of the corresponding substances also
• By looking at such a report, a person can know this:
    ♦ Heat energy required
    ♦ to raise the temperature by 1 oC
    ♦ for 1 kg mass
    ♦ of a particular substance
• Thus, all required details are included
11. An important note can be written in 3 steps:
(i) In the above discussion, we did some experiments
    ♦ Each of those experiments start when we begin the supply of heat
    ♦ Each of those experiments end when we stop the supply of heat
(ii) It is compulsory that, from the start to the end, there must be no phase change
■ That means:
• If at the start, the sample is in solid state, the experiment should end before melting point is reached
• If at the start, the sample is in liquid state, the experiment should end before boiling point is reached
(iii) In later sections, we will see the reason for making this compulsory
12. Now we can write the definition of specific heat capacity of a substance
    ♦ It is the amount of heat absorbed or rejected
    ♦ by one kg of the substance
    ♦ while it’s temperature changes by 1 oC
    ♦ and not undergoing any phase change
13. Let us write the unit of s:
• From Eq.11.7, we have:
Unit of s = $\mathbf\small{\rm{\frac{(J)}{(kg)(K)}=J \,kg^{-1} \,K^{-1}}}$
14. We can derive another relation also:
• Dividing Eq.11.6 by 11.7, we get: $\mathbf\small{\rm{\frac{S}{s}= \frac{\frac{Q}{\Delta T}}{\frac{Q}{m \Delta T}}=m}}$
• Thus we get Eq.11.8: $\mathbf\small{\rm{s=\frac{S}{m}}}$
15. We have seen that, to find the specific heat capacity, we need to know the mass of the substance in the sample. Sometimes, instead of mass, we use ‘number of moles’, n
• In such cases, we divide $\mathbf\small{\rm{\frac{Q}{\Delta T}}}$ by n
(Recall that, earlier, we divided $\mathbf\small{\rm{\frac{Q}{\Delta T}}}$ by m)
• So instead of ‘per kg’, we get ‘per moles’
• The result is called molar specific heat capacity. It’s symbol is C
• So we can write Eq.11.9: $\mathbf\small{\rm{C=\frac{S}{n}=\frac{Q}{n \;\Delta T}}}$
16. Now we will see the C values of gases. The present step (16) and the next step (17) will help us to understand them
• To find the specific heat capacity, we heat the substance
• But if the substance is in the gaseous state, heating can be done in two ways:
(i) The gas is allowed to expand freely
    ♦ Then, the pressure experienced by the gas will be constant
    ♦ The volume will change
(ii) The gas is not allowed to expand freely. That is., volume is kept constant
    ♦ Then, the pressure experienced by the gas will change continuously
    ♦ Volume will remain constant
17. Two types of molar specific heat capacity for gases:
• If the experiment is done as in 16(i), the result is called molar specific heat capacity at constant pressure
    ♦ It’s symbol is Cp
• If the experiment is done as in 16(ii), the result is called molar specific heat capacity at constant volume
    ♦ It’s symbol is Cv
18. Comparison between various substances:
• We can obtain the specific heat capacity of various substances from the data book
    ♦ We see that, water has a very high specific heat capacity
• s for water is 4186 J kg-1 K-1
    ♦ This is much larger than that of iron or aluminum
          ✰ s of iron is 450 J kg-1 K-1
          ✰ s of aluminum is 900 J kg-1 K-1
■ Let us see two advantages of water having such a high specific heat capacity:
(i) Water can be used as a coolant in automobile radiators
• In the radiators, water absorb a large amount of heat. It’s temperature will rise only slowly. Because, 1 kg of water will need 4186 J of heat energy to increase temperature even by 1 oC
• So water will reach the boiling point only slowly
(ii) Water can be used as a heater in hot water bags
• This is because, water cools down only slowly
• 4186 J will have to be rejected to lower the temperature even by 1 oC

