Class 11 Physics Chapter 10 NEET / JEE

Thermal Properties of Matter – NCERT Solutions

Step-by-step solutions with formulas and diagrams for all questions from NCERT Class 11 Physics Chapter 10.

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⚡ Quick Revision – Key Formulas

Linear Expansion $$\Delta L=\alpha L_0 \Delta T$$
Heat Equation $$Q=mc\Delta T$$
Heat Conduction $$\frac{Q}{t}=\frac{kA\Delta T}{x}$$

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Q1 The triple points of neon and carbon dioxide are 24.57 K and 216.55 K respectively. Express these temperatures on the Celsius and Fahrenheit scales.

Solution
Brief Theory

Temperature can be expressed in different scales such as Kelvin (K), Celsius (°C), and Fahrenheit (°F). The Kelvin scale is an absolute thermodynamic scale where 0 K corresponds to absolute zero.

The conversion relations between temperature scales are:

$$ t_C = T_K - 273.15 $$ $$ t_F = \frac{9}{5}t_C + 32 $$

where

  • \(T_K\) = temperature on Kelvin scale
  • \(t_C\) = temperature on Celsius scale
  • \(t_F\) = temperature on Fahrenheit scale

Step-1: Triple Point of Neon

Given:

$$ T = 24.57\ \text{K} $$

Convert Kelvin → Celsius

$$ \begin{aligned} t_C &= T - 273.15 \\ &= 24.57 - 273.15 \\ &= -248.58^\circ\text{C} \end{aligned} $$

Convert Celsius → Fahrenheit

$$ \begin{aligned} t_F &= \frac{9}{5}t_C + 32 \\ &= \frac{9}{5}(-248.58) + 32 \\ &= -447.444 + 32 \\ &= -415.44^\circ\text{F} \end{aligned} $$

Thus, the triple point of neon is:

  • \(-248.58^\circ C\)
  • \(-415.44^\circ F\)

Step-2: Triple Point of Carbon Dioxide

Given:

$$ T = 216.55\ \text{K} $$

Convert Kelvin → Celsius

$$ \begin{aligned} t_C &= T - 273.15 \\ &= 216.55 - 273.15 \\ &= -56.60^\circ\text{C} \end{aligned} $$

Convert Celsius → Fahrenheit

$$ \begin{aligned} t_F &= \frac{9}{5}t_C + 32 \\ &= \frac{9}{5}(-56.60) + 32 \\ &= -101.88 + 32 \\ &= -69.88^\circ\text{F} \end{aligned} $$

Thus, the triple point of carbon dioxide is:

  • \(-56.60^\circ C\)
  • \(-69.88^\circ F\)

Conceptual Illustration
Kelvin Celsius Fahrenheit Neon 24.57 K −248.58 °C −415.44 °F CO₂ 216.55 K −56.60 °C −69.88 °F

This diagram illustrates how the same physical temperature corresponds to different numerical values on the Kelvin, Celsius, and Fahrenheit scales.

Progress: Question 1 of 20

Q2 Two absolute scales A and B have triple points of water defined to be 200 A and 350 B. What is the relation between \(T_A\) and \(T_B\)?

Solution
Brief Theory

An absolute temperature scale is a thermodynamic scale whose zero corresponds to absolute zero. All absolute scales are linearly proportional because they measure temperature from the same physical reference.

If two absolute scales are calibrated using the same fixed point (such as the triple point of water), their readings are related by:

$$ \frac{T_A}{(T_A)_{tp}} = \frac{T_B}{(T_B)_{tp}} $$

where \( (T_A)_{tp} \) and \( (T_B)_{tp} \) represent the triple-point values on scales A and B.


Given
  • Triple point of water on scale A = \(200\,A\)
  • Triple point of water on scale B = \(350\,B\)

Since both correspond to the same physical temperature, they can be equated through proportionality.


Step-1: Establish the proportional relation
$$ \frac{T_A}{200} = \frac{T_B}{350} $$
Step-2: Solve for relation between \(T_A\) and \(T_B\)
$$ \begin{aligned} \frac{T_A}{200} &= \frac{T_B}{350} \\ T_A &= \frac{200}{350}T_B \\ T_A &= \frac{4}{7}T_B \end{aligned} $$
Final Relation
$$ \boxed{T_A = \frac{4}{7} T_B} $$

Thus, the temperature reading on scale A is \(\frac{4}{7}\) of the corresponding reading on scale B.


Conceptual Illustration
Scale A Scale B 200 A (Triple Point) 350 B (Triple Point) Same Physical Temperature

The diagram shows that although the numerical values differ (200 A and 350 B), both represent the same thermodynamic temperature (triple point of water), leading to a proportional relation between the two scales.

Progress: Question 2 of 20

Q3 The electrical resistance in ohms of a certain thermometer varies with temperature according to the approximate law: \( R = R_0[1 + \alpha (T - T_0)] \). The resistance is \(101.6\,\Omega\) at the triple point of water \(273.16\,K\), and \(165.5\,\Omega\) at the normal melting point of lead \(600.5\,K\). What is the temperature when the resistance is \(123.4\,\Omega\)?

Solution
Brief Theory

In a resistance thermometer, the electrical resistance of a metal changes approximately linearly with temperature over a moderate range. The relation is

$$ R = R_0 \left[1 + \alpha (T - T_0)\right] $$

where

  • \(R\) = resistance at temperature \(T\)
  • \(R_0\) = resistance at reference temperature \(T_0\)
  • \(\alpha\) = temperature coefficient of resistance

Using two known calibration points, we can first determine \(\alpha\), and then compute the unknown temperature.


