JEE Physics Thermal Properties Of Matter MCQs Set 22

Multiple Choice Questions (MCQs) for JEE Physics: Thermal Properties Of Matter

Access targeted multiple-choice questions for Thermal Properties Of Matter designed to align with the latest JEE academic syllabus for JEE Physics. These objective practice sets help students evaluate their conceptual understanding and improve exam readiness.

Practice Thermal Properties Of Matter MCQs for JEE Physics

View or download the dedicated Thermal Properties Of Matter MCQ resource below. Practicing these 50 objective questions regularly builds familiarity with standard exam patterns and helps secure higher marks in final Physics evaluations.

Multiple Choice Questions

Question 1: A cylinder of radius R is surrounded by a cylindrical shell of inner radius R and outer radius 2R. The thermal conductivity of the material of the inner cylinder is \( K_1 \) and that of the outer cylinder is \( K_2 \). Assuming no loss of heat, the effective thermal conductivity of the system for heat flowing along the length of the cylinder is
(a) \( \dfrac{K_1+K_2}{2} \)
(b) \( \dfrac{2K_1+3K_2}{5} \)
(c) \( \dfrac{K_1+3K_2}{4} \)
(d) \( K_1+K_2 \)
Show Answer & Explanation

Answer: (c) \( \dfrac{K_1+3K_2}{4} \)

Explanation:
1. Heat flows along the length through the two parts in parallel, with areas \( \pi R^2 \) and \( \pi(4R^2-R^2)=3\pi R^2 \).
2. \( K_{eff}(4\pi R^2)=K_1\pi R^2+K_2(3\pi R^2)\Rightarrow K_{eff}=\dfrac{K_1+3K_2}{4} \).

Teacher's Note:
1. Identify the mode of heat transfer, then use the matching law: conduction \( Q/t = K A (T1-T2)/L \), radiation \( P = e \sigma A T^4 \), Newton cooling for small differences.
2. For rods in series the same heat current flows through each; for rods in parallel the temperature difference is common.

Question 2: A temperature difference of 120 \(^\circ\)C is maintained between the two ends of a uniform rod AB of length 2L. Another bent rod PQ, of the same cross-section as AB and of length \( \tfrac{3L}2 \), is connected across AB so that P and Q lie on AB with \( AP=QB=\tfrac L2 \) and \( PQ=L \) (the bent rod goes up \( \tfrac L4 \), across L and down \( \tfrac L4 \)). In steady state, the temperature difference between P and Q will be close to
(a) \( 35^\circ\text{C} \)
(b) \( 75^\circ\text{C} \)
(c) \( 60^\circ\text{C} \)
(d) \( 45^\circ\text{C} \)
Show Answer & Explanation

Answer: (d) \( 45^\circ\text{C} \)

Explanation:
1. Thermal resistances (proportional to length): AP \( =\tfrac L2 \), QB \( =\tfrac L2 \), and between \( P \) and \( Q \) the straight part \( (L) \) and the bent rod (\( \tfrac{3L}2 \)) in parallel: \( \dfrac{L\times1.5L}{2.5L}=0.6L \).
2. Total \( =1.6L \). The temperature difference across PQ \( =120\times\dfrac{0.6}{1.6}=45^\circ C \).

Teacher's Note:
1. Identify the mode of heat transfer, then use the matching law: conduction \( Q/t = K A (T1-T2)/L \), radiation \( P = e \sigma A T^4 \), Newton cooling for small differences.
2. For rods in series the same heat current flows through each; for rods in parallel the temperature difference is common.

