Multiple Choice Questions (MCQs) for JEE Physics: Thermodynamics
Review structured MCQ sets for JEE Physics Thermodynamics. Built according to official JEE guidelines, these downloadable questions support daily revision and core concept reinforcement.
Practice Thermodynamics MCQs for JEE Physics
Access the complete set of multiple-choice questions for Thermodynamics below. This focused format allows students to isolate specific topics for thorough review and uninterrupted practice alongside official JEE textbooks.
Multiple Choice Questions
Reason (R): In such a device no dissipation of energy takes place.
(a) Both Assertion and Reason are true and the Reason is a correct explanation of the Assertion.
(b) Both Assertion and Reason are true but the Reason is not a correct explanation of the Assertion.
(c) Assertion is true but the Reason is false.
(d) Both Assertion and Reason are false.
Show Answer & Explanation
Answer: (a) Both Assertion and Reason are true and the Reason is a correct explanation of the Assertion.
Explanation:
1. A reversible engine has no dissipative losses, so it gives the greatest possible efficiency between two given temperatures.
2. The Reason explains the Assertion.
Teacher's Note:
1. Dissipation (friction, heat leaks) lowers efficiency.
2. A reversible engine has none.
Reason (R): The initial and final temperatures are equal, therefore the change in internal energy is zero.
(a) Both Assertion and Reason are true and the Reason is a correct explanation of the Assertion.
(b) Both Assertion and Reason are true but the Reason is not a correct explanation of the Assertion.
(c) Assertion is true but the Reason is false.
(d) Both Assertion and Reason are false.
Show Answer & Explanation
Answer: (d) Both Assertion and Reason are false.
Explanation:
1. In a cyclic process \(\Delta U = 0\), so the Reason is true.
2. But the net work equals the net heat absorbed, which is not zero in general (it is the area of the loop): the Assertion is false.
Teacher's Note:
1. Net work in a cycle is the loop area.
2. Only the change in internal energy vanishes.
Reason (R): The efficiency of a Carnot engine is the ratio of net mechanical work done per cycle by the gas to the amount of heat energy absorbed per cycle from the source.
(a) Both Assertion and Reason are true and the Reason is a correct explanation of the Assertion.
(b) Both Assertion and Reason are true but the Reason is not a correct explanation of the Assertion.
(c) Assertion is true but the Reason is false.
(d) Both Assertion and Reason are false.
Show Answer & Explanation
Answer: (b) Both Assertion and Reason are true but the Reason is not a correct explanation of the Assertion.
Explanation:
1. \(\eta = 1 - \frac{T_2}{T_1}\) increases when \(T_2\) falls: the Assertion is true.
2. The Reason is the definition of efficiency and is true, but it does not by itself explain the temperature dependence.
Teacher's Note:
1. The definition does not mention temperature.
2. The temperature dependence comes from \(\eta = 1 - T_2/T_1\).
Reason (R): The Carnot cycle provides a way of determining the maximum possible efficiency achievable with reservoirs of given temperatures.
(a) Both Assertion and Reason are true and the Reason is a correct explanation of the Assertion.
(b) Both Assertion and Reason are true but the Reason is not a correct explanation of the Assertion.
(c) Assertion is true but the Reason is false.
(d) Both Assertion and Reason are false.
Show Answer & Explanation
Answer: (a) Both Assertion and Reason are true and the Reason is a correct explanation of the Assertion.
Explanation:
1. The Carnot efficiency is an upper limit that any engine can be compared with.
2. So the Reason explains the Assertion.
Teacher's Note:
1. Carnot efficiency is the benchmark.
2. Real engines are always below it.
(a) 13.2 J
(b) 15.4 J
(c) 12.6 J
(d) 16.8 J
Show Answer & Explanation
Answer: (b) 15.4 J
Explanation:
1. Adiabatic A to B: \(Q = 0\), work done on the system is 35 J, so \(\Delta U = +35\ \text{J}\).
2. Other path: \(Q = 12\times4.2 = 50.4\ \text{J}\).
3. \(W = Q - \Delta U = 50.4 - 35 = 15.4\ \text{J}\).
Teacher's Note:
1. Internal energy change is path independent.
2. Convert calories to joules before using the first law.
(a) 6400 J
(b) 5400 J
(c) 7900 J
(d) 8900 J
Show Answer & Explanation
Answer: (c) 7900 J
Explanation:
1. \(Q = 2000\times4.2 = 8400\ \text{J}\).