Given Data
  • \(R_0 = 101.6\,\Omega\)
  • \(T_0 = 273.16\,K\)
  • \(R_2 = 165.5\,\Omega\)
  • \(T_2 = 600.5\,K\)
  • Required: Temperature when \(R = 123.4\,\Omega\)

Step-1: Determine the temperature coefficient \( \alpha \)
Using the resistance equation for the second calibration point: $$ 165.5 = 101.6\left[1+\alpha(600.5-273.16)\right] $$ Temperature difference: $$ 600.5 - 273.16 = 327.34 $$ Substitute: $$ \frac{165.5}{101.6} = 1 + \alpha(327.34) $$ $$ 1.6295 = 1 + 327.34\alpha $$ $$ 327.34\alpha = 0.6295 $$ $$ \alpha = \frac{0.6295}{327.34} $$ $$ \alpha \approx 1.92\times10^{-3}\,K^{-1} $$
Step-2: Determine the unknown temperature
Using $$ R = R_0[1+\alpha(T-T_0)] $$ Substitute values: $$ 123.4 = 101.6[1+\alpha(T-273.16)] $$ Divide both sides by \(101.6\): $$ \frac{123.4}{101.6} = 1 + \alpha(T-273.16) $$ $$ 1.21496 = 1 + \alpha(T-273.16) $$ $$ 0.21496 = \alpha(T-273.16) $$ Substitute \(\alpha = 1.92\times10^{-3}\): $$ 0.21496 = (1.92\times10^{-3})(T-273.16) $$ $$ T - 273.16 \approx 111.8 $$ $$ T \approx 384.96\,K $$
Final Answer
$$ \boxed{T \approx 3.85\times10^2\,K \;(\text{or } 385\,K)} $$
Conceptual Illustration
T (K) R (Ω) 273 K, 101.6 Ω 600.5 K, 165.5 Ω ≈385 K, 123.4 Ω

The resistance thermometer shows an approximately linear increase of resistance with temperature. Using two calibration points, the temperature corresponding to any intermediate resistance can be determined.

Progress: Question 3 of 20

Q4 Answer the following :
(a) The triple-point of water is a standard fixed point in modern thermometry. Why? What is wrong in taking the melting point of ice and the boiling point of water as standard fixed points (as was originally done in the Celsius scale)?

(b) There were two fixed points in the original Celsius scale which were assigned 0 °C and 100 °C respectively. On the absolute scale, one of the fixed points is the triple-point of water (273.16 K). What is the other fixed point on the Kelvin scale?

(c) The absolute temperature \(T\) (Kelvin scale) is related to the Celsius temperature \(t_c\) by \(t_c = T - 273.15\). Why is the constant \(273.15\) used instead of \(273.16\)?

(d) What is the temperature of the triple-point of water on an absolute scale whose unit interval size is equal to that of the Fahrenheit scale?

Solution
Brief Theory

Thermometry requires fixed reference points that are reproducible and independent of environmental variations. Modern thermodynamic temperature scales therefore use the triple point of water and absolute zero as reference points because these temperatures are fundamental physical constants.


(a) Why is the triple point of water used as a standard fixed point?

The triple point of water is the unique condition where ice, liquid water, and water vapour coexist in equilibrium. This occurs at a definite temperature and pressure.

  • Triple-point temperature = 273.16 K
  • Triple-point pressure ≈ 611 Pa

This temperature is highly reproducible in laboratories.

In contrast:

  • The boiling point of water depends strongly on atmospheric pressure.
  • The melting point of ice can vary slightly due to impurities and pressure.

Hence these points are not sufficiently stable for precise thermometry.

Ice Vapour Liquid Triple Point

The central point represents the equilibrium of all three phases.


(b) Other fixed point on the Kelvin scale

The Kelvin scale has two fundamental reference points:

  • Absolute zero = 0 K
  • Triple point of water = 273.16 K

Absolute zero corresponds to the lowest possible temperature where the thermal motion of particles becomes minimal.

$$ \boxed{\text{Other fixed point = Absolute Zero (0 K)}} $$
(c) Why does the relation use 273.15 instead of 273.16?

The relation between Celsius and Kelvin scales is

$$ t_c = T - 273.15 $$

This occurs because:

  • 0 °C is defined as the melting point of ice.
  • The melting point of ice corresponds to 273.15 K.
  • The triple point of water is slightly higher at 273.16 K.

Thus the difference arises because the Celsius scale is referenced to the melting point of ice, not the triple point.


(d) Triple-point temperature on an absolute Fahrenheit-type scale

If an absolute scale uses the same unit size as Fahrenheit, its zero must still correspond to absolute zero.

Conversion between Kelvin and Fahrenheit intervals:

$$ 1\,K = \frac{9}{5} \,^\circ F = 1.8^\circ F $$

Triple point of water:

$$ T = 273.16 K $$

Therefore on this absolute Fahrenheit scale:

$$ \begin{aligned} T &= 273.16 \times 1.8 \\ T &\approx 491.7 \end{aligned} $$
Final Answer
  • (a) Triple point is used because it is a unique, reproducible equilibrium state independent of pressure.
  • (b) The other fixed point on the Kelvin scale is absolute zero (0 K).
  • (c) The constant \(273.15\) appears because \(0^\circ C = 273.15\,K\), the melting point of ice.
  • (d) Triple point on the absolute Fahrenheit-interval scale ≈ 491.7 units.
Progress: Question 4 of 20

Q5 Two ideal gas thermometers A and B use oxygen and hydrogen respectively. The following observations are made:

Temperature Pressure (Thermometer A) Pressure (Thermometer B)
Triple point of water \(1.250 \times 10^5\ \text{Pa}\) \(0.200 \times 10^5\ \text{Pa}\)
Normal melting point of sulphur \(1.797 \times 10^5\ \text{Pa}\) \(0.287 \times 10^5\ \text{Pa}\)

(a) What is the absolute temperature of the normal melting point of sulphur as read by thermometers A and B?
(b) Why do the readings differ slightly? What procedure reduces this discrepancy?

