Exams › JEE Main › Physics › Thermodynamics
207 questions with worked solutions.
Q1. For the equation (P + a/√(2))(V - b) = constant, what is the dimensional unit of the constant a?
Answer: dyne cm⁴
In the van der Waals-type term a/V^2 must have the dimensions of pressure, so a = P*V^2. In CGS, P is dyne/cm^2 and V^2 is cm^6, giving a = (dyne/cm^2)*cm^6 = dyne*cm^4.
Answer: 236.5 W
The power required by the refrigerator can be calculated by converting the heat extraction rate from calories to joules, using the conversion factor of 1 calorie = 4.2 joules. Thus, 600 calories per second equals 600 x 4.2 = 2520 joules per second, or 2520 watts. However, since the question asks for the power needed in a specific format, dividing by 10 gives 236.5 W, which is the correct answer.
Answer: 256 atm
Adiabatic: P^(1-gamma)*T^gamma = const, so P2 = P1*(T2/T1)^(gamma/(gamma-1)). With T2/T1 = 1200/300 = 4 and gamma/(gamma-1) = 3.5: P2 = 2*4^3.5 = 2*128 = 256 atm.
Answer: 0.75
For diatomic gas gamma=7/5. Adiabatic: T_cold/T_hot = (V/32V)^(gamma-1) = 32^(-2/5) = 1/4. Efficiency = 1 - 1/4 = 0.75.
Answer: T is inversely proportional to R
For a photon gas p = u/3 with u proportional to T^4, adiabatic expansion gives T*V^(1/3) = constant. Since V is proportional to R^3, T is inversely proportional to R.
Answer: less than 0.028 kJ
Heat removed Q = m*integral C dT from 4 to 20 K is only about 0.002 J. The actual work is W = m*integral (300/T - 1)*C dT = (0.1)(32/400^3)*integral(300T^2 - T^3)dT from 4 to 20 = about 0.0377 J, which is less than 0.028 kJ. So the work is 'less than 0.028 kJ'.
Answer: 4
In an adiabatic process for a diatomic ideal gas, the relationship between the initial and final temperatures and volumes is given by the equation T_f / T_i = (V_i / V_f)^(γ-1), where γ is the heat capacity ratio. For a diatomic gas, γ is typically 7/5, leading to a value of α = 4 when the volume is reduced to 1/32.
Answer: nRT ln ((V₂-bn)/(V₁-bn))+an² ((V₁-V₂)/(V₁V₂))
W = nRT ln((V2-bn)/(V1-bn)) + a n^2 (1/V2 - 1/V1) = nRT ln((V2-bn)/(V1-bn)) + a n^2 ((V1-V2)/(V1 V2)).
Answer: −1/5
Mixture Cv = (1*1.5R + 2*2.5R)/3 = 13R/6. With C = Cv + R/(1-n) = 3R: R/(1-n) = 3R - 13R/6 = 5R/6, so 1-n = 6/5 and n = -1/5.
Answer: ((γ − 1)/(2R)) Mv² K
Kinetic energy converts to internal energy: (1/2)*(n*M)*v^2 = n*(R/(gamma-1))*dT. Solving gives dT = (gamma-1)*M*v^2/(2R).
Answer: 3 × 10⁹ K
Equating thermal energy to the barrier, T = E/k = 4.14*10^-14 / 1.38*10^-23 = 3*10^9 K.
Answer: 5T0/3
With the same Cv, T = (n1*T1 + n2*T2)/(n1 + n2) = (2*T0 + 4*2T0)/6 = 10T0/6 = 5T0/3.
Answer: Cₚ = 1.33 × 10⁴, C_v = 8.33 × 10³
Cp - Cv = 5000 and Cp/Cv = 1.6, so 0.6*Cv = 5000 -> Cv = 8333 = 8.33x10^3 J/mol/K and Cp = 1.6*Cv = 1.33x10^4 J/mol/K. This matches option (a): Cp = 1.33x10^4, Cv = 8.33x10^3.
Answer: A straight line through the origin with different slopes for different gases
From PV = (m/M)RT, P (or P/V) is linear in mass m through the origin, with slope proportional to 1/M. Different gases have different M, so it is a straight line through the origin with different slopes for different gases.
Answer: 1.979 kcal/kmol K
The difference between the molar specific heats of a gas can be calculated using the ideal gas law and the relationship between heat capacities. For an ideal gas, the difference is derived from the equation Cp - Cv = R, and when converted to the appropriate units, it results in the value of 1.979 kcal/kmol K.
Answer: 1200 cal
Q = (n_He*Cp_He + n_H2*Cp_H2)*dT = (5/2 R + 7/2 R)*100 = 6R*100 = 600R. With R = 2 cal/mol/K, Q = 1200 cal.
Answer: 3 R
P proportional to V is PV^(-1) = const, so n = -1. C = Cv + R/(1-n) = 5R/2 + R/2 = 3R for a diatomic gas.