2. \(\Delta U = Q - W = 8400 - 500 = 7900\ \text{J}\).
Teacher's Note:
1. Work done by the system is subtracted from the heat absorbed.
2. Convert kcal to joules first.
(a) 567.2 K and \(6.3\times10^{6}\ \text{N/m}^2\)
(b) 675.2 K and \(3.6\times10^{6}\ \text{N/m}^2\)
(c) 275.2 K and \(2.3\times10^{6}\ \text{N/m}^2\)
(d) 465.6 K and \(4.2\times10^{6}\ \text{N/m}^2\)
Show Answer & Explanation
Answer: (b) 675.2 K and \(3.6\times10^{6}\ \text{N/m}^2\)
Explanation:
1. \(n = \frac{PV}{RT} = \frac{1.6\times10^6\times0.0083}{8.3\times300} = 5.33\ \text{mol}\).
2. Closed vessel means constant volume, \(C_V = C_P - R = \frac{3R}{2}\).
3. \(Q = nC_V\Delta T\) gives \(\Delta T = \frac{2.49\times10^4}{5.33\times1.5\times8.3} \approx 375\ \text{K}\), so \(T = 675\ \text{K}\).
4. \(P = 1.6\times10^6\times\frac{675}{300} = 3.6\times10^6\ \text{N/m}^2\).
Teacher's Note:
1. In a closed rigid vessel use \(C_V\), not \(C_P\).
2. Pressure scales with absolute temperature at constant volume.
(a) 2.08 kJ
(b) 3.08 kJ
(c) 4.08 kJ
(d) 5.08 kJ
Show Answer & Explanation
Answer: (a) 2.08 kJ
Explanation:
1. \(n = \frac{40}{28} = 1.43\ \text{mol}\).
2. Nitrogen is diatomic: \(C_P = \frac{7}{2}R\).
3. \(Q = nC_P\Delta T = 1.43\times3.5\times8.3\times50 \approx 2075\ \text{J} \approx 2.08\ \text{kJ}\).
Teacher's Note:
1. Use \(C_P\) for constant pressure heating.
2. Nitrogen is diatomic, so \(C_P = 7R/2\).
(a) 273 cal/K
(b) \(8\times10^{4}\) cal/K
(c) 80 cal/K
(d) 293 cal/K
Show Answer & Explanation
Answer: (d) 293 cal/K
Explanation:
1. \(Q = mL = 1000\times80 = 8\times10^4\ \text{cal}\).
2. \(\Delta S = \frac{Q}{T} = \frac{8\times10^4}{273} \approx 293\ \text{cal/K}\).
Teacher's Note:
1. Latent heat per gram must be multiplied by the mass in grams.
2. Use absolute temperature.
(a) 28 atm
(b) 68.7 atm
(c) 256 atm
(d) 8 atm
Show Answer & Explanation
Answer: (c) 256 atm
Explanation:
1. \(T_1 = 300\ \text{K}\), \(T_2 = 1200\ \text{K}\).
2. Adiabatic: \(P \propto T^{\gamma/(\gamma-1)} = T^{3.5}\).
3. \(P_2 = 2\times4^{3.5} = 2\times128 = 256\ \text{atm}\).
Teacher's Note:
1. Use the form of the adiabatic law that links \(P\) and \(T\).
2. \(\frac{\gamma}{\gamma-1} = 3.5\) for a diatomic gas.
(a) 18 C
(b) 668.4 K
(c) 395.4 C
(d) 144 C
Show Answer & Explanation
Answer: (b) 668.4 K
Explanation:
1. \(T_1 = 291\ \text{K}\), \(\gamma = 1.4\).
2. \(T_2 = T_1\left(\frac{V_1}{V_2}\right)^{\gamma-1} = 291\times8^{0.4} = 291\times2.297 \approx 668.4\ \text{K}\).
Teacher's Note:
1. Convert Celsius to kelvin before using the adiabatic law.
2. \(8^{0.4} = 2^{1.2}\).
(a) Final pressure will be three times less than the initial pressure
(b) Final pressure will be three times more than the initial pressure
(c) Change in pressure will be more than three times the initial pressure
(d) Change in pressure will be less than three times the initial pressure
Show Answer & Explanation
Answer: (c) Change in pressure will be more than three times the initial pressure
Explanation:
1. \(P_2 = P_1\left(\frac{V_1}{V_2}\right)^{\gamma} = 3^{\gamma}P_1\).