Question 3: Three rods of copper, brass and steel are welded together to form a Y-shaped structure. The area of cross-section of each rod is 4 cm\(^2\). The end of the copper rod is maintained at 100 \(^\circ\)C whereas the ends of the brass and steel rods are kept at 0 \(^\circ\)C. The lengths of the copper, brass and steel rods are 46, 13 and 12 cm respectively. The rods are thermally insulated from surroundings except at the ends. Thermal conductivities of copper, brass and steel are 0.92, 0.26 and 0.12 in CGS units respectively. The rate of heat flow through the copper rod is
(a) 1.2 cal/s
(b) 4.8 cal/s
(c) 2.4 cal/s
(d) 6.0 cal/s
Show Answer & Explanation

Answer: (b) 4.8 cal/s

Explanation:
1. Values of \( K/L \): copper \( \dfrac{0.92}{46}=0.02 \), brass \( \dfrac{0.26}{13}=0.02 \), steel \( \dfrac{0.12}{12}=0.01 \). Let the junction be at \( T \): \( 0.02(100-T)=0.02T+0.01T\Rightarrow T=40^\circ C \).
2. Rate \( =KA\dfrac{\Delta T}{L}=4(0.02)(60)=4.8 \) cal/s.

Teacher's Note:
1. Identify the mode of heat transfer, then use the matching law: conduction \( Q/t = K A (T1-T2)/L \), radiation \( P = e \sigma A T^4 \), Newton cooling for small differences.
2. For rods in series the same heat current flows through each; for rods in parallel the temperature difference is common.

Question 4: If a piece of metal is heated to temperature \( \theta \) and then allowed to cool in a room which is at temperature \( \theta_0 \), the graph between the temperature T of the metal and time t will be
(a) a straight line falling uniformly to the absolute zero
(b) a straight line falling to \( \theta_0 \) and then staying constant
(c) a decreasing curve that is steepest at the start and flattens out, approaching \( \theta_0 \) asymptotically from above
(d) a curve that falls slowly at first and then more and more steeply below \( \theta_0 \)
Show Answer & Explanation

Answer: (c) a decreasing curve that is steepest at the start and flattens out, approaching \( \theta_0 \) asymptotically from above

Explanation:
1. Newton's law: \( \dfrac{dT}{dt}=-k(T-\theta_0) \), so \( T=\theta_0+(\theta-\theta_0)e^{-kt} \).
2. The rate of fall is largest when the excess temperature is largest and the curve tends to \( \theta_0 \) but never goes below it.

Teacher's Note:
1. Identify the mode of heat transfer, then use the matching law: conduction \( Q/t = K A (T1-T2)/L \), radiation \( P = e \sigma A T^4 \), Newton cooling for small differences.
2. For rods in series the same heat current flows through each; for rods in parallel the temperature difference is common.

Question 5: Three very large plates of same area are kept parallel and close to each other. They are considered as ideal black surfaces and have very high thermal conductivity. The first and third plates are maintained at temperatures 2T and 3T respectively. The temperature of the middle (i.e. second) plate under steady state condition is
(a) \( \left(\dfrac{97}{2}\right)^{1/4}T \)
(b) \( \left(\dfrac{65}{2}\right)^{1/4}T \)
(c) \( \left(\dfrac{97}{4}\right)^{1/4}T \)
(d) \( (97)^{1/4}T \)
Show Answer & Explanation

Answer: (a) \( \left(\dfrac{97}{2}\right)^{1/4}T \)

Explanation:
1. Steady state: energy absorbed by the middle plate equals energy emitted: \( \sigma(3T)^4-\sigma T_m^4=\sigma T_m^4-\sigma(2T)^4 \).
2. \( 2T_m^4=(81+16)T^4\Rightarrow T_m=\left(\dfrac{97}{2}\right)^{1/4}T \).

Teacher's Note:
1. Identify the mode of heat transfer, then use the matching law: conduction \( Q/t = K A (T1-T2)/L \), radiation \( P = e \sigma A T^4 \), Newton cooling for small differences.
2. For rods in series the same heat current flows through each; for rods in parallel the temperature difference is common.

Question 6: In which of the following processes does convection not take place primarily?
(a) Sea and land breeze
(b) Warming of glass of bulb due to filament
(c) Boiling of water
(d) Heating air around a furnace
Show Answer & Explanation

Answer: (b) Warming of glass of bulb due to filament

Explanation:
1. Convection needs a fluid moving in bulk because of density differences: sea and land breeze, boiling water and hot air near a furnace all involve this.
2. The glass of a bulb is mainly warmed by radiation (and conduction through the gas) from the filament, not by bulk fluid flow.

