Heat and Thermodynamics

JEE Physics · 315 questions · Page 28 of 32 · Click an option or "Show Solution" to reveal answer

Q271
An ideal gas goes from an initial state to final state. During the process, the pressure of gas increases linearly with temperature. A. The work done by gas during the process is zero. B. The heat added to gas is different from change in its internal energy. C. The volume of the gas is increased. D. The internal energy of the gas is increased. E. The process is isochoric (constant volume process) Choose the correct answer from the options given below:
A A, C Only
B A, D, E Only
C E Only
D A, B, C, D Only
Correct Answer
Option B
Solution

For an ideal gas, the equation of state is given by

pV=nRT.pV = nRT.

If during a process the pressure increases linearly with temperature (i.e.,

pTp \propto T

), then from the ideal gas law (with a fixed amount of gas,

nn

, and with the gas constant,

RR

), it follows that

pT=nRV.\frac{p}{T} = \frac{nR}{V}.

Since

nRnR

is constant, a linear relationship between

pp

and

TT

implies that

pT\frac{p}{T}

remains constant throughout the process. This can only be true if the volume

VV

is constant.

Hence, the process is isochoric.

For an isochoric (constant volume) process: The work done by the gas is given by

W=pdV,W = \int p\, dV,

and since

dV=0dV = 0

, we have

W=0.W = 0.

(Statement A is true.) The internal energy change for an ideal gas depends only on temperature:

ΔU=nCVΔT.\Delta U = nC_V\Delta T.

If the temperature increases, then

ΔU>0.\Delta U > 0.

(Statement D is true.)

For an isochoric process, no expansion work is done, so any heat added goes entirely into increasing the internal energy.

This means the heat added is not different from the change in internal energy (in fact,

Q=ΔUQ = \Delta U

).

(Statement B is false.)

Since the process is isochoric, the volume does not change (and certainly is not increased).

(Statement C is false, and Statement E stating it is isochoric is true.)

Thus, the correct true statements are A, D, and E.

Q272
The temperature of a body in air falls from 40C40^{\circ} \mathrm{C} to 24C24^{\circ} \mathrm{C} in 4 minutes. The temperature of the air is 16C16^{\circ} \mathrm{C}. The temperature of the body in the next 4 minutes will be :
A 283C\dfrac{28}{3}{ }^{\circ} \mathrm{C}
B 563C\dfrac{56}{3}{ }^{\circ} \mathrm{C}
C 423C\dfrac{42}{3}{ }^{\circ} \mathrm{C}
D 143C\dfrac{14}{3}{ }^{\circ} \mathrm{C}
Correct Answer
Option B
Solution
T2T1t=K[ Tavg Ts]T1=24C;T2=40C,t=4, Ts=16C40244=K[3216]K=416=14 Now 24T4=K[ T+24216]24T=T162+163 T2=28 T=563C\begin{aligned} & \frac{\mathrm{T}_2-\mathrm{T}_1}{\mathrm{t}}=\mathrm{K}\left[\mathrm{~T}_{\text{avg }}-\mathrm{T}_{\mathrm{s}}\right] \\ & \mathrm{T}_1=24^{\circ} \mathrm{C} ; \mathrm{T}_2=40^{\circ} \mathrm{C}, \mathrm{t}=4, \mathrm{~T}_{\mathrm{s}}=16^{\circ} \mathrm{C} \\ & \frac{40-24}{4}=\mathrm{K}[32-16] \\ & \mathrm{K}=\frac{4}{16}=\frac{1}{4} \\ & \text{ Now } \frac{24-\mathrm{T}}{4}=\mathrm{K}\left[\frac{\mathrm{~T}+24}{2}-16\right] \\ & 24-\mathrm{T}=\frac{\mathrm{T}-16}{2}+16 \\ & \frac{3 \mathrm{~T}}{2}=28 \\ & \mathrm{~T}=\frac{56}{3} \mathrm{C} \end{aligned}
Q273
Given below are two statements. One is labelled as Assertion (A) and the other is labelled as Reason (R). Assertion (A) : In an insulated container, a gas is adiabatically shrunk to half of its initial volume. The temperature of the gas decreases. Reason (R) : Free expansion of an ideal gas is an irreversible and an adiabatic process. In the light of the above statements, choose the correct answer from the options given below :
A Both (A)(\mathbf{A}) and (R)(\mathbf{R}) are true and (R)(\mathbf{R}) is the correct explanation of (A)(\mathbf{A})
B Both (A) and (R) are true but (R) is NOT the correct explanation of (A)
C (A) is false but (R) is true
D (A) is true but (R)(\mathbf{R}) is false
Correct Answer
Option C
Solution

Let's analyze both statements step by step.