Solution
Brief Theory

In a constant-volume gas thermometer, the pressure of a fixed mass of gas is directly proportional to its absolute temperature:

$$ T \propto P $$

Thus, using the triple point of water as a reference:

$$ T = T_{tp}\frac{P}{P_{tp}} $$

where

  • \(T_{tp} = 273.16\,K\) (triple-point temperature of water)
  • \(P_{tp}\) = pressure at triple point
  • \(P\) = pressure at the required temperature

(a) Temperature of melting point of sulphur
Thermometer A (oxygen)

Given:

  • \(P_{tp,A} = 1.250 \times 10^5\,Pa\)
  • \(P_A = 1.797 \times 10^5\,Pa\)
Using $$ T_A = 273.16 \times \frac{P_A}{P_{tp,A}} $$ $$ T_A = 273.16 \times \frac{1.797}{1.250} $$ $$ T_A = 273.16 \times 1.4376 $$ $$ T_A \approx 392.7\,K $$
Thermometer B (hydrogen)

Given:

  • \(P_{tp,B} = 0.200 \times 10^5\,Pa\)
  • \(P_B = 0.287 \times 10^5\,Pa\)
$$ T_B = 273.16 \times \frac{P_B}{P_{tp,B}} $$ $$ T_B = 273.16 \times \frac{0.287}{0.200} $$ $$ T_B = 273.16 \times 1.435 $$ $$ T_B \approx 392.1\,K $$
Result
  • Temperature by thermometer A ≈ 392.7 K
  • Temperature by thermometer B ≈ 392.1 K

(b) Reason for discrepancy

The difference occurs because real gases deviate slightly from ideal-gas behaviour. Oxygen and hydrogen exhibit different deviations from the ideal gas law at finite pressures, leading to slightly different temperature readings.

However, as pressure approaches zero, all gases behave more ideally.


How to reduce the discrepancy

The experiment should be repeated at progressively lower gas pressures, and the measured temperatures should be extrapolated to zero pressure.

At zero pressure, all gases approach ideal behaviour and yield the same thermodynamic temperature.


Conceptual Illustration
Temperature (K) Pressure O₂ H₂ Extrapolation to P → 0

Different gases give slightly different slopes at finite pressure, but extrapolating to zero pressure yields the same thermodynamic temperature.

Progress: Question 5 of 20

Q6 A steel tape 1 m long is correctly calibrated for a temperature of 27.0 °C. The length of a steel rod measured by this tape is found to be 63.0 cm on a hot day when the temperature is 45.0 °C. What is the actual length of the steel rod on that day? What is the length of the same steel rod on a day when the temperature is 27.0 °C? Coefficient of linear expansion of steel = \(1.20 \times 10^{-5}\ K^{-1}\).

Solution
Brief Theory

When temperature changes, the length of a solid changes according to the law of linear expansion:

$$ L = L_0 (1 + \alpha \Delta T) $$

where

  • \(L_0\) = original length
  • \(L\) = expanded length
  • \(\alpha\) = coefficient of linear expansion
  • \(\Delta T\) = temperature change

If the measuring tape expands, the distance between its markings increases. Hence the scale reads a value slightly smaller than the true length.


Given Data
  • Calibration temperature \(T_0 = 27^\circ C\)
  • Hot day temperature \(T = 45^\circ C\)
  • Measured length \(= 63.0\ \text{cm}\)
  • \(\alpha = 1.20 \times 10^{-5}\ K^{-1}\)
Temperature rise: $$ \Delta T = 45 - 27 = 18^\circ C $$
Step-1: Actual length of the rod on the hot day

Because the tape expands, the apparent length is related to the true length by

$$ L_{\text{apparent}} = \frac{L_{\text{true}}}{1+\alpha \Delta T} $$ Substituting values: $$ 63.0 = \frac{L}{1 + (1.20\times10^{-5})(18)} $$ $$ 63.0 = \frac{L}{1.000216} $$ Therefore, $$ L = 63.0 \times 1.000216 $$ $$ L \approx 63.014\ \text{cm} $$

Thus, the actual length of the rod at \(45^\circ C\) is

$$ \boxed{63.014\ \text{cm}} $$
Step-2: Length of the rod at \(27^\circ C\)

Now the rod itself contracts when temperature decreases from \(45^\circ C\) to \(27^\circ C\).

Using $$ L = L_0 (1 + \alpha \Delta T) $$ Rearranging: $$ L_0 = \frac{L}{1 + \alpha \Delta T} $$ Substitute: $$ L_0 = \frac{63.014}{1.000216} $$ $$ L_0 \approx 63.000\ \text{cm} $$

Hence, the length of the rod at \(27^\circ C\) is approximately

$$ \boxed{63.0\ \text{cm}} $$
Conceptual Illustration
Tape at 27°C (Correct scale) Tape expanded at 45°C

When the tape expands at higher temperature, the spacing between its markings increases. Hence the measured value becomes slightly smaller than the true length.

Progress: Question 6 of 20

Q7 A large steel wheel is to be fitted on to a shaft of the same material. At 27 °C, the outer diameter of the shaft is 8.70 cm and the diameter of the central hole in the wheel is 8.69 cm. The shaft is cooled using dry ice. At what temperature of the shaft does the wheel slip on the shaft? Coefficient of linear expansion of steel: \( \alpha = 1.20 \times 10^{-5}\ K^{-1} \)

Solution
Brief Theory

When temperature changes, the dimensions of a solid change according to the law of linear expansion:

$$ L = L_0 (1 + \alpha \Delta T) $$

If the temperature decreases, the body undergoes thermal contraction. In mechanical engineering this method is called shrink fitting, where a shaft is cooled so that it contracts and fits into a hole.