Teacher's Note:
1. Identify the mode of heat transfer, then use the matching law: conduction \( Q/t = K A (T1-T2)/L \), radiation \( P = e \sigma A T^4 \), Newton cooling for small differences.
2. For rods in series the same heat current flows through each; for rods in parallel the temperature difference is common.

Question 7: Three discs A, B and C having radii 2 m, 4 m and 6 m respectively are coated with carbon black on their outer surfaces. The wavelengths corresponding to maximum intensity are 300 nm, 400 nm and 500 nm, respectively. The powers radiated by them are \( Q_A \), \( Q_B \) and \( Q_C \) respectively. Then
(a) \( Q_A\text{ is maximum} \)
(b) \( Q_C\text{ is maximum} \)
(c) \( Q_B\text{ is maximum} \)
(d) \( Q_A=Q_B=Q_C \)
Show Answer & Explanation

Answer: (c) \( Q_B\text{ is maximum} \)

Explanation:
1. Wien's law: \( T\propto\dfrac1{\lambda_m} \), and power \( Q\propto r^2T^4\propto\dfrac{r^2}{\lambda_m^4} \).
2. In units of 100 nm: \( Q_A\propto\dfrac{4}{81}=0.049 \), \( Q_B\propto\dfrac{16}{256}=0.0625 \), \( Q_C\propto\dfrac{36}{625}=0.058 \). So \( Q_B \) is maximum.

Teacher's Note:
1. Identify the mode of heat transfer, then use the matching law: conduction \( Q/t = K A (T1-T2)/L \), radiation \( P = e \sigma A T^4 \), Newton cooling for small differences.
2. For rods in series the same heat current flows through each; for rods in parallel the temperature difference is common.

Question 8: Two bodies x and y of the same surface area cool by radiation, and x cools faster than y (its temperature falls faster). The correct relation between their emissivities E and absorptive powers a is
(a) \( E_x\gt E_y\ \text{and}\ a_x\gt a_y \)
(b) \( E_x\gt E_y\ \text{and}\ a_x\lt a_y \)
(c) \( E_x\lt E_y\ \text{and}\ a_x\gt a_y \)
(d) \( E_x\lt E_y\ \text{and}\ a_x\lt a_y \)
Show Answer & Explanation

Answer: (a) \( E_x\gt E_y\ \text{and}\ a_x\gt a_y \)

Explanation:
1. Faster cooling by radiation means a greater emissive power, so \( E_x\gt E_y \).
2. By Kirchhoff's law a good emitter is a good absorber (\( E/a \) is the same for all bodies at one temperature), so \( a_x\gt a_y \) as well.

Teacher's Note:
1. Identify the mode of heat transfer, then use the matching law: conduction \( Q/t = K A (T1-T2)/L \), radiation \( P = e \sigma A T^4 \), Newton cooling for small differences.
2. For rods in series the same heat current flows through each; for rods in parallel the temperature difference is common.

Question 9: An ideal black body at room temperature is thrown into a furnace. It is observed that
(a) initially it is the darkest body and at later times the brightest
(b) initially it is the darkest body and at later times it cannot be distinguished
(c) it is the darkest body at all times
(d) it cannot be distinguished at all times
Show Answer & Explanation

Answer: (b) initially it is the darkest body and at later times it cannot be distinguished

Explanation:
1. At room temperature a black body absorbs all light and emits little, so it looks darkest against the furnace walls.
2. Once in thermal equilibrium with the furnace it emits exactly what the walls emit, so it cannot be distinguished.

Teacher's Note:
1. Identify the mode of heat transfer, then use the matching law: conduction \( Q/t = K A (T1-T2)/L \), radiation \( P = e \sigma A T^4 \), Newton cooling for small differences.
2. For rods in series the same heat current flows through each; for rods in parallel the temperature difference is common.

Question 10: Three rods made of the same material and having the same cross-section have been joined at a junction. Each rod is of the same length. The left end is at 0 \(^\circ\)C and the other two ends (right) are at 90 \(^\circ\)C each. The temperature of the junction of the three rods will be
(a) \( 45^\circ\text{C} \)
(b) \( 30^\circ\text{C} \)
(c) \( 60^\circ\text{C} \)
(d) \( 20^\circ\text{C} \)
Show Answer & Explanation

Answer: (c) \( 60^\circ\text{C} \)

Explanation:
1. Heat entering the junction from the two hot rods equals heat leaving through the cold rod: \( 2(90-T)=T-0 \).
2. \( 180=3T\Rightarrow T=60^\circ C \).