2. For \(\gamma \geq 1.4\), \(3^{\gamma} \geq 4.66\), so the change \(P_2 - P_1 = (3^\gamma - 1)P_1 > 3P_1\).
Teacher's Note:
1. In an adiabatic compression the pressure rises more than in an isothermal one.
2. Isothermal compression would give exactly three times.
(a) \(6.25\times10^{5}\ \text{J}\)
(b) \(3\times10^{5}\ \text{J}\)
(c) \(2.19\times10^{5}\ \text{J}\)
(d) \(4\times10^{4}\ \text{J}\)
Show Answer & Explanation
Answer: (a) \(6.25\times10^{5}\ \text{J}\)
Explanation:
1. Assume a Carnot engine: \(\eta = 1 - \frac{375}{500} = 0.25\).
2. \(W = \eta Q = 0.25\times25\times10^5 = 6.25\times10^5\ \text{J}\).
Teacher's Note:
1. Heat consumed is the heat absorbed from the source.
2. Work = efficiency times heat absorbed.
(a) \(\frac{100}{3}\ \text{J}\)
(b) 100 J
(c) \(\frac{200}{3}\ \text{J}\)
(d) 150 J
Show Answer & Explanation
Answer: (d) 150 J
Explanation:
1. \(\beta = \frac{Q_2}{W} = \frac{1}{3}\) gives \(Q_2 = \frac{W}{3}\).
2. Heat released is \(Q_1 = Q_2 + W = \frac{4W}{3} = 200\ \text{J}\).
3. So \(W = 150\ \text{J}\).
Teacher's Note:
1. Heat released to the hot reservoir includes the work supplied.
2. \(Q_1 = Q_2 + W\).
(a) 240 K
(b) 250 K
(c) 230 K
(d) 260 K
Show Answer & Explanation
Answer: (b) 250 K
Explanation:
1. \(\beta = \frac{T_2}{T_1 - T_2} = 5\) with \(T_1 = 300\ \text{K}\).
2. \(T_2 = 5(300 - T_2)\), so \(6T_2 = 1500\) and \(T_2 = 250\ \text{K}\).
Teacher's Note:
1. Take room temperature as the hot reservoir.
2. Solve the linear equation in \(T_2\).
(a) the temperature of the room will reduce a little
(b) the room can be cooled considerably but this will take a long time
(c) the room will get a little hotter
(d) None of these
Show Answer & Explanation
Answer: (c) the room will get a little hotter
Explanation:
1. The refrigerator rejects heat \(Q_1 = Q_2 + W\) to the room, which is more than the heat \(Q_2\) it removes from the room.
2. So the room gets a little hotter.
Teacher's Note:
1. The work supplied by the compressor ends up as heat in the room.
2. A refrigerator cannot cool a closed room.
(a) 64P
(b) 32P
(c) \(\frac{P}{64}\)
(d) 16P
Show Answer & Explanation
Answer: (c) \(\frac{P}{64}\)
Explanation:
1. Isothermal: \(P_1 = \frac{P}{2}\) at volume \(2V\).
2. Adiabatic from \(2V\) to \(16V\): ratio 8, so \(P_2 = \frac{P}{2}\times8^{-5/3} = \frac{P}{2}\times\frac{1}{32} = \frac{P}{64}\).
Teacher's Note:
1. Apply the isothermal law first and then the adiabatic law.
2. \(8^{5/3} = 2^5 = 32\).
(a) 1 J
(b) 2 J
(c) 3 J
(d) 4 J
Show Answer & Explanation
Answer: (c) 3 J
Explanation:
1. Stored energy is \(\frac{1}{2}kx^2 \propto x^2\).
2. At 1 mm: 1 J. At 2 mm: 4 J.
3. Additional work \(= 4 - 1 = 3\ \text{J}\).
Teacher's Note:
1. Energy grows with the square of the compression.
2. Subtract the energy already stored.
(a) 2 kJ
(b) 8 kJ
(c) 3.5 kJ
(d) 5.5 kJ
Show Answer & Explanation
Answer: (b) 8 kJ
Explanation:
1. \(Q = 2000\times4.2 = 8400\ \text{J}\).
2. \(\Delta U = Q - W = 8400 - 400 = 8000\ \text{J} = 8\ \text{kJ}\).