Assertion (A): "In an insulated container, a gas is adiabatically shrunk to half of its initial volume.

The temperature of the gas decreases."

• In an adiabatic process, no heat is exchanged with the surroundings.

• For a reversible adiabatic (compression) process, the relationship between temperature and volume is given by

TVγ1=constant,T V^{\gamma-1} = \text{constant},

where γ\gamma is the heat capacity ratio (greater than 1). • If the volume is reduced from

VV

to

V/2V/2

, then

Tfinal=Tinitial(VV/2)γ1=Tinitial(2)γ1.T_{\text{final}} = T_{\text{initial}} \left(\frac{V}{V/2}\right)^{\gamma-1} = T_{\text{initial}}\,(2)^{\gamma-1}.

• Since

(2)γ1>1,(2)^{\gamma-1} > 1,

the final temperature is higher than the initial temperature.

• Therefore, the assertion that the temperature decreases is incorrect.

Reason (R): "Free expansion of an ideal gas is an irreversible and an adiabatic process."

• In a free expansion, the gas expands into a vacuum without doing any work on the surroundings.

• Since the container is insulated, no heat is exchanged, making it adiabatic.

• However, the process is inherently irreversible due to the spontaneous expansion and mixing of states.

• Thus, this statement is true.

Since Assertion (A) is false and Reason (R) is true (but the reason does not explain the false assertion about temperature change during compression), the correct answer is: Option C (A) is false but (R) is true.

Q274
A monoatomic gas having γ=53 \gamma = \dfrac{5}{3} is stored in a thermally insulated container and the gas is suddenly compressed to (18)th \left( \dfrac{1}{8} \right)^{\text{th}} of its initial volume. The ratio of final pressure and initial pressure is: (γ\gamma is the ratio of specific heats of the gas at constant pressure and at constant volume)
A 16
B 32
C 28
D 40
Correct Answer
Option B
Solution

To find the ratio of final pressure (Pf P_f ) to initial pressure (Pi P_i ), we use the adiabatic condition: PiViγ=PfVfγ P_i V_i^\gamma = P_f V_f^\gamma We aim to express the pressure ratio: PfPi=(ViVf)γ \dfrac{P_f}{P_i} = \left(\dfrac{V_i}{V_f}\right)^\gamma Given that the final volume Vf V_f is 18 \dfrac{1}{8} of the initial volume Vi V_i , this simplifies to: (ViVf)=8 \left(\dfrac{V_i}{V_f}\right) = 8 Thus, the pressure ratio becomes: PfPi=853 \dfrac{P_f}{P_i} = 8^\dfrac{5}{3} Calculating 853 8^\dfrac{5}{3} gives: PfPi=32 \dfrac{P_f}{P_i} = 32

Q275
Water falls from a height of 200 m into a pool. Calculate the rise in temperature of the water assuming no heat dissipation from the water in the pool.(Take g = 10 m/s2, specific heat of water = 4200 J/(kg K))
A 0.36 K
B 0.23 K
C 0.48 K
D 0.14 K
Correct Answer
Option C
Solution

To find the rise in temperature of the water as it falls from a height, we start by equating the potential energy loss to the heat gained, assuming no heat is lost from the water in the pool.

The potential energy lost by the water can be expressed as: mgh mgh where: m m is the mass of water, g g is the acceleration due to gravity (10 m/s²), h h is the height (200 m).

The heat gained by the water when temperature changes is given by: msΔT ms \Delta T where: s s is the specific heat capacity of water (4200 J/(kg K)), ΔT \Delta T is the change in temperature.

Setting the potential energy loss equal to the heat gained: mgh=msΔT mgh = ms \Delta T We can simplify this equation by canceling out the mass m m : gh=sΔT gh = s \Delta T Now, solve for ΔT \Delta T : ΔT=ghs \Delta T = \dfrac{gh}{s} Substitute the known values: ΔT=10×2004200 \Delta T = \dfrac{10 \times 200}{4200} Calculate ΔT \Delta T : ΔT=20004200 \Delta T = \dfrac{2000}{4200} Simplify the fraction: ΔT=1021 \Delta T = \dfrac{10}{21} Therefore, the rise in temperature is ΔT0.48K \Delta T \approx 0.48 \, \text{K} .