Teacher's Note:
1. Identify the mode of heat transfer, then use the matching law: conduction \( Q/t = K A (T1-T2)/L \), radiation \( P = e \sigma A T^4 \), Newton cooling for small differences.
2. For rods in series the same heat current flows through each; for rods in parallel the temperature difference is common.

Question 11: A black body is at a temperature of 2880 K. The energy of radiation emitted by this body with wavelength between 499 nm and 500 nm is \( U_1 \), between 999 nm and 1000 nm is \( U_2 \) and between 1499 nm and 1500 nm is \( U_3 \). The Wien constant, \( b=2.88\times10^6 \) nm-K. Then
(a) \( U_2\gt U_1 \)
(b) \( U_1=0 \)
(c) \( U_3=0 \)
(d) \( U_1\gt U_2 \)
Show Answer & Explanation

Answer: (a) \( U_2\gt U_1 \)

Explanation:
1. \( \lambda_m=\dfrac bT=\dfrac{2.88\times10^6}{2880}=1000 \) nm, so the peak of the spectrum lies in the 999-1000 nm band.
2. A black body emits some energy at every wavelength, so \( U_1,U_3\neq0 \), and the band at the peak has the most energy: \( U_2\gt U_1 \).

Teacher's Note:
1. Identify the mode of heat transfer, then use the matching law: conduction \( Q/t = K A (T1-T2)/L \), radiation \( P = e \sigma A T^4 \), Newton cooling for small differences.
2. For rods in series the same heat current flows through each; for rods in parallel the temperature difference is common.

Question 12: A spherical black body with a radius of 12 cm radiates 450 W power at 500 K. If the radius were halved and the temperature doubled, the power radiated in watt would be
(a) 225
(b) 1800
(c) 450
(d) 900
Show Answer & Explanation

Answer: (b) 1800

Explanation:
1. \( P\propto r^2T^4 \).
2. New power \( =450\times\left(\dfrac12\right)^2\times2^4=450\times4=1800 W \).

Teacher's Note:
1. Identify the mode of heat transfer, then use the matching law: conduction \( Q/t = K A (T1-T2)/L \), radiation \( P = e \sigma A T^4 \), Newton cooling for small differences.
2. For rods in series the same heat current flows through each; for rods in parallel the temperature difference is common.

Question 13: Two metallic spheres \( S_1 \) and \( S_2 \) are made of the same material and have got identical surface finish. The mass of \( S_1 \) is thrice that of \( S_2 \). Both the spheres are heated to the same high temperature and placed in the same room having lower temperature but are thermally insulated from each other. The ratio of the initial rate of cooling of \( S_1 \) to that of \( S_2 \) is
(a) \( \dfrac13 \)
(b) \( \dfrac1{\sqrt3} \)
(c) \( \dfrac{\sqrt3}{1} \)
(d) \( \left(\dfrac13\right)^{1/3} \)
Show Answer & Explanation

Answer: (d) \( \left(\dfrac13\right)^{1/3} \)

Explanation:
1. Rate of cooling \( \propto\dfrac{\text{surface area}}{\text{mass}}\propto\dfrac{r^2}{r^3}=\dfrac1r \).
2. \( m_1=3m_2\Rightarrow r_1=3^{1/3}r_2 \), so the ratio is \( 3^{-1/3}=(1/3)^{1/3} \).

Teacher's Note:
1. Identify the mode of heat transfer, then use the matching law: conduction \( Q/t = K A (T1-T2)/L \), radiation \( P = e \sigma A T^4 \), Newton cooling for small differences.
2. For rods in series the same heat current flows through each; for rods in parallel the temperature difference is common.