Solved example 11.10
400 J heat is given to 0.1 kg of a metal. Temperature of the metal increases by 20 oC. What is the specific heat capacity of the metal?
Solution:
1. 400 J of heat is required for a ΔT of 20 oC
• So, for a ΔT of 1 oC, (400⁄20) = 20 J will be required
2. 20 J is required for a ΔT of 1 oC for a mass of 0.1 kg
• So, for a mass of 1 kg, (20⁄0.1)= 200 J will be required
3. s of the metal is 200 J kg-1 K-1
4. Alternatively, we can use Eq.11.7: $\mathbf\small{\rm{s=\frac{Q}{m \Delta T}}}$
• Substituting the known values, we get: $\mathbf\small{\rm{s=\frac{(400)}{(0.1)(20)}}}$ = 200 J kg-1 K-1.  

Calorimetry

• The word calorimetry means: heat measurement
    ♦ Calorie means heat energy
    ♦ Metry means measurement
• The basics of calorimetry can be written in 6 steps
1. Fig.11.9(a) shows a 3D space. It is colored green
• It is not a plane surface. It is a 3D space. It can be a class room, a lab room, a stadium etc.,

Isolated system and Calorimetry
Fig.11.9

2. In this 3D space, we place a box made of insulating material
• This is denoted by the brown rectangle in fig.b
    ♦ Though it is shown as a rectangle, it is a 3D box
    ♦ The insulating material is present on all six sides
3. In fig.b, the green space can be considered as:
• The surroundings of the box
• Due to the presence of the insulating material on all the six sides,
    ♦ There is no passage of heat from the box into the green space (surroundings)
    ♦ There is no passage of heat from the surroundings into the box
4. Inside the box, there are only two items:
    ♦ A hot body shown in red color
    ♦ A cold body shown in white color
■ When the two bodies are brought into contact with each other, heat flows from the hot body to the cold body
■ That means:
    ♦ The hot body loses some heat
    ♦ The cold body gains some heat
5. Since there is no loss into the surroundings, we can write:
    ♦ Heat lost by the hot body
    ♦ is equal to
    ♦ Heat gained by the cold body
■ This is the principle of calorimetry
6. The hot body and the cold body are together known as a system
• We call it a ‘system’ because, there is more than one component
    ♦ The components work together to give the desired results
(For example, the computer system consists of four components: The monitor, CPU, keyboard and UPS. We get desired results only when the four components work together. If there is only one component, we need not call it a system. We can call it by it’s individual name)
• In our present case, the system consists of two components: The hot body and the cold body
■ Since there is no loss or gain of heat from the surroundings, we call it: an isolated system
• The ‘sides of the box’ forms the boundary of the system


• Next we will see the application of calorimetry
• Using calorimetry, we can determine unknown s values (specific heat capacity values) of various materials
• Before doing such calculations, we will first see how the arrangement shown in fig.11.9(b) can be achieved in practice. It can be written in 5 steps
1. The box shown in fig.11.9(b) is made of wood
    ♦ The inside of the box is covered with a layer of insulating material
    ♦ Usually glass wool is used as the insulating material
    ♦ Some images can be seen here
2. The cold body consists of three items:
    ♦ A metallic vessel
    ♦ A liquid (usually water) contained inside the metallic vessel
    ♦ A stirrer (made of the same metal as that of the vessel)
          ✰
When water is stirred, heat will be uniformly distributed in the system
3
. The hot body can be arranged by any one of the two methods given below:
(i) Heat a body outside the box, measure it’s temperature and quickly place it inside the water in the  metallic vessel
(ii) Place combustible material in a stainless steel chamber, place the chamber in the water in the metallic vessel and ignite using an electric fuse
4. A thermometer can be inserted through a hole in the wooden box
• In this way, the final temperature of the water can be measured
5. Thus the isolated system can be obtained in practice

■ Some solved examples will help us to get a good understanding about the procedure. Link to five such solved examples is given below:

Solved examples 11.11 to 11.16



In the next section, we will see Change of phase



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