Teacher's Note:
1. Convert kcal to J before subtracting.
2. Work done by the system is subtracted.
(a) Kinetic energy of the box
(b) Translational kinetic energy of molecules of the gas
(c) Rotational kinetic energy of molecules of the gas
(d) Vibrational kinetic energy of the molecules of the gas
Show Answer & Explanation
Answer: (a) Kinetic energy of the box
Explanation:
1. Internal energy is the energy of the molecular motions and interactions in the frame of the gas.
2. The bulk kinetic energy of the moving box is mechanical energy and is not included.
Teacher's Note:
1. Internal energy is measured relative to the centre of mass.
2. Bulk motion is excluded.
(a) remains constant
(b) becomes 1
(c) decreases
(d) increases
Show Answer & Explanation
Answer: (d) increases
Explanation:
1. \(\eta = \frac{T_1 - T_2}{T_1}\).
2. After the change \(\eta' = \frac{T_1 - T_2}{T_1 - 100}\) has the same numerator and a smaller denominator.
3. So the efficiency increases.
Teacher's Note:
1. The difference stays the same while the source temperature falls.
2. Hence the ratio increases.
(a) 0.5
(b) 0.75
(c) 0.99
(d) 0.25
Show Answer & Explanation
Answer: (b) 0.75
Explanation:
1. \(TV^{\gamma-1}\) is constant with \(\gamma = 1.4\): \(\frac{T_2}{T_1} = \left(\frac{1}{32}\right)^{0.4} = 2^{-2} = \frac{1}{4}\).
2. Efficiency of the cycle \(\eta = 1 - \frac{T_2}{T_1} = 1 - \frac{1}{4} = 0.75\).
Teacher's Note:
1. \(32^{0.4} = 2^{2} = 4\).
2. Efficiency of an Otto-type cycle depends on the expansion ratio.
(a) 372 K and 330 K
(b) 330 K and 268 K
(c) 310 K and 248 K
(d) 372 K and 310 K
Show Answer & Explanation
Answer: (d) 372 K and 310 K
Explanation:
1. \(\frac{T_2}{T_1} = \frac{5}{6}\) and \(\frac{T_2 - 62}{T_1} = \frac{2}{3}\).
2. Subtracting: \(\frac{62}{T_1} = \frac{1}{6}\), so \(T_1 = 372\ \text{K}\).
3. \(T_2 = \frac{5}{6}\times372 = 310\ \text{K}\).
Teacher's Note:
1. Write both efficiencies as temperature ratios.
2. Subtract to eliminate \(T_2\).
(a) \(16.8\times10^{6}\ \text{J}\)
(b) \(4\times10^{6}\ \text{J}\)
(c) \(7.6\times10^{6}\ \text{J}\)
(d) \(4.2\times10^{6}\ \text{J}\)
Show Answer & Explanation
Answer: (a) \(16.8\times10^{6}\ \text{J}\)
Explanation:
1. \(\eta = 1 - \frac{300}{1200} = 0.75\).
2. \(Q_1 = \frac{W}{\eta} = \frac{12.6\times10^6}{0.75} = 16.8\times10^6\ \text{J}\).
Teacher's Note:
1. Efficiency links work output with heat absorbed.
2. Convert Celsius to kelvin.
(a) 200 K, 150 K
(b) 250 K, 200 K
(c) 300 K, 250 K
(d) 300 K, 200 K
Show Answer & Explanation
Answer: (b) 250 K, 200 K
Explanation:
1. \(T_2 = 0.8T_1\) and \(T_2 - 50 = 0.6T_1\).
2. Subtracting: \(50 = 0.2T_1\), so \(T_1 = 250\ \text{K}\).
3. \(T_2 = 200\ \text{K}\).
Teacher's Note:
1. Write efficiency as \(1 - T_2/T_1\) twice.
2. Subtract the two equations.
(a) \(\frac{1}{3}\)
(b) \(\frac{1}{4}\)
(c) \(\frac{2}{5}\)
(d) \(\frac{2}{3}\)
Show Answer & Explanation
Answer: (d) \(\frac{2}{3}\)
Explanation:
1. \(Q_1 = 3W\), so \(Q_2 = Q_1 - W = 2W\).
2. Fraction rejected \(= \frac{Q_2}{Q_1} = \frac{2}{3}\).
Teacher's Note:
1. Energy in equals work plus energy rejected.
2. The fraction is taken with respect to input.
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