Question 14: Three rods of identical cross-sectional area and made from the same metal form the sides of an isosceles triangle ABC, right angled at B. The points A and B are maintained at temperatures T and \( \sqrt2\,T \) respectively. In the steady state, the temperature of the point C is \( T_c \). Assuming that only heat conduction takes place, \( T_c/T \) is
(a) \( \dfrac{3}{\sqrt2+1} \)
(b) \( \dfrac{1}{2(\sqrt2-1)} \)
(c) \( \dfrac{1}{\sqrt3(\sqrt2-1)} \)
(d) \( \dfrac1{\sqrt2+1} \)
Show Answer & Explanation

Answer: (a) \( \dfrac{3}{\sqrt2+1} \)

Explanation:
1. Let \( AB=BC=l \), so \( AC=\sqrt2\,l \). Heat reaches \( C \) from \( B \) through BC and leaves \( C \) towards \( A \) through CA.
2. \( \dfrac{\sqrt2T-T_c}{l}=\dfrac{T_c-T}{\sqrt2\,l}\Rightarrow2T-\sqrt2T_c=T_c-T\Rightarrow\dfrac{T_c}{T}=\dfrac3{\sqrt2+1} \).

Teacher's Note:
1. Identify the mode of heat transfer, then use the matching law: conduction \( Q/t = K A (T1-T2)/L \), radiation \( P = e \sigma A T^4 \), Newton cooling for small differences.
2. For rods in series the same heat current flows through each; for rods in parallel the temperature difference is common.

Question 15: Two bodies A and B have thermal emissivities of 0.01 and 0.81 respectively. The outer surface areas of the two bodies are the same. The two bodies emit total radiant power at the same rate. The wavelength \( \lambda_B \) corresponding to maximum spectral radiancy in the radiation from B is shifted from the wavelength corresponding to maximum spectral radiancy in the radiation from A by 1.00 \( \mu \)m. If the temperature of A is 5802 K, which statements are correct? (a) The temperature of B is 1934 K. (b) \( \lambda_B=1.5\ \mu \)m. (c) The temperature of B is 11604 K. (d) The temperature of B is 2901 K.
(a) (c) only
(b) (a) and (b) only
(c) (a) and (d) only
(d) (b) and (c) only
Show Answer & Explanation

Answer: (b) (a) and (b) only

Explanation:
1. Equal power and equal area: \( 0.01T_A^4=0.81T_B^4\Rightarrow\left(\dfrac{T_A}{T_B}\right)^4=81\Rightarrow T_B=\dfrac{5802}{3}=1934 K \): \( (a) \) true.
2. \( \lambda_A=\dfrac{2.898\times10^{-3}}{5802}=0.5\ \mu m \) and \( \lambda_B=3\lambda_A=1.5\ \mu m, a \) shift of 1.0 \( \mu m \): \( (b) \) true. \( (c) \) and \( (d) \) are false.

Teacher's Note:
1. Identify the mode of heat transfer, then use the matching law: conduction \( Q/t = K A (T1-T2)/L \), radiation \( P = e \sigma A T^4 \), Newton cooling for small differences.
2. For rods in series the same heat current flows through each; for rods in parallel the temperature difference is common.

Question 16: Two spherical stars A and B emit black body radiation. The radius of A is 400 times that of B and A emits \( 10^4 \) times the power emitted from B. The ratio \( \lambda_A/\lambda_B \) of their wavelengths at which the peaks occur in their respective radiation curves is
(a) 1/2
(b) 4
(c) 8
(d) 2
Show Answer & Explanation

Answer: (d) 2

Explanation:
1. \( P\propto r^2T^4 \): \( 10^4=(400)^2\left(\dfrac{T_A}{T_B}\right)^4\Rightarrow\left(\dfrac{T_A}{T_B}\right)^4=\dfrac1{16}\Rightarrow\dfrac{T_A}{T_B}=\dfrac12 \).
2. Wien: \( \dfrac{\lambda_A}{\lambda_B}=\dfrac{T_B}{T_A}=2 \).

Teacher's Note:
1. Identify the mode of heat transfer, then use the matching law: conduction \( Q/t = K A (T1-T2)/L \), radiation \( P = e \sigma A T^4 \), Newton cooling for small differences.
2. For rods in series the same heat current flows through each; for rods in parallel the temperature difference is common.