Q276
In an adiabatic process, which of the following statements is true?
A The internal energy of the gas decreases as the temperature increases
B The molar heat capacity is zero
C Work done by the gas equals the increase in internal energy
D The molar heat capacity is infinite
Correct Answer
Option B
Solution

Option B is correct. • In an adiabatic process no heat is exchanged, so

δQ=0.\delta Q = 0.

• The (molar) heat capacity for any process is defined by

C=δQndT.C = \frac{\delta Q}{n\,dT}\,.

Since δQ=0\delta Q=0 even when dT0dT\neq0, it follows that

Cadiabatic=0.C_{\rm adiabatic}=0\,.

All other statements are therefore false.

Q277
The equation for real gas is given by (P+aV2)(Vb)=RT\left(\mathrm{P}+\dfrac{\mathrm{a}}{\mathrm{V}^2}\right)(\mathrm{V}-\mathrm{b})=\mathrm{RT}, where P,V,T\mathrm{P}, \mathrm{V}, \mathrm{T} and R are the pressure, volume, temperature and gas constant, respectively. The dimension of ab2\mathrm{ab}^{-2} is equivalent to that of :
A Compressibility
B Planck's constant
C Energy density
D Strain
Correct Answer
Option C
Solution

The equation for a real gas is given by: (P+aV2)(Vb)=RT \left(\mathrm{P} + \dfrac{\mathrm{a}}{\mathrm{V}^2}\right)(\mathrm{V} - \mathrm{b}) = \mathrm{RT} Here, P \mathrm{P} , V \mathrm{V} , T \mathrm{T} , and R R are the pressure, volume, temperature, and gas constant, respectively.

To find the dimension of ab2 ab^{-2} , we proceed with the following steps: Rearrange the equation for dimensions: [a]=[P][V2] [\mathrm{a}] = [\mathrm{P}][\mathrm{V}^2] Since [P]=ML1T2[\mathrm{P}] = \mathrm{ML}^{-1}\mathrm{T}^{-2} and [V]=L3[\mathrm{V}] = \mathrm{L}^3, we have: [a]=ML1T2(L6)=ML5T2 [\mathrm{a}] = \mathrm{ML}^{-1}\mathrm{T}^{-2}(\mathrm{L}^6) = \mathrm{ML}^5\mathrm{T}^{-2} As derived from the equation: [b]=[V]=L3[\mathrm{b}] = [\mathrm{V}] = \mathrm{L}^3 Now, to find [ab2][\mathrm{ab}^{-2}]: [ab2]=[a][b]2=ML5T2L6=ML1T2[\mathrm{ab}^{-2}] = \dfrac{[\mathrm{a}]}{[\mathrm{b}]^2} = \mathrm{ML}^5\mathrm{T}^{-2} \cdot \mathrm{L}^{-6} = \mathrm{ML}^{-1}\mathrm{T}^{-2} This dimension, ML1T2\mathrm{ML}^{-1}\mathrm{T}^{-2}, is equivalent to the dimension of energy density.

Q278

 Match with .  \text{ Match with . } $$ \begin{array}{lll} & \text { } & { }\\ \text { } \\ \text {

List - IList - II
(A) } & \text { Heat capacity of body } & \text { (I) } \mathrm{J} \mathrm{~kg}^{-1} \\ \text {
(B) } & \text { Specific heat capacity of body } & \text { (II) } \mathrm{J} \mathrm{~K}^{-1} \\ \text {
(C) } & \text { Latent heat } & \text { (III) } \mathrm{J} \mathrm{~kg}^{-1} \mathrm{~K}^{-1} \\ \text {
(D) } & \text { Thermal conductivity } & \text { (IV) } \mathrm{J} \mathrm{~m}^{-1} \mathrm{~K}^{-1} \mathrm{~s}^{-1} \end{array} \text {
A (A)-(IV), (B)-(III), (C)-(II), (D)-(I)
B (A)-(III), (B)-(I), (C)-(II), (D)-(IV)
C (A)-(III), (B)-(IV), (C)-(I), (D)-(II)
D (A)-(II), (B)-(III), (C)-(I), (D)-(IV)
Correct Answer
Option D
Solution

To match the entries in List-I with their corresponding units in List-II, we can use the definitions and formulas related to each concept in thermal physics: Heat Capacity of a Body (C') is defined as: C=ΔQΔT C' = \dfrac{\Delta Q}{\Delta T} The unit for heat capacity (C') is Joules per Kelvin (J K1^{-1}).

Specific Heat Capacity of a Body (S) indicates how much heat energy is required to change the temperature of a unit mass of a substance by one degree Kelvin: S=ΔQmΔT S = \dfrac{\Delta Q}{m \Delta T} The unit for specific heat capacity (S) is Joules per kilogram per Kelvin (J kg1^{-1} K1^{-1}).