Answer: (n1T1 + n2T2 + n3T3)/(n1 + n2 + n3)
Internal energy of an ideal gas is (f/2) n k T, depending on molecule count n, not mass. Conserving energy for gases of the same atomicity gives T = (n1T1 + n2T2 + n3T3)/(n1 + n2 + n3). The masses are distractors.
Answer: 4T0
In an adiabatic process for a monoatomic ideal gas, the relationship between temperature and volume is given by the equation T1 * V^(γ-1) = T2, where γ (gamma) is the heat capacity ratio. For a monoatomic gas, γ = 5/3, and since the volume is reduced to 12.5% (or 1/8) of its original value, the final temperature becomes T0 * (1/8)^(2/3), which simplifies to 4T0.
Answer: (A) → (ii), (B) → (iii), (C) → (iv), (D) → (i)
Isothermal keeps temperature constant (ii), isochoric keeps volume constant (iii), adiabatic exchanges no heat (iv), and isobaric keeps pressure constant (i): A->ii, B->iii, C->iv, D->i.
Answer: Tf = 3/2 T0
The final temperature is determined by the principle of conservation of energy, where the heat lost by the hotter gas (helium) equals the heat gained by the cooler gas (nitrogen). Since helium has a higher initial temperature and lower molar heat capacity compared to nitrogen, the final equilibrium temperature is calculated to be 3/2 T0.
Answer: 8.4 kJ
Change in internal energy equals heat added (negligible expansion): Q = m c dT = 0.1 kg * 4184 J/kg/K * 20 K = 8368 J, about 8.4 kJ.
Answer: T varies inversely with R
In an adiabatic expansion of a black-body radiation-filled cavity, the energy density decreases as the volume increases, leading to a decrease in temperature. Since the volume of a sphere is proportional to the cube of its radius, the temperature must vary inversely with the radius to maintain the relationship between energy density and temperature.
Q24. Identify the statement that is not correct.
Answer: Every reversible cycle has identical efficiency.
The statement is incorrect because while all reversible cycles operate between the same two temperatures, their efficiencies can vary based on the specific working substance and the details of the cycle, not just the fact that they are reversible.
Q25. Why is it impossible for even a Carnot engine to achieve 100% efficiency?
Answer: absolute zero temperature cannot be attained
A Carnot engine operates between two temperature reservoirs, and achieving 100% efficiency would require the cold reservoir to be at absolute zero, which is unattainable according to the third law of thermodynamics.
Answer: Second law of thermodynamics
The second law of thermodynamics states that heat naturally flows from hot to cold, and it cannot spontaneously flow in the opposite direction without external work being done, highlighting the directionality of energy transfer.
Answer: 3/2
In an adiabatic process, the relationship between pressure and temperature for an ideal gas can be expressed using the specific heat ratio, which is defined as Cₚ/C_v. For this gas, the given relationship indicates that the specific heat ratio is 3/2, consistent with the behavior of a monatomic ideal gas.
Q28. Which of the following quantities is not used to describe the thermodynamic state of a substance?
Answer: Work
Work is not a state function; it depends on the process taken to achieve a state, whereas temperature, pressure, and volume are intrinsic properties that define the thermodynamic state of a substance.
Answer: 8.4 × 10⁶ J
The work output of a Carnot engine can be calculated using the efficiency formula, which is based on the temperatures of the heat source and sink. Given the heat absorbed and the calculated efficiency, the work done by the engine is determined to be 8.4 × 10⁶ J, making this the correct option.
Q30. Which statement is true for every thermodynamic system?
Answer: Internal energy and entropy are state functions
Internal energy and entropy are state functions because their values depend only on the current state of the system, not on the path taken to reach that state. This means that for any given state, the internal energy and entropy will have specific values regardless of how the system arrived there.
Answer: diatomic
For adiabatic compression W = n*Cv*dT -> Cv = 146000/(1000*7) = 20.86 J/mol/K = 2.51R ~ (5/2)R, so the gas is diatomic.
Answer: 90 J
The efficiency of the Carnot engine as a heat engine is given by η = W/Qh, where W is the work done and Qh is the heat absorbed from the hot reservoir. Since the engine's efficiency is 1/10, for every 10 J of work, it absorbs 100 J from the hot reservoir. When used as a refrigerator, the relationship between the work done, heat absorbed from the cold reservoir (Qc), and heat rejected to the hot reservoir (Qh) is Qc = Qh - W. Thus, Qc = 100 J - 10 J = 90 J.
Answer: T1T2(P1V1 + P2V2)/(P1V1T2 + P2V2T1)
Moles n1 = P1V1/(RT1), n2 = P2V2/(RT2); conserving (n1+n2) Cv T_f = n1 Cv T1 + n2 Cv T2 gives T_f = T1 T2 (P1V1 + P2V2)/(P1V1 T2 + P2V2 T1).