Question 17: A metal is heated in a furnace where a sensor is kept above the metal surface to read the power radiated (P) by the metal. The sensor has a scale that displays \( \log_2(P/P_0) \), where \( P_0 \) is a constant. When the metal surface is at a temperature of 487 \(^\circ\)C, the sensor shows a value 1. Assume that the emissivity of the metallic surface remains constant. What is the value displayed by the sensor when the temperature of the metal surface is raised to 2767 \(^\circ\)C?
(a) 9
(b) 8
(c) 6
(d) 16
Show Answer & Explanation

Answer: (a) 9

Explanation:
1. At 487 \( ^\circ C =760 K \): \( \log_2(P/P_0)=1\Rightarrow P=2P_0 \).
2. 2767 \( ^\circ C =3040 K =4\times760 K \), so \( P\propto T^4 \) grows 256 times: \( P=512P_0 \) and \( \log_2512=9 \).

Teacher's Note:
1. Identify the mode of heat transfer, then use the matching law: conduction \( Q/t = K A (T1-T2)/L \), radiation \( P = e \sigma A T^4 \), Newton cooling for small differences.
2. For rods in series the same heat current flows through each; for rods in parallel the temperature difference is common.

Question 18: Two spherical bodies A (radius 6 cm) and B (radius 18 cm) are at temperatures \( T_1 \) and \( T_2 \), respectively. The maximum intensity in the emission spectrum of A is at 500 nm and in that of B is at 1500 nm. Considering them to be black bodies, what will be the ratio of the rate of total energy radiated by A to that of B?
(a) 3
(b) 9
(c) 27
(d) 81
Show Answer & Explanation

Answer: (b) 9

Explanation:
1. Wien: \( \dfrac{T_1}{T_2}=\dfrac{1500}{500}=3 \).
2. \( \dfrac{P_A}{P_B}=\left(\dfrac{r_A}{r_B}\right)^2\left(\dfrac{T_1}{T_2}\right)^4=\dfrac19\times81=9 \).

Teacher's Note:
1. Identify the mode of heat transfer, then use the matching law: conduction \( Q/t = K A (T1-T2)/L \), radiation \( P = e \sigma A T^4 \), Newton cooling for small differences.
2. For rods in series the same heat current flows through each; for rods in parallel the temperature difference is common.

Question 19: A point source of heat of power P is placed at the centre of a spherical shell of mean radius R. The material of the shell has thermal conductivity K. If the temperature difference between the outer and inner surface of the shell is not to exceed T, the thickness of the shell should not be less than
(a) \( \dfrac{4\pi RKT}{P} \)
(b) \( \dfrac{PR^2}{4\pi KT} \)
(c) \( \dfrac{P}{4\pi R^2KT} \)
(d) \( \dfrac{4\pi R^2KT}{P} \)
Show Answer & Explanation

Answer: (d) \( \dfrac{4\pi R^2KT}{P} \)

Explanation:
1. For a thin shell of thickness \( x \), \( P=KA\dfrac{T}{x} \) with \( A=4\pi R^2 \).
2. \( x=\dfrac{4\pi R^2KT}{P} \), so the thickness must be at least this much.

Teacher's Note:
1. Identify the mode of heat transfer, then use the matching law: conduction \( Q/t = K A (T1-T2)/L \), radiation \( P = e \sigma A T^4 \), Newton cooling for small differences.
2. For rods in series the same heat current flows through each; for rods in parallel the temperature difference is common.

Question 20: A solid copper sphere (density \( \rho \) and specific heat c) of radius r at an initial temperature of 200 K is suspended inside a chamber whose walls are at almost 0 K. Treating the sphere as a black body, the time required for the temperature of the sphere to drop to 100 K is
(a) \( \dfrac{7\rho cr}{72\sigma}\times10^{-6} \)
(b) \( \dfrac{7\rho cr}{9\sigma}\times10^{-6} \)
(c) \( \dfrac{7\rho cr}{72\sigma}\times10^{6} \)
(d) \( \dfrac{\rho cr}{3\sigma}\times10^{-6} \)
Show Answer & Explanation

Answer: (a) \( \dfrac{7\rho cr}{72\sigma}\times10^{-6} \)

Explanation:
1. \( \dfrac43\pi r^3\rho c\,dT=-\sigma(4\pi r^2)T^4dt\Rightarrow dt=-\dfrac{\rho cr}{3\sigma}\dfrac{dT}{T^4} \).
2. \( t=\dfrac{\rho cr}{3\sigma}\cdot\dfrac13\left[\dfrac1{100^3}-\dfrac1{200^3}\right]=\dfrac{\rho cr}{9\sigma}\cdot\dfrac78\times10^{-6}=\dfrac{7\rho cr}{72\sigma}\times10^{-6} \).

