Physics Objective Questions and Answers: Thermodynamics
Access targeted multiple-choice questions for Thermodynamics 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.
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Multiple Choice Questions
(a) Heat
(b) Work
(c) Internal energy
(d) All of these
Show Answer & Explanation
Answer: (c) Internal energy
Explanation:
1. A state variable depends only on the present state of the system, not on the path followed.
2. Heat and work are path dependent, whereas internal energy is fixed by the state.
3. So internal energy is the state variable.
Teacher's Note:
1. Heat and work are energy in transit, not properties stored in the system.
2. Internal energy, pressure, volume and temperature are state variables.
(a) temperature of the gas
(b) pressure of the gas
(c) atomicity of the gas
(d) number of moles of the gas
Show Answer & Explanation
Answer: (b) pressure of the gas
Explanation:
1. For an ideal gas \(U = \frac{f}{2}nRT\).
2. It depends on the number of moles, on the temperature and on the degrees of freedom (atomicity).
3. It does not depend on pressure separately.
Teacher's Note:
1. Ideal gas molecules have no intermolecular forces, so only kinetic energy counts.
2. Pressure matters only through the temperature it implies.
(a) in liquid state is equal to that in gaseous state
(b) in liquid state is less than that in gaseous state
(c) in liquid state is more than that in gaseous state
(d) is equal for the three states of matter
Show Answer & Explanation
Answer: (b) in liquid state is less than that in gaseous state
Explanation:
1. Converting a liquid to vapour at constant temperature needs latent heat.
2. This heat raises the potential energy of the molecules, so the vapour has more internal energy.
3. Hence the liquid has less internal energy than the gas.
Teacher's Note:
1. Latent heat changes internal energy without changing temperature.
2. Compare states at the same temperature using the latent heat absorbed.
(a) It is a restatement of the principle of conservation of energy
(b) It is applicable to cyclic processes
(c) It introduces the concept of entropy
(d) It introduces the concept of internal energy
Show Answer & Explanation
Answer: (c) It introduces the concept of entropy
Explanation:
1. The first law is energy conservation and defines internal energy.
2. It applies to every process including cyclic ones.
3. Entropy is introduced by the second law, so (c) is incorrect.
Teacher's Note:
1. First law: energy; zeroth law: temperature; second law: entropy.
2. Remember which law introduces which quantity.
(a) The change in entropy can never be zero
(b) Internal energy and entropy are state functions
(c) The internal energy changes in all processes
(d) The work done in an adiabatic process is always zero
Show Answer & Explanation
Answer: (b) Internal energy and entropy are state functions
Explanation:
1. Entropy change is zero in a reversible adiabatic process, so (a) is false.
2. Internal energy does not change in an isothermal process of an ideal gas, so (c) is false.
3. Adiabatic work equals the fall in internal energy, so (d) is false.
4. Both internal energy and entropy depend only on the state, so (b) is correct.
Teacher's Note:
1. A state function depends only on the initial and final states.
2. Test each option with one counter-example.
(a) \(C = \frac{3R}{T}\)
(b) \(C = 3R\)
(c) \(C = \frac{1}{3}RT\)
(d) \(C = \frac{1}{3}R\)
Show Answer & Explanation
Answer: (b) \(C = 3R\)
Explanation:
1. Each atom in a solid vibrates in three dimensions, giving \(6\) quadratic terms.
2. Energy per mole is \(U = 3RT\).
3. So \(C = \frac{dU}{dT} = 3R\) (law of Dulong and Petit).
Teacher's Note:
1. This law holds at ordinary and high temperatures.
2. It is independent of the temperature.
(a) \(PV = \text{constant}\)
(b) \(PV^{-\gamma} = \text{constant}\)
(c) \(PV^{\gamma} = \text{constant}\)
(d) \(\frac{P}{V^{\gamma}} = \text{constant}\)
Show Answer & Explanation
Answer: (c) \(PV^{\gamma} = \text{constant}\)
Explanation:
1. For a reversible adiabatic change of an ideal gas \(dQ = 0\).
2. Combining this with \(PV = nRT\) and \(C_P/C_V = \gamma\) gives \(PV^{\gamma} = \text{constant}\).
Teacher's Note:
1. \(PV = \text{constant}\) is for the isothermal case.