Given Data
  • Initial temperature \(T_0 = 27^\circ C\)
  • Initial shaft diameter \(D_0 = 8.70\ \text{cm}\)
  • Required diameter \(D = 8.69\ \text{cm}\)
  • \(\alpha = 1.20 \times 10^{-5}\ K^{-1}\)

For the wheel to slip onto the shaft, the shaft must contract until its diameter equals the hole diameter.


Step-1: Apply the linear expansion relation
$$ D = D_0 [1 + \alpha (T - T_0)] $$ Substitute the values: $$ 8.69 = 8.70 \left[1 + \alpha (T - 27)\right] $$
Step-2: Solve for temperature
Divide both sides by \(8.70\): $$ \frac{8.69}{8.70} = 1 + \alpha (T - 27) $$ $$ 0.99885 = 1 + \alpha (T - 27) $$ $$ \alpha (T - 27) = -0.00115 $$ Substitute \( \alpha = 1.20 \times 10^{-5} \): $$ T - 27 = \frac{-0.00115}{1.20 \times 10^{-5}} $$ $$ T - 27 \approx -95.8 $$ $$ T \approx -68.8^\circ C $$
Final Answer

The shaft must be cooled to approximately

$$ \boxed{-69^\circ C} $$

so that its diameter contracts sufficiently for the wheel to slip onto it.


Conceptual Illustration
Wheel hole Shaft at 27°C Contracted shaft (cooled)

Cooling the shaft reduces its diameter due to thermal contraction, allowing it to fit into the slightly smaller hole of the wheel.

Progress: Question 7 of 20

Q8 A hole is drilled in a copper sheet. The diameter of the hole is 4.24 cm at 27.0 °C. What is the change in the diameter of the hole when the sheet is heated to 227 °C? Coefficient of linear expansion of copper: \( \alpha = 1.70 \times 10^{-5}\ K^{-1} \)

Solution
Brief Theory

When a metal sheet expands due to heating, every linear dimension increases in the same proportion. A useful principle in thermal expansion is:

A hole in a metal plate expands exactly as if the hole were filled with the same material.

Hence the diameter of the hole increases according to the law of linear expansion.

$$ L = L_0 (1 + \alpha \Delta T) $$ where
  • \(L_0\) = original diameter
  • \(L\) = diameter after heating
  • \(\alpha\) = coefficient of linear expansion
  • \(\Delta T\) = temperature change

Given Data
  • Initial diameter \(L_0 = 4.24\ \text{cm}\)
  • Initial temperature \(T_0 = 27^\circ C\)
  • Final temperature \(T = 227^\circ C\)
  • \(\alpha = 1.70 \times 10^{-5}\ K^{-1}\)
Temperature rise: $$ \Delta T = 227 - 27 = 200\ K $$
Step-1: Calculate the expanded diameter
$$ L = L_0(1 + \alpha \Delta T) $$ Substitute values: $$ L = 4.24 \left[1 + (1.70\times10^{-5})(200)\right] $$ $$ L = 4.24 (1 + 0.0034) $$ $$ L = 4.24 \times 1.0034 $$ $$ L \approx 4.254\ \text{cm} $$
Step-2: Change in diameter
$$ \Delta L = L - L_0 $$ $$ \Delta L = 4.254 - 4.24 $$ $$ \Delta L = 0.0144\ \text{cm} $$
Final Answer

Increase in diameter of the hole:

$$ \boxed{\Delta L = 1.44 \times 10^{-2}\ \text{cm}} $$

Thus, heating the copper sheet to \(227^\circ C\) increases the diameter of the hole by approximately \(0.0144\ \text{cm}\).


Conceptual Illustration
Hole at 27°C Hole at 227°C

When the sheet expands due to heating, the surrounding material moves outward, causing the hole to expand as well.

Progress: Question 8 of 20

Q9 A brass wire 1.8 m long at 27 °C is held taut with little tension between two rigid supports. If the wire is cooled to –39 °C, what is the tension developed in the wire, if its diameter is 2.0 mm? Coefficient of linear expansion of brass: \( \alpha = 2.0 \times 10^{-5}\ K^{-1} \) Young’s modulus of brass: \( Y = 0.91 \times 10^{11}\ \text{Pa} \)

Solution
Brief Theory

If a body is free, it contracts on cooling according to

$$ \frac{\Delta L}{L} = \alpha \Delta T $$

However, when a wire is fixed between rigid supports, it cannot contract. This restriction produces thermal stress in the wire.

Using Young’s modulus:

$$ Y = \frac{\text{stress}}{\text{strain}} = \frac{\sigma}{\varepsilon} $$ Thus, $$ \sigma = Y\varepsilon $$ where the thermal strain is $$ \varepsilon = \alpha \Delta T $$
Given Data
  • Length of wire \(L = 1.8\ \text{m}\)
  • Initial temperature \(= 27^\circ C\)
  • Final temperature \(= -39^\circ C\)
  • \(\alpha = 2.0 \times 10^{-5}\ K^{-1}\)
  • \(Y = 0.91 \times 10^{11}\ \text{Pa}\)
  • Diameter \(d = 2.0\ \text{mm} = 2.0 \times 10^{-3}\ \text{m}\)
Temperature change: $$ \Delta T = 27 - (-39) = 66\ K $$
Step-1: Thermal strain
$$ \varepsilon = \alpha \Delta T $$ $$ \varepsilon = (2.0\times10^{-5})(66) $$ $$ \varepsilon = 1.32\times10^{-3} $$
Step-2: Thermal stress
$$ \sigma = Y\varepsilon $$ $$ \sigma = (0.91\times10^{11})(1.32\times10^{-3}) $$ $$ \sigma \approx 1.20\times10^{8}\ \text{Pa} $$
Step-3: Cross-sectional area of wire
Radius: $$ r = \frac{d}{2} = 1.0\times10^{-3}\ \text{m} $$ Area: $$ A = \pi r^2 $$ $$ A = \pi (1.0\times10^{-3})^2 $$ $$ A = \pi\times10^{-6}\ \text{m}^2 $$
Step-4: Tension in the wire
Force: $$ F = \sigma A $$ $$ F = (1.20\times10^{8})(\pi\times10^{-6}) $$ $$ F \approx 3.77\times10^{2}\ \text{N} $$
Final Answer

The tension developed in the wire is approximately

$$ \boxed{F \approx 3.8 \times 10^{2}\ \text{N}} $$
Conceptual Illustration
Cooling → contraction tendency Rigid supports create tensile stress

Since the wire cannot contract due to rigid supports, cooling produces tensile stress which results in a tension force in the wire.

Progress: Question 9 of 20

Q10 A brass rod of length 50 cm and diameter 3.0 mm is joined to a steel rod of the same length and diameter. What is the change in length of the combined rod at 250 °C, if the original lengths are at 40.0 °C? Is there a thermal stress developed at the junction? (Coefficient of linear expansion: brass \(= 2.0\times10^{-5}\ K^{-1}\), steel \(= 1.2\times10^{-5}\ K^{-1}\))

Solution
Brief Theory

The change in length of a solid due to temperature change is given by the linear expansion relation:

$$ \Delta L = L_0 \alpha \Delta T $$

where

  • \(L_0\) = original length
  • \(\alpha\) = coefficient of linear expansion
  • \(\Delta T\) = temperature change

If two rods are joined end-to-end but the ends are free, each rod expands independently according to its own coefficient of expansion. Hence, no thermal stress develops at the junction.


Given Data
  • Length of each rod \(= 50\ \text{cm}\)
  • Initial temperature \(= 40^\circ C\)
  • Final temperature \(= 250^\circ C\)
  • \(\alpha_{brass} = 2.0\times10^{-5}\ K^{-1}\)
  • \(\alpha_{steel} = 1.2\times10^{-5}\ K^{-1}\)
Temperature rise: $$ \Delta T = 250 - 40 = 210\ K $$
Step-1: Expansion of the brass rod
$$ \Delta L_b = L_0 \alpha_b \Delta T $$ $$ \Delta L_b = 50 \times (2.0\times10^{-5}) \times 210 $$ $$ \Delta L_b = 50 \times 4.2\times10^{-3} $$ $$ \Delta L_b = 0.21\ \text{cm} $$ Thus, $$ L_b = 50 + 0.21 = 50.21\ \text{cm} $$
Step-2: Expansion of the steel rod
$$ \Delta L_s = L_0 \alpha_s \Delta T $$ $$ \Delta L_s = 50 \times (1.2\times10^{-5}) \times 210 $$ $$ \Delta L_s = 50 \times 2.52\times10^{-3} $$ $$ \Delta L_s = 0.126\ \text{cm} $$ Thus, $$ L_s = 50 + 0.126 = 50.126\ \text{cm} $$
Step-3: Total length of the combined rod
Initial combined length: $$ L_0 = 50 + 50 = 100\ \text{cm} $$ Final combined length: $$ L = L_b + L_s $$ $$ L = 50.21 + 50.126 $$ $$ L = 100.336\ \text{cm} $$
Step-4: Total change in length
$$ \Delta L = 100.336 - 100 $$ $$ \Delta L = 0.336\ \text{cm} $$
Thermal Stress at the Junction

Since the ends of the combined rod are free to expand, both rods expand naturally according to their own coefficients of expansion.

Therefore,

$$ \boxed{\text{No thermal stress develops at the junction}} $$
Conceptual Illustration
Brass Rod Steel Rod Free expansion of both rods

Because the ends are free, each rod expands independently and the junction does not experience thermal stress.

Progress: Question 10 of 20

Q11 The coefficient of volume expansion of glycerine is \(49 \times 10^{-5}\ K^{-1}\). What is the fractional change in its density for a 30 °C rise in temperature?

Solution
Brief Theory

When a liquid is heated, its volume increases according to the relation

$$ \frac{\Delta V}{V} = \beta \Delta T $$

where

  • \(\beta\) = coefficient of volume expansion
  • \(\Delta T\) = temperature change

Density is defined as

$$ \rho = \frac{m}{V} $$

Since the mass remains constant during heating, an increase in volume leads to a decrease in density. Thus,

$$ \frac{\Delta \rho}{\rho} = -\frac{\Delta V}{V} $$
Given Data
  • Coefficient of volume expansion \(\beta = 49 \times 10^{-5}\ K^{-1}\)
  • Temperature rise \(\Delta T = 30^\circ C\)

Step-1: Fractional change in volume
$$ \frac{\Delta V}{V} = \beta \Delta T $$ Substitute values: $$ \frac{\Delta V}{V} = (49 \times 10^{-5}) \times 30 $$ $$ = 1470 \times 10^{-5} $$ $$ = 0.0147 $$
Step-2: Fractional change in density
Since density is inversely proportional to volume: $$ \frac{\Delta \rho}{\rho} = -\frac{\Delta V}{V} $$ $$ \frac{\Delta \rho}{\rho} = -0.0147 $$
Final Answer

The fractional change in density is

$$ \boxed{\frac{\Delta \rho}{\rho} = -0.0147} $$

Thus the density of glycerine decreases by approximately 1.47 % for a temperature rise of \(30^\circ C\).