Teacher's Note:
1. Identify the mode of heat transfer, then use the matching law: conduction \( Q/t = K A (T1-T2)/L \), radiation \( P = e \sigma A T^4 \), Newton cooling for small differences.
2. For rods in series the same heat current flows through each; for rods in parallel the temperature difference is common.

Question 21: Two spheres of the same material have radii 1 m and 4 m, and temperatures 4000 K and 2000 K respectively. The ratio of the energy radiated per second by the first sphere to that by the second is
(a) 16 : 1
(b) 1 : 16
(c) 1 : 1
(d) 4 : 1
Show Answer & Explanation

Answer: (c) 1 : 1

Explanation:
1. \( P\propto r^2T^4 \).
2. \( \dfrac{P_1}{P_2}=\left(\dfrac14\right)^2(2)^4=\dfrac{16}{16}=1 \): the two spheres radiate equal energy per second.

Teacher's Note:
1. Identify the mode of heat transfer, then use the matching law: conduction \( Q/t = K A (T1-T2)/L \), radiation \( P = e \sigma A T^4 \), Newton cooling for small differences.
2. For rods in series the same heat current flows through each; for rods in parallel the temperature difference is common.

Question 22: A double-pane window used for insulating a room thermally from outside consists of two glass sheets each of area 1 m\(^2\) and thickness 0.01 m separated by a 0.05 m thick stagnant air space. In the steady state, the room glass interface and the glass-outdoor interface are at constant temperatures of 27 \(^\circ\)C and 0 \(^\circ\)C respectively. The rate of heat flow through the window pane is close to (thermal conductivities of glass and air are 0.8 and 0.08 W m\(^{-1}\)K\(^{-1}\) respectively)
(a) 27 W
(b) 83 W
(c) 10 W
(d) 41.5 W
Show Answer & Explanation

Answer: (d) 41.5 W

Explanation:
1. Series resistances: glass \( \dfrac{0.01}{0.8(1)}=0.0125 K/W \) each and air \( \dfrac{0.05}{0.08(1)}=0.625 K/W \).
2. Total \( R=0.65 K/W \), so \( H=\dfrac{27}{0.65}\approx41.5 W \).

Teacher's Note:
1. Identify the mode of heat transfer, then use the matching law: conduction \( Q/t = K A (T1-T2)/L \), radiation \( P = e \sigma A T^4 \), Newton cooling for small differences.
2. For rods in series the same heat current flows through each; for rods in parallel the temperature difference is common.

Question 23: For the double-pane window (two glass sheets each 0.01 m thick, a 0.05 m air gap between them, outer faces at 27 \(^\circ\)C indoors and 0 \(^\circ\)C outdoors, conductivities 0.8 and 0.08 W m\(^{-1}\)K\(^{-1}\), area 1 m\(^2\)), the temperature of the glass-air interface on the room side is close to
(a) \( 26.5^\circ\text{C} \)
(b) \( 13.5^\circ\text{C} \)
(c) \( 20^\circ\text{C} \)
(d) \( 1.0^\circ\text{C} \)
Show Answer & Explanation

Answer: (a) \( 26.5^\circ\text{C} \)

Explanation:
1. Heat current \( H=\dfrac{27}{0.65}=41.5 W \). Temperature drop across the first glass sheet \( =41.5\times0.0125=0.52^\circ C \).
2. So this interface is at \( 27-0.52\approx26.5^\circ C \) (and the air-glass interface on the outdoor side is at about 0.5 \( ^\circ C \)).