Latent Heat (L) is the heat energy absorbed or released during a phase change of a substance at a constant temperature: L=ΔQm L = \dfrac{\Delta Q}{m} The unit for latent heat (L) is Joules per kilogram (J kg1^{-1}).

Thermal Conductivity (K) measures the ability of a material to conduct heat: ΔQ=KAΔTLK=ΔQLAΔT \Delta Q = \dfrac{KA \Delta T}{L} \quad \Rightarrow \quad K = \dfrac{\Delta Q \cdot L}{A \Delta T} The unit for thermal conductivity (K) is Joules per meter per Kelvin per second (J m1^{-1} K1^{-1} s1^{-1}).

Using these formulas and their corresponding units, the correct matches are: (A) Heat capacity of body \rightarrow (II) J K1^{-1} (B) Specific heat capacity of body \rightarrow (III) J kg1^{-1} K1^{-1} (C) Latent heat \rightarrow (I) J kg1^{-1} (D) Thermal conductivity \rightarrow (IV) J m1^{-1} K1^{-1} s1^{-1}

Q279
The helium and argon are put in the flask at the same room temperature (300 K). The ratio of average kinetic energies (per molecule) of helium and argon is: (Give: Molar mass of helium = 4 g/mol, Molar mass of argon = 40 g/mol)
A 1 : 10 \sqrt{10}
B 10 : 1
C 1 : 10
D 1 : 1
Correct Answer
Option D
Solution

Given the same room temperature of 300 K for helium and argon, we are tasked with finding the ratio of their average kinetic energies per molecule.

Formula for Kinetic Energy per Molecule: K.E.=f2kT \mathrm{K.E.} = \dfrac{\mathrm{f}}{2} \mathrm{kT} In this equation: f\mathrm{f} is the degrees of freedom, which is 3 for both helium (He) and argon (Ar) since they are monatomic gases. kk is the Boltzmann constant. TT is the temperature in Kelvin.

Kinetic Energy Comparison: For both helium and argon, since f=3\mathrm{f} = 3, the expression simplifies: KEHeKEAr=11 \dfrac{\mathrm{K} \cdot \mathrm{E}_{\mathrm{He}}}{\mathrm{K} \cdot \mathrm{E}_{\mathrm{Ar}}} = \dfrac{1}{1} Thus, the average kinetic energy per molecule for both gases is the same at the same temperature, leading to a ratio of: 1:1 1:1 This result implies that despite their differences in molar masses (helium being 4 g/mol and argon 40 g/mol), the average kinetic energy per molecule remains equal at the same temperature.

Q280
A gas is kept in a container having walls which are thermally non-conducting. Initially the gas has a volume of 800 cm3800 \mathrm{~cm}^3 and temperature 27C27^{\circ} \mathrm{C}. The change in temperature when the gas is adiabatically compressed to 200 cm3200 \mathrm{~cm}^3 is: (Take γ=1.5;γ\gamma=1.5 ; \gamma is the ratio of specific heats at constant pressure and at constant volume)
A 300 K
B 600 K
C 327 K
D 522 K
Correct Answer
Option A
Solution

To determine the change in temperature when a gas is adiabatically compressed, we are given the following initial conditions: Initial volume, V1=800cm3 V_1 = 800 \, \text{cm}^3 Final volume, V2=200cm3 V_2 = 200 \, \text{cm}^3 Initial temperature, T1=27C=300K T_1 = 27^\circ \text{C} = 300 \, \text{K} Adiabatic index (ratio of specific heats) γ=1.5 \gamma = 1.5 In an adiabatic process, the relationship between temperature and volume is given by the equation: TVγ1=constant TV^{\gamma-1} = \text{constant} Applying this to the initial and final states: 300×(800)0.5=T2×(200)0.5 300 \times (800)^{0.5} = T_2 \times (200)^{0.5} Solving for the final temperature T2 T_2 : T2=300×(800200)0.5=300×(4)0.5 T_2 = 300 \times \left( \dfrac{800}{200} \right)^{0.5} = 300 \times (4)^{0.5} T2=300×2=600K T_2 = 300 \times 2 = 600 \, \text{K} Thus, the change in temperature is: ΔT=T2T1=600K300K=300K \Delta T = T_2 - T_1 = 600 \, \text{K} - 300 \, \text{K} = 300 \, \text{K} Therefore, when the gas is adiabatically compressed, the temperature increases by 300 K.

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