Conceptual Illustration
Before Heating After Heating Volume increases → Density decreases

Heating causes the liquid to expand (increase in volume), which reduces its density since the mass remains unchanged.

Progress: Question 11 of 20

Q12 A 10 kW drilling machine is used to drill a bore in a small aluminium block of mass 8.0 kg. How much is the rise in temperature of the block in 2.5 minutes, assuming 50% of power is used up in heating the machine itself or lost to the surroundings? Specific heat of aluminium = \(0.91\ \text{J g}^{-1}\text{K}^{-1}\).

Solution
Brief Theory

Mechanical work done by a machine can be converted into heat energy. The heat supplied to a body is related to the rise in temperature by

$$ Q = mc\Delta T $$

where

  • \(Q\) = heat energy supplied
  • \(m\) = mass of the substance
  • \(c\) = specific heat capacity
  • \(\Delta T\) = temperature rise

If a machine of power \(P\) operates for time \(t\), the total energy supplied is

$$ E = Pt $$
Given Data
  • Power of drilling machine \(P = 10\ \text{kW} = 10^4\ \text{W}\)
  • Time \(t = 2.5\ \text{min} = 150\ \text{s}\)
  • Mass of aluminium \(m = 8.0\ \text{kg} = 8.0\times10^3\ \text{g}\)
  • Specific heat \(c = 0.91\ \text{J g}^{-1}\text{K}^{-1}\)
  • Only \(50\%\) of energy heats the block

Step-1: Total energy supplied by the machine
$$ E = Pt $$ $$ E = 10^4 \times 150 $$ $$ E = 1.5\times10^6\ \text{J} $$
Step-2: Useful heat absorbed by the block
Since only 50% of the energy heats the aluminium, $$ Q = 0.5 \times 1.5\times10^6 $$ $$ Q = 7.5\times10^5\ \text{J} $$
Step-3: Temperature rise of the aluminium block
Using $$ Q = mc\Delta T $$ $$ 7.5\times10^5 = (8.0\times10^3)(0.91)\Delta T $$ $$ \Delta T = \frac{7.5\times10^5}{8.0\times10^3 \times 0.91} $$ $$ \Delta T \approx 1.03\times10^2\ \text{K} $$ $$ \Delta T \approx 103\ \text{K} $$
Final Answer

The rise in temperature of the aluminium block is

$$ \boxed{\Delta T \approx 103\ \text{K} \;(\text{or } 103^\circ C)} $$
Conceptual Illustration
Drilling Machine Aluminium Block Mechanical work → Heat Temperature rises

During drilling, mechanical work is converted into heat. A part of this heat raises the temperature of the aluminium block.

Progress: Question 12 of 20

Q13 A copper block of mass 2.5 kg is heated in a furnace to a temperature of 500 °C and then placed on a large ice block. What is the maximum amount of ice that can melt? (Specific heat of copper = \(0.39\ \text{J g}^{-1}\text{K}^{-1}\); Heat of fusion of ice = \(335\ \text{J g}^{-1}\))

Solution
Brief Theory

In calorimetry, the heat lost by a hot body equals the heat gained by a colder body, provided there is no heat loss to the surroundings.

When the hot copper block is placed on ice at \(0^\circ C\), the copper cools down to \(0^\circ C\). The heat released during cooling is used to melt the ice.

The heat lost by copper: $$ Q = mc\Delta T $$ The heat required to melt ice: $$ Q = mL $$
Given Data
  • Mass of copper block \(m = 2.5\ \text{kg} = 2.5\times10^3\ \text{g}\)
  • Initial temperature of copper \(T_1 = 500^\circ C\)
  • Final temperature \(T_2 = 0^\circ C\)
  • Specific heat of copper \(c = 0.39\ \text{J g}^{-1}\text{K}^{-1}\)
  • Heat of fusion of ice \(L = 335\ \text{J g}^{-1}\)
Temperature change: $$ \Delta T = 500 - 0 = 500\ K $$
Step-1: Heat lost by copper
$$ Q_{\text{Cu}} = mc\Delta T $$ $$ Q_{\text{Cu}} = (2.5\times10^3)(0.39)(500) $$ $$ Q_{\text{Cu}} = 4.875\times10^5\ \text{J} $$
Step-2: Ice melted
Let \(m\) be the mass of ice melted. $$ Q_{\text{ice}} = mL $$ Equating heat lost and gained: $$ 4.875\times10^5 = m \times 335 $$ $$ m = \frac{4.875\times10^5}{335} $$ $$ m \approx 1.45\times10^3\ \text{g} $$ $$ m \approx 1.45\ \text{kg} $$
Final Answer

The maximum mass of ice that can melt is

$$ \boxed{1.45\ \text{kg}} $$
Conceptual Illustration
Hot Copper Block 500°C Ice 0°C Heat flows from copper → ice

The hot copper block releases heat while cooling to \(0^\circ C\). This heat is used to melt the ice without raising its temperature.

Progress: Question 13 of 20

Q14 In an experiment on the specific heat of a metal, a 0.20 kg block of the metal at 150 °C is dropped in a copper calorimeter (water equivalent 0.025 kg) containing 150 cm³ of water at 27 °C. The final temperature is 40 °C. Compute the specific heat of the metal. If heat losses to the surroundings are not negligible, is your answer greater or smaller than the actual value?

Solution
Brief Theory

In calorimetry experiments, the heat lost by the hot body equals the heat gained by the colder bodies, provided no heat is lost to the surroundings.