Teacher's Note:
1. Identify the mode of heat transfer, then use the matching law: conduction \( Q/t = K A (T1-T2)/L \), radiation \( P = e \sigma A T^4 \), Newton cooling for small differences.
2. For rods in series the same heat current flows through each; for rods in parallel the temperature difference is common.

Question 24: An electric heater is used in a room of total wall area 137 m\(^2\) to maintain a temperature of +20 \(^\circ\)C inside it, when the outside temperature is \(-10^\circ\)C. The walls have three different layers. The innermost layer is of wood of thickness 2.5 cm, the middle layer is of cement of thickness 1.0 cm and the outermost layer is of brick of thickness 25.0 cm. Assume that there is no heat loss through the floor and the ceiling. The thermal conductivities of wood, cement and brick are 0.125, 1.5 and 1.0 W/m\(^\circ\)C respectively. The power of the electric heater is
(a) 4.5 kW
(b) 18 kW
(c) 9 kW
(d) 3 kW
Show Answer & Explanation

Answer: (c) 9 kW

Explanation:
1. Resistance per unit area: \( \dfrac{0.025}{0.125}+\dfrac{0.01}{1.5}+\dfrac{0.25}{1.0}=0.2+0.0067+0.25=0.4567 m ^2 K/W \).
2. \( P=\dfrac{A\Delta T}{R}=\dfrac{137\times30}{0.4567}\approx9000 W \).

Teacher's Note:
1. Identify the mode of heat transfer, then use the matching law: conduction \( Q/t = K A (T1-T2)/L \), radiation \( P = e \sigma A T^4 \), Newton cooling for small differences.
2. For rods in series the same heat current flows through each; for rods in parallel the temperature difference is common.

Question 25: A solid sphere of copper of radius R and a hollow sphere of the same material of inner radius r and outer radius R are heated to the same temperature and allowed to cool in the same environment. Which of them starts cooling faster?
(a) The solid sphere
(b) Both cool at the same rate
(c) It depends on the room temperature only
(d) The hollow sphere
Show Answer & Explanation

Answer: (d) The hollow sphere

Explanation:
1. Rate of loss of heat \( =e\sigma A(T^4-T_0^4) \) is the same for both because the outer area is the same.
2. Rate of fall of temperature \( =\dfrac{\text{heat loss rate}}{mc} \); the hollow sphere has less mass, so it cools faster.

Teacher's Note:
1. Identify the mode of heat transfer, then use the matching law: conduction \( Q/t = K A (T1-T2)/L \), radiation \( P = e \sigma A T^4 \), Newton cooling for small differences.
2. For rods in series the same heat current flows through each; for rods in parallel the temperature difference is common.

Question 26: A room is maintained at 20 \(^\circ\)C by a heater of resistance 20 \(\Omega\) connected to 200 V mains. The temperature is uniform throughout the room and the heat is transmitted through a glass window of area 1 m\(^2\) and thickness 0.2 cm. The temperature outside is close to (thermal conductivity of glass = 0.2 cal m\(^{-1}\)s\(^{-1}\)(\(^\circ\)C)\(^{-1}\); mechanical equivalent of heat = 4.2 J cal\(^{-1}\))
(a) \( 15.2^\circ\text{C} \)
(b) \( 10.0^\circ\text{C} \)
(c) \( 4.8^\circ\text{C} \)
(d) \( 18.4^\circ\text{C} \)
Show Answer & Explanation

Answer: (a) \( 15.2^\circ\text{C} \)

Explanation:
1. Heater power \( P=\dfrac{V^2}{R}=\dfrac{200^2}{20}=2000 W \), all of which flows through the window. \( K=0.2\times4.2=0.84 W m ^{-1} K ^{-1} \).
2. \( \Delta T=\dfrac{PL}{KA}=\dfrac{2000\times0.002}{0.84\times1}=4.76^\circ C \), so the outside temperature \( =20-4.76\approx15.2^\circ C \).

Teacher's Note:
1. Identify the mode of heat transfer, then use the matching law: conduction \( Q/t = K A (T1-T2)/L \), radiation \( P = e \sigma A T^4 \), Newton cooling for small differences.
2. For rods in series the same heat current flows through each; for rods in parallel the temperature difference is common.

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