2. The adiabatic curve is steeper because of the factor \(\gamma\).
(a) \(C_V = \frac{R}{\gamma - 1}\)
(b) \(C_P = \frac{\gamma R}{\gamma - 1}\)
(c) \(C_P / C_V = \gamma\)
(d) \(C_P - C_V = 2R\)
Show Answer & Explanation
Answer: (d) \(C_P - C_V = 2R\)
Explanation:
1. Mayer's relation is \(C_P - C_V = R\) for one mole.
2. Using \(\gamma = C_P/C_V\) gives \(C_V = \frac{R}{\gamma-1}\) and \(C_P = \frac{\gamma R}{\gamma-1}\).
3. So (d) is wrong.
Teacher's Note:
1. Mayer's relation has no factor of 2.
2. Derive \(C_V\) and \(C_P\) from Mayer's relation and \(\gamma\) to check any variant.
(a) negative
(b) zero
(c) between zero and one
(d) more than one
Show Answer & Explanation
Answer: (d) more than one
Explanation:
1. \(C_P = C_V + R\) with \(R > 0\), so \(C_P > C_V\).
2. Therefore \(\gamma = C_P/C_V > 1\).
Teacher's Note:
1. At constant pressure the gas also does expansion work, so it needs more heat.
2. That is why \(C_P\) exceeds \(C_V\).
(a) Adiabatic compression
(b) Adiabatic expansion
(c) Isothermal compression
(d) Isothermal expansion
Show Answer & Explanation
Answer: (a) Adiabatic compression
Explanation:
1. With no heat exchange, \(\Delta U = -W_{by}\).
2. In adiabatic compression work is done on the gas, so \(\Delta U > 0\) and the temperature rises.
Teacher's Note:
1. Compressing a gas quickly heats it, as in a bicycle pump.
2. Isothermal changes keep the temperature fixed.
(a) infinite
(b) zero
(c) negative
(d) remains constant
Show Answer & Explanation
Answer: (a) infinite
Explanation:
1. Specific heat is \(c = \frac{Q}{m\,\Delta T}\).
2. In an isothermal process heat is absorbed while \(\Delta T = 0\), so \(c \to \infty\).
Teacher's Note:
1. Adiabatic process has \(Q = 0\), so specific heat is zero.
2. Isothermal has \(\Delta T = 0\), so specific heat is infinite.
(a) change in volume
(b) change in temperature
(c) change in pressure
(d) None of these
Show Answer & Explanation
Answer: (b) change in temperature
Explanation:
1. In an adiabatic change \(W_{by} = -\Delta U = -nC_V\Delta T\).
2. So the work depends only on the change in temperature (for a given amount of gas).
Teacher's Note:
1. Use the first law with \(Q = 0\).
2. Work depends on the temperature change only.
(a) Melting of ice
(b) Bursting of a tyre
(c) Motion of the piston of an engine at constant speed
(d) None of these
Show Answer & Explanation
Answer: (b) Bursting of a tyre
Explanation:
1. A tyre bursts so rapidly that the escaping air has no time to exchange heat.
2. So it is an adiabatic process.
3. Melting of ice needs heat from outside.
Teacher's Note:
1. Fast processes are nearly adiabatic.
2. Very slow processes in conducting walls are nearly isothermal.
(a) \(P^{\gamma}V = \text{constant}\)
(b) \(T^{\gamma}V = \text{constant}\)
(c) \(TV^{\gamma-1} = \text{constant}\)
(d) \(TV^{\gamma} = \text{constant}\)
Show Answer & Explanation
Answer: (c) \(TV^{\gamma-1} = \text{constant}\)
Explanation:
1. Put \(P = \frac{nRT}{V}\) in \(PV^{\gamma} = \text{constant}\).
2. This gives \(TV^{\gamma-1} = \text{constant}\).
Teacher's Note:
1. There are three equivalent forms: in \(P,V\), in \(T,V\) and in \(P,T\).
2. Remember \(\gamma - 1\) goes with \(TV\).
(a) \(\Delta U = -W\) in an adiabatic process
(b) \(\Delta U = W\) in an isothermal process
(c) \(\Delta U = -W\) in an isothermal process
(d) \(\Delta U = W\) in an adiabatic process
Show Answer & Explanation
Answer: (a) \(\Delta U = -W\) in an adiabatic process
Explanation:
1. First law: \(Q = \Delta U + W\).
2. In an adiabatic process \(Q = 0\), so \(\Delta U = -W\).
3. For an ideal gas isothermal process \(\Delta U = 0\), so (b) and (c) fail.
Teacher's Note:
1. Write the first law with the sign convention given in the question.
2. Then set \(Q = 0\) for adiabatic changes.
(a) isothermal slope = adiabatic slope
(b) isothermal slope = \(\gamma \times\) adiabatic slope
(c) adiabatic slope = \(\gamma \times\) isothermal slope
(d) adiabatic slope = \(\frac{1}{2} \times\) isothermal slope
Show Answer & Explanation
Answer: (c) adiabatic slope = \(\gamma \times\) isothermal slope
Explanation:
1. Isothermal: \(PV = c\), so \(\frac{dP}{dV} = -\frac{P}{V}\).
2. Adiabatic: \(PV^{\gamma} = c\), so \(\frac{dP}{dV} = -\gamma\frac{P}{V}\).
3. So the adiabatic slope is \(\gamma\) times the isothermal slope.
Teacher's Note:
1. Since \(\gamma > 1\), the adiabatic curve is steeper.
2. Differentiate both laws at the same point.
(a) isothermal
(b) isobaric
(c) adiabatic
(d) equal in all cases
Show Answer & Explanation
Answer: (b) isobaric
Explanation:
1. Work is the area under the P-V curve.
2. Starting at the same point, the isobaric line stays highest, the isothermal curve falls, and the adiabatic curve falls fastest.
3. So the isobaric expansion does the most work.
Teacher's Note:
1. Compare areas under the three curves from the same starting point.
2. The adiabatic expansion does least work.
(a) \(\frac{V}{T} = \text{constant}\)
(b) \(W = P\Delta V\)
(c) Heat given to a system is used up in raising the temperature only
(d) \(\Delta Q > W\)
Show Answer & Explanation
Answer: (c) Heat given to a system is used up in raising the temperature only
Explanation:
1. At constant pressure \(V/T\) is constant and \(W = P\Delta V\).
2. Heat supplied is shared between increasing internal energy and doing work, so \(\Delta Q > W\).
3. So (c) is incorrect.
Teacher's Note:
1. In an isobaric expansion some heat becomes work.
2. That is why \(C_P > C_V\).
(a) In an isochoric process pressure remains constant
(b) In an isothermal process the temperature remains constant
(c) In an adiabatic process \(PV^{\gamma} = \text{constant}\)
(d) In an adiabatic process the system is insulated from the surroundings
Show Answer & Explanation
Answer: (a) In an isochoric process pressure remains constant
Explanation:
1. In an isochoric process the volume stays constant, not the pressure.
2. The other three statements are correct.
Teacher's Note:
1. Iso-choric means same volume; iso-baric means same pressure.
2. Learn the prefixes.
(a) For an adiabatic process \(\Delta E_{int} = -W\)
(b) For a constant volume process \(\Delta E_{int} = +Q\)
(c) For a cyclic process \(\Delta E_{int} = 0\)
(d) For free expansion of a gas \(\Delta E_{int} > 0\)
Show Answer & Explanation
Answer: (d) For free expansion of a gas \(\Delta E_{int} > 0\)
Explanation:
1. In free expansion \(Q = 0\) and \(W = 0\), so \(\Delta E_{int} = 0\).
2. Hence (d) is wrong.
3. Statements (a), (b) and (c) follow from the first law.
Teacher's Note:
1. Free expansion of an ideal gas keeps the temperature constant.
2. Use the first law for each option.
(a) isothermal
(b) isochoric
(c) adiabatic
(d) isobaric
Show Answer & Explanation
Answer: (c) adiabatic
Explanation:
1. The definition of an adiabatic process is \(Q = 0\).
Teacher's Note:
1. Adiabatic means no heat exchange.
2. It does not mean the temperature is constant.
(a) \(\frac{\theta_2}{\theta_1 - \theta_2}\)
(b) \(\frac{\theta_1}{\theta_1 - \theta_2}\)
(c) \(\frac{\theta_1 - \theta_2}{\theta_2}\)
(d) \(\frac{\theta_1 - \theta_2}{\theta_1}\)
Show Answer & Explanation
Answer: (a) \(\frac{\theta_2}{\theta_1 - \theta_2}\)
Explanation:
1. Coefficient of performance is \(\beta = \frac{Q_2}{W} = \frac{Q_2}{Q_1 - Q_2}\).
2. For a reversible refrigerator \(\frac{Q_2}{Q_1} = \frac{\theta_2}{\theta_1}\), giving \(\beta = \frac{\theta_2}{\theta_1 - \theta_2}\).
Teacher's Note:
1. The numerator is the heat removed from the cold space.
2. The denominator is the work supplied.
(a) The whole of the heat can be converted into mechanical energy in a cycle
(b) No heat engine can be 100% efficient
(c) Every heat engine has an efficiency of 100%
(d) A refrigerator can reduce the temperature to absolute zero
Show Answer & Explanation
Answer: (b) No heat engine can be 100% efficient
Explanation:
1. Kelvin-Planck statement: no cyclic engine can convert all absorbed heat into work.
2. So no heat engine can be 100% efficient.
Teacher's Note:
1. Some heat must always be rejected to a colder sink.
2. Absolute zero cannot be reached by finite steps.
(a) \(\Delta Q = \Delta U\)
(b) \(\Delta U = \Delta W\)
(c) \(\Delta W = 0\)
(d) \(\Delta U = 0\)
Show Answer & Explanation
Answer: (d) \(\Delta U = 0\)
Explanation:
1. After a complete cycle the system returns to its initial state, so \(\Delta U = 0\).
2. Then \(\Delta Q = \Delta W\), which is not zero in general.
Teacher's Note:
1. Internal energy is a state function.
2. Net work in a cycle equals net heat absorbed.
(a) \(\eta = 1 + \frac{\theta_2}{\theta_1}\)
(b) \(\eta = 1 + \frac{\theta_1}{\theta_2}\)
(c) \(\eta = 1 - \frac{\theta_1}{\theta_2}\)
(d) \(\eta = 1 - \frac{\theta_2}{\theta_1}\)
Show Answer & Explanation
Answer: (d) \(\eta = 1 - \frac{\theta_2}{\theta_1}\)
Explanation:
1. Efficiency is \(\eta = \frac{W}{Q_{in}} = \frac{Q_{in} - Q_{out}}{Q_{in}} = 1 - \frac{\theta_2}{\theta_1}\).
Teacher's Note:
1. Efficiency is always less than one.
2. Options with a plus sign would exceed one.
(a) \(\frac{\theta_1}{\theta_2} = \frac{T_2}{T_1}\)
(b) \(\frac{\theta_1}{\theta_2} = \frac{T_1}{T_2}\)
(c) \(\frac{\theta_1}{\theta_2} = \frac{P_1}{P_2}\)
(d) all of these
Show Answer & Explanation
Answer: (b) \(\frac{\theta_1}{\theta_2} = \frac{T_1}{T_2}\)
Explanation:
1. For a Carnot cycle \(\frac{Q_1}{Q_2} = \frac{T_1}{T_2}\), where \(Q\) is heat and \(T\) the absolute temperature of the reservoir.
2. The other relations do not hold.
Teacher's Note:
1. Heats exchanged are proportional to the temperatures of the reservoirs.
2. Use absolute temperature.
(a) \(T_1\) and \(T_2\) are both high
(b) \(T_1\) and \(T_2\) are both low
(c) \(T_1\) is low and \(T_2\) is high
(d) \(T_1\) is high and \(T_2\) is low
Show Answer & Explanation
Answer: (d) \(T_1\) is high and \(T_2\) is low
Explanation:
1. \(\eta = 1 - \frac{T_2}{T_1}\) is largest when \(\frac{T_2}{T_1}\) is smallest.
2. That needs a high \(T_1\) and a low \(T_2\).
Teacher's Note:
1. A large temperature difference helps.
2. The ratio matters, not the difference alone.
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