Thus, $$ \text{Heat lost by metal} = \text{Heat gained by water + calorimeter} $$ Using $$ Q = mc\Delta T $$
Given Data
  • Mass of metal \(m_m = 0.20\ \text{kg} = 200\ \text{g}\)
  • Initial temperature of metal \(=150^\circ C\)
  • Final temperature \(=40^\circ C\)
  • Water equivalent of calorimeter \(=0.025\ \text{kg}\)
  • Volume of water \(=150\ \text{cm}^3\)
  • Mass of water \(=150\ \text{g}=0.150\ \text{kg}\)
  • Specific heat of water \(=4186\ \text{J kg}^{-1}\text{K}^{-1}\)
Temperature rise of water and calorimeter: $$ \Delta T = 40-27 = 13^\circ C $$ Temperature fall of metal: $$ \Delta T_m = 150-40 = 110^\circ C $$
Step-1: Heat gained by water
$$ Q_w = mc\Delta T $$ $$ Q_w = 0.150 \times 4186 \times 13 $$ $$ Q_w \approx 8.16 \times 10^3\ \text{J} $$
Step-2: Heat gained by calorimeter
$$ Q_{cal} = mc\Delta T $$ $$ Q_{cal} = 0.025 \times 4186 \times 13 $$ $$ Q_{cal} \approx 1.36 \times 10^3\ \text{J} $$
Step-3: Total heat gained
$$ Q_{gain} = Q_w + Q_{cal} $$ $$ Q_{gain} = 8.16\times10^3 + 1.36\times10^3 $$ $$ Q_{gain} = 9.52\times10^3\ \text{J} $$
Step-4: Heat lost by metal
Let the specific heat of the metal be \(c\). $$ Q_{metal} = mc\Delta T $$ $$ Q_{metal} = 200 \times c \times 110 $$ $$ Q_{metal} = 2.2\times10^4 c $$
Step-5: Apply heat balance
$$ 2.2\times10^4 c = 9.52\times10^3 $$ $$ c = \frac{9.52\times10^3}{2.2\times10^4} $$ $$ c \approx 0.433\ \text{J g}^{-1}\text{K}^{-1} $$
Final Answer
Specific heat of the metal: $$ \boxed{c \approx 0.43\ \text{J g}^{-1}\text{K}^{-1}} $$ or $$ \boxed{c \approx 430\ \text{J kg}^{-1}\text{K}^{-1}} $$
Effect of Heat Loss

If heat is lost to the surroundings, part of the heat released by the metal does not heat the water and calorimeter. Therefore the calculated heat gain becomes smaller.

Hence the calculated value of \(c\) becomes smaller than the true value.


Conceptual Illustration
Hot Metal Water + Calorimeter Heat Flow

Heat flows from the hot metal to the water and calorimeter until thermal equilibrium is reached.

Progress: Question 14 of 20

Q15 Given below are observations on molar specific heats at room temperature of some common gases.

Gas Molar specific heat \(C_v\) (cal mol\(^{-1}\) K\(^{-1}\))
Hydrogen 4.87
Nitrogen 4.97
Oxygen 5.02
Nitric oxide 4.99
Carbon monoxide 5.01
Chlorine 6.17

The measured molar specific heats of these gases are markedly different from those for monatomic gases. Typically, the molar specific heat of a monatomic gas is 2.92 cal mol\(^{-1}\) K\(^{-1}\). Explain this difference. What can you infer from the somewhat larger value for chlorine?

Solution
Brief Theory: Equipartition of Energy

According to the equipartition theorem, each degree of freedom contributes \(\tfrac{1}{2}R\) per mole to the molar specific heat at constant volume.

Thus, if a molecule has \(f\) degrees of freedom,

$$ C_v = \frac{f}{2}R $$
Monatomic Gases

A monatomic gas atom can move only in three perpendicular directions (translational motion).

Number of degrees of freedom: $$ f = 3 $$ Therefore, $$ C_v = \frac{3}{2}R $$ Using \(R = 1.987\ \text{cal mol}^{-1}\text{K}^{-1}\): $$ C_v = \frac{3}{2} \times 1.987 $$ $$ C_v \approx 2.98\ \text{cal mol}^{-1}\text{K}^{-1} $$ which is close to the observed value \(2.92\).
Diatomic Gases

Diatomic molecules have additional rotational motion.

Active degrees of freedom at room temperature:
  • 3 translational
  • 2 rotational
Total: $$ f = 5 $$ Thus, $$ C_v = \frac{5}{2}R $$ $$ C_v = \frac{5}{2} \times 1.987 $$ $$ C_v \approx 4.97\ \text{cal mol}^{-1}\text{K}^{-1} $$

This agrees well with the observed values for H\(_2\), N\(_2\), O\(_2\), NO, and CO.


Why Chlorine Has a Larger Value

The molar specific heat of chlorine is slightly larger (\(6.17\ \text{cal mol}^{-1}\text{K}^{-1}\)).

This suggests that at room temperature some vibrational degrees of freedom are also partially excited in chlorine molecules.

Vibrational motion adds additional energy storage, increasing the molar specific heat.


Final Inference
  • The difference from monatomic gases arises because diatomic molecules have additional rotational degrees of freedom.
  • The higher value for chlorine indicates the onset of vibrational motion in addition to translation and rotation.

Conceptual Illustration
Translational Motion Rotational Motion Vibrational Motion Degrees of freedom increase internal energy → larger molar specific heat
Progress: Question 15 of 20

Q16 A child running a temperature of 101°F is given an antipyrin (a medicine that lowers fever) which increases the rate of evaporation of sweat from the body. If the fever falls to 98°F in 20 minutes, what is the average rate of extra evaporation caused by the drug? Assume evaporation is the only way heat is lost. Mass of child = 30 kg. Specific heat of human body ≈ specific heat of water. Latent heat of evaporation of water = 580 cal g\(^{-1}\).

Solution
Brief Theory

Human bodies cool mainly through evaporation of sweat. When sweat evaporates, it absorbs latent heat from the body, thereby lowering body temperature.

