CAIE A-Level Physics 14 Temperature
Practise analysing thermal equilibrium and temperature scales, evaluating thermometers and calculating heating, phase-change and energy-transfer quantities.
- Syllabus
- 2028–2030
- Course
- Physics 9702
- Level
- A2
Practise analysing thermal equilibrium and temperature scales, evaluating thermometers and calculating heating, phase-change and energy-transfer quantities.
Use the information in (i) to draw, on Fig. 1.1, a line to represent the temperature of the block, assuming no energy losses to the surroundings.
State
what may be deduced from the difference in the temperatures of two objects,
direction or rate of transfer of (thermal) energy
or (if different,) not in thermal equilibrium/energy is transferred
B1
the basic principle by which temperature is measured.
uses a property (of a substance) that changes with temperature
B1
By reference to your answer in (a)(ii), explain why two thermometers may not give the same temperature reading for an object.
temperature scale assumes linear change of property with temperature
- physical properties may not vary linearly with temperature
- agrees only at fixed points
Any 2 points.
B2
A block of aluminium of mass 670 g is heated at a constant rate of 95 W for 6.0 minutes. The specific heat capacity of aluminium is 910Jkg−1 K−1. The initial temperature of the block is 24∘C.
Assuming that no thermal energy is lost to the surroundings, show that the final temperature of the block is 80∘C.
Pt=mc(Δ)θ
C1
95×6×60=0.670×910×Δθ
M1
Δθ=56∘C so final temperature =56+24=80∘C
A1
or
95×6×60=0.67×910×(θ−24)
(M1)
so final temperature or θ=80∘C
(A1)
In practice, there are energy losses to the surroundings. The actual variation with time t of the temperature θ of the block is shown in Fig. 1.1.

Fig. 1.1
1. sketch: straight line from (0,24) to (6,80)
2. temperature drop due to energy loss =(80−64)=16∘C
energy loss =0.670×910×(80−64)=9800J
or
energy to raise temperature to 64∘C=0.670×910×(64−24)=24400Jloss=(95×6×60)−24400=9800J
Fig. 2.1 shows a laboratory thermometer that is calibrated to measure temperature in degrees Celsius.

Fig. 2.1
The thermometer makes use of the fact that the density of mercury varies with temperature.
State two other physical properties of materials, apart from the density of a liquid, that can be used for measuring temperature.
1
2
resistance of a metal
- volume of a gas at constant pressure
- e.m.f. of a thermocouple
Any two points, 1 mark each
B2
The thermometer is initially at 23.0∘C, as shown in Fig. 2.1. It is used to measure the temperature of an insulated beaker of water that is at 37.4∘C. The bulb of the thermometer is inserted into the water, and the water is stirred until the reading on the thermometer becomes steady.
The mass of water in the beaker is 18.7 g .
The mass of mercury in the thermometer is 6.94 g .
The specific heat capacity of water is 4.18 J g−1 K−1.
The specific heat capacity of mercury is 0.140 J g−1 K−1.
The glass of the thermometer and the beaker containing the water can be considered to have negligible heat capacity.
Calculate, to three significant figures, the final steady temperature indicated by the thermometer in the water. ∘C
Q=mcΔT
C1
evidence of realisation that Q lost by water =Q gained by mercury
C1
18.7×4.18×(37.4−T)=6.94×0.140×(T−23.0)
C1
T=37.2∘C
A1
Suggest one change that could be made to the design of the thermometer that would enable it to give a more accurate measurement of temperature.
use a liquid with a lower (specific) heat capacity (than mercury)
or
use a smaller mass of mercury
B1
Explain why the thermometer in Fig. 2.1 does not provide a direct measurement of thermodynamic temperature.
depends on properties of a real substance
B1
0∘C is not absolute zero
B1
A fixed mass of an ideal gas at a temperature of 20∘C is sealed in a cylinder by a piston, as shown in Fig. 2.1.

Fig. 2.1
The initial volume of the gas is 1.24×10−4 m3.
Thermal energy is supplied to the gas and its volume increases by 5.20×10−5 m3.
The mass of the gas is 16 g . For this expansion, there is a net transfer of 960 J of thermal energy to the gas.
Calculate the specific heat capacity c of the gas at this pressure.
c=Q/mΔT
C1
=960/(0.016×(416−293))=490 J kg−1 K−1
A1