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Thermo HW1

The document contains multiple-choice questions (MCQs) related to thermodynamics, covering topics such as thermodynamic functions, heat engines, and adiabatic processes. It includes questions about specific heat capacities, work done by gases, and the behavior of ideal gases under various conditions. Each question provides four answer options, with a focus on understanding the principles of thermodynamics.

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0% found this document useful (0 votes)
33 views2 pages

Thermo HW1

The document contains multiple-choice questions (MCQs) related to thermodynamics, covering topics such as thermodynamic functions, heat engines, and adiabatic processes. It includes questions about specific heat capacities, work done by gases, and the behavior of ideal gases under various conditions. Each question provides four answer options, with a focus on understanding the principles of thermodynamics.

Uploaded by

jane
Copyright
© © All Rights Reserved
We take content rights seriously. If you suspect this is your content, claim it here.
Available Formats
Download as PDF, TXT or read online on Scribd
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11

THERMODYNAMICS

MCQs with One Correct Answer (a) R (b) 2 R


R R
1. Which of the following is not a thermodynamical (c) (d)
3 4
function 5. Four curves A, B, C and D are drawn in the figure
(a) Enthalpy (b) Work done for a given amount of a gas. The curves which
(c) Gibb’s energy (d) Internal energy represent adiabatic and isothermal changes are
2. A gas can be taken from A to B via two different (a) C and D respectively
processes ACB and ADB. B
(b) D and C respectively P C
P A
D
C B (c) A and B respectively
(d) B and A respectively V
6. One mole of an ideal gas at an initial temperature
of T K does 6R joules of work adiabatically. If
A D the ratio of specific heats of this gas at constant
V pressure and at constant volume is 5/3, the final
When path ACB is used 60 J of heat flows into temperature of gas will be
the system and 30J of work is done by the (a) (T – 4) K (b) (T + 2.4) K
(c) (T – 2.4) K (d) (T + 4) K
system. If path ADB is used work done by the
7. A thermally insulted vessel contains 150 g of
system is 10 J. The heat Flow into the system in
water at 0°C. Then the air from the vessel is
path ADB is :
pumped out adiabatically. A fraction of water
(a) 40 J (b) 80 J turns into ice and the rest evaporates at 0°C
(c) 100 J (d) 20 J itself. The mass of evaporated water will be
3. Unit mass of a liquid with volume V 1 is closed to :
completely changed into a gas of volume V2 at a (Latent heat of vaporization of water = 2.10 ×
constant external pressure P and temperature T. 106 J kg–1 and Latent heat of Fusion of water
If the latent heat of evaporation for the given
= 3.36 × 105 J kg–1)
mass is L, then the increase in the internal energy
of the system is (a) 150 g (b) 20 g
(a) Zero (b) P(V2 – V1) (c) 130 g (d) 35 g
(c) L – P(V2 – V1) (d) L 8. Two Carnot engines A and B are operated in
4. The specific heat capacity of a monoatomic gas series. The engine A receives heat from the
for the process TV2 = constant is (where R is gas source at temperature T1 and rejects the heat to
constant) the sink at temperature T. The second engine B
40 PHYSICS

receives the heat at temperature T and rejects to undergoes and adiabatic change until the
its sink at temperature T2. For what value of T temperature returns to the initial value. What is
the efficiencies of the two engines are equal? the final volume of the gas?
T1 + T2 T -T
(a) (b) 1 2 (a) 112.4 lit. (b) 115.2 lit
2 2
(c) T 1T 2 (d) T1T2 (c) 120 lit (d) 125 lit
15. The relation between U, P and V for an ideal gas
9. An ideal heat engine works between in an adiabatic process is given by relation U = a
temperatures T1 = 500 K and T2 = 375 K. If the + bP V. Find the value of adiabatic exponent (g)
engine absorbs 600J of heat from the source, of this gas.
then the amount of heat released to the sink is: b +1 b +1
(a) 450 J (b) 600 J (a) (b)
b a
(c) 45 J (d) 500 J a +1 a
10. In a Carnot engine, the temperature of reservoir (c) (d)
b a+b
is 927°C and that of sink is 27°C. If the work 16. A thermodynamic system undergoes cyclic
done by the engine when it transfers heat from process ABCDA as shown in fig. The work
reservoir to sink is 12.6 × 106J, the quantity of done by the system in the cycle is :
heat absorbed by the engine from the reservoir (a) P0V0
is P C B
(b) 2P0V0 3P0
(a) 16.8 × 106 J (b) 4 × 106 J 2P0
(c) 7.6 × 106 J (d) 4.2 × 106 J P0 V0
(c) P0 D
11. A reversible engine converts one-sixth of the 2 A
heat input into work. When the temperature of V0 2V0 V
(d) Zero
the sink is reduced by 62ºC, the efficiency of the
17. An ideal gas goes through
engine is doubled. The temperatures of the
a r eversible cycle V
source and sink are c
a®b®c®d has the V - T b
(a) 99ºC, 37ºC (b) 80ºC, 37ºC diagram shown below.
(c) 95ºC, 37ºC (d) 90ºC, 37ºC Process d®a and b®c are d
a
12. Adiabatic modulus of elasticity of gas is 2.1 × adiabatic. T
105 N/m2. What will be its iosthermal modulus The corresponding P - V diagram for the process
æC ö
is (all figures are schematic and not drawn to
p
of elasticity ? çç C = 1.4 ÷÷ scale) :
è v ø P P
(a) 1.8 × 105 N/m2 (b) 1.5 × 105 N/m2 d c a b
5
(c) 1.4 × 10 N/m 2 (d) 1.2 × 105 N/m2. (a) (b) c
a b d
13. In an adiabatic process, the pressure is increased
2 3 V V
by % . If g = , then the volume decreases by P P
a
3 2 d c b
nearly
(c) a b (d) d c
4 2
(a) % (b) % V V
9 3 18. An ideal monatomic gas with pressure P, volume
9 V and temperature T is expanded isothermally to
(c) 1% (d) % a volume 2V and a final pressure Pi. If the same
4 gas is expanded adiabatically to a volume 2V,
14. Two moles of helium gas (g = 5/3) are initially at P
temperature 27°C and occupy a volume of 20 the final pressure is Pa. The ratio a is
Pi
litres. The gas is first expanded at constant –1/3 1/3
(a) 2 (b) 2
pressure until the volume is doubled. Then, it
(c) 22/3 (d) 2–2/3

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