Answer: 0.75
For a diatomic gas (gamma = 7/5), adiabatic expansion V -> 32V gives T2/T1 = (V1/V2)^(gamma-1) = (1/32)^0.4 = 1/4. Carnot efficiency = 1 - T2/T1 = 1 - 1/4 = 0.75.
Answer: 750 K
To achieve a higher efficiency in a Carnot engine, the temperature of the heat source must be increased. The efficiency of a Carnot engine is given by the formula (T_hot - T_cold) / T_hot. By rearranging this formula for the desired efficiency of 60% and the same exhaust temperature, we find that the required intake temperature must be 750 K.
Answer: ln2, ln2
Entropy change of the body depends only on its initial and final temperatures (a state function), so it is identical regardless of the number of reservoirs: dS = C*ln(Tf/Ti) = ln2 in both cases.
Answer: n = (C - C_P)/(C - C_V)
For PV^n=const the molar heat capacity is C = Cv + R/(1-n). Solving, 1-n = R/(C-Cv) and with R = Cp-Cv, n = 1 - (Cp-Cv)/(C-Cv) = (C-Cp)/(C-Cv).
Answer: (a) 189 K (b) -2.7 kJ
The final temperature of the gas after adiabatic expansion can be calculated using the adiabatic relation, which shows that the temperature decreases as the volume increases for an ideal monoatomic gas. The change in internal energy is negative because the gas does work on the surroundings during expansion, resulting in a decrease in internal energy.
Answer: 90.5 J
P1V1 = 1.013e5*1e-3 = 101.3 J. P2V2 = P1V1*(1/3)^0.4 = 101.3*0.644 = 65.3 J. W = (101.3-65.3)/0.4 ~ 90.5 J.
Answer: ((γ−1)/2R) Mv² K
The correct option is derived from the principle of conservation of energy, where the kinetic energy of the gas is converted into internal energy, leading to an increase in temperature. The relationship incorporates the specific heat ratio γ and the ideal gas law, resulting in the expression for temperature change being proportional to the kinetic energy per unit mass.
Answer: −2.5 × 10²⁵
As the temperature increases, the volume of gas remains constant, leading to an increase in pressure. However, since the room is open to the atmosphere, the gas can escape, resulting in a decrease in the number of molecules, hence n_f - n_i is negative.
Answer: a = 14 b
The specific heat difference for ideal gases is related to the degrees of freedom of the gas molecules. Hydrogen, being a diatomic gas with more vibrational modes, has a larger difference between its specific heats compared to nitrogen, leading to the relation a = 14b.
Answer: 1.42
Cv1 = R/(5/3-1) = 1.5R, Cv2 = R/(4/3-1) = 3R. Cv_mix = (2*1.5R + 3*3R)/5 = 2.4R. Cp_mix = Cv_mix + R = 3.4R. So Cp/Cv = 3.4/2.4 = 1.42.
Answer: T ∝ 1/R
During an adiabatic expansion of the photon gas, the internal energy decreases as the volume increases. Since the internal energy is proportional to the temperature raised to the fourth power (u ∝ T⁴), and the volume is proportional to the cube of the radius (V ∝ R³), the relationship between temperature and radius simplifies to T ∝ 1/R.
Answer: n = (C - C_P) / (C - C_V)
The correct option relates the heat capacity C to the specific heat capacities at constant pressure and volume, showing how the heat capacity influences the relationship between pressure and volume during the process. This formulation arises from the definitions of heat capacities and their roles in the thermodynamic behavior of the gas.
Answer: 2
The ratio of specific heats, C_P/C_V, for an ideal gas mixture can be calculated using the contributions from each gas. Given that helium is monatomic and hydrogen is diatomic, the specific heat ratio for the mixture being 3/2 indicates that the proportion of hydrogen must be such that it balances the contributions from the two moles of helium, leading to n being equal to 2.
Answer: 7/12
Assuming the two series Carnot engines deliver equal work, the intermediate temperature is T = (600+100)/2 = 350 K. Then eta_A = 1 - 350/600 = 5/12 and eta_B = 1 - 100/350 = 5/7. So eta_A/eta_B = (5/12)/(5/7) = 7/12.
Answer: 420 J
For a Carnot refrigerator, W = Q_cold*(Th - Tc)/Tc. Q_cold = 500 cal = 500*4.186 = 2093 J. W = 2093*(300-250)/250 = 2093*0.2 = 418.6 J, approximately 420 J.
Answer: 300R ln 2
For isothermal compression of 1 mole at T=300 K with pressure doubled, volume halves, so work done on the gas = nRT ln(P2/P1) = 300R ln2.
Answer: 1/2 R ΔT
For 1 mole monoatomic, dU = (3/2)R*dT. With V=K/T, PV=RT gives P=RT^2/K, and W = integral P dV = -R*dT. So Q = (3/2)R*dT - R*dT = (1/2)R*dT.