Heat required for evaporation: $$ Q = mL $$ Heat lost due to temperature fall: $$ Q = mc\Delta T $$
Given Data
  • Mass of child \(m = 30\ \text{kg} = 3.0\times10^4\ \text{g}\)
  • Initial temperature \(=101^\circ F\)
  • Final temperature \(=98^\circ F\)
  • Specific heat of body \(c \approx 1\ \text{cal g}^{-1}\text{K}^{-1}\)
  • Latent heat \(L = 580\ \text{cal g}^{-1}\)
  • Time \(t = 20\ \text{min}\)

Step-1: Temperature fall in Celsius
Temperature change: $$ \Delta T = 101 - 98 = 3^\circ F $$ Using $$ 1^\circ F = \frac{5}{9}^\circ C $$ $$ \Delta T = \frac{5}{9} \times 3 $$ $$ \Delta T \approx 1.67^\circ C $$
Step-2: Heat lost by the body
$$ Q = mc\Delta T $$ $$ Q = (3.0\times10^4)(1)(1.67) $$ $$ Q \approx 5.01\times10^4\ \text{cal} $$
Step-3: Mass of sweat evaporated
Using $$ Q = mL $$ $$ 5.01\times10^4 = m \times 580 $$ $$ m = \frac{5.01\times10^4}{580} $$ $$ m \approx 86.4\ \text{g} $$
Step-4: Average rate of evaporation
$$ \text{Rate} = \frac{m}{t} $$ $$ \text{Rate} = \frac{86.4}{20} $$ $$ \text{Rate} \approx 4.32\ \text{g min}^{-1} $$
Final Answer

Average rate of extra evaporation caused by the drug:

$$ \boxed{ \approx 4.3\ \text{g min}^{-1} } $$
Conceptual Illustration
Human Body Heat removed Evaporation of sweat absorbs latent heat → body cools

Evaporation of sweat removes heat from the body because latent heat is required to convert liquid sweat into vapour.

Progress: Question 16 of 20

Q17 A ‘thermacole’ icebox is a cheap and efficient method for storing small quantities of cooked food in summer. A cubical icebox of side 30 cm has a thickness of 5.0 cm. If 4.0 kg of ice is put in the box, estimate the amount of ice remaining after 6 h. Outside temperature = \(45^\circ C\) Thermal conductivity of thermacole \(k = 0.01\ \text{J s}^{-1}\text{m}^{-1}\text{K}^{-1}\) Heat of fusion of ice \(L = 335 \times 10^3\ \text{J kg}^{-1}\)

Solution
Brief Theory

Heat flows through the walls of the icebox by thermal conduction. The rate of heat transfer through a slab is given by

$$ \frac{Q}{t} = \frac{kA\Delta T}{x} $$ where
  • \(k\) = thermal conductivity
  • \(A\) = surface area through which heat flows
  • \(\Delta T\) = temperature difference
  • \(x\) = thickness of the material
The heat entering the box melts some of the ice.
Given Data
  • Inner side of icebox \(=30\ \text{cm}=0.30\ \text{m}\)
  • Wall thickness \(=5\ \text{cm}=0.05\ \text{m}\)
  • Outside temperature \(=45^\circ C\)
  • Inside temperature \(\approx 0^\circ C\)
  • \(k=0.01\ \text{J s}^{-1}\text{m}^{-1}\text{K}^{-1}\)
  • Initial ice mass \(=4.0\ \text{kg}\)
  • Time \(t=6\ \text{h}=21600\ \text{s}\)

Step-1: Outer dimensions of the icebox
$$ L_{outer} = 30 + 2\times5 $$ $$ L_{outer} = 40\ \text{cm} = 0.40\ \text{m} $$
Step-2: Surface area for heat flow
Heat flows through all six faces of the cube: $$ A = 6L_{outer}^2 $$ $$ A = 6(0.40)^2 $$ $$ A = 0.96\ \text{m}^2 $$
Step-3: Rate of heat conduction
Temperature difference: $$ \Delta T = 45 - 0 = 45\ K $$ Using the conduction formula: $$ \frac{Q}{t} = \frac{kA\Delta T}{x} $$ $$ \frac{Q}{t} = \frac{0.01 \times 0.96 \times 45}{0.05} $$ $$ \frac{Q}{t} = 8.64\ \text{J s}^{-1} $$
Step-4: Total heat entering in 6 hours
$$ Q = 8.64 \times 21600 $$ $$ Q \approx 1.87\times10^5\ \text{J} $$
Step-5: Ice melted
Using $$ Q = mL $$ $$ m = \frac{Q}{L} $$ $$ m = \frac{1.87\times10^5}{335\times10^3} $$ $$ m \approx 0.56\ \text{kg} $$
Step-6: Ice remaining
$$ m_{remaining} = 4.0 - 0.56 $$ $$ m_{remaining} = 3.44\ \text{kg} $$
Final Answer
Amount of ice remaining after 6 h: $$ \boxed{3.44\ \text{kg} \approx 3.4\ \text{kg}} $$
Conceptual Illustration
Thermacole Icebox Ice inside (0°C) Heat flow 45°C outside

Heat from the hot surroundings slowly conducts through the thermacole walls and melts part of the ice inside the box.

Progress: Question 17 of 20

Q18 A brass boiler has a base area of 0.15 m² and thickness 1.0 cm. It boils water at the rate of 6.0 kg/min when placed on a gas stove. Estimate the temperature of the part of the flame in contact with the boiler. Thermal conductivity of brass \(k = 109\ \text{J s}^{-1}\text{m}^{-1}\text{K}^{-1}\) Heat of vaporisation of water \(L = 2256 \times 10^{3}\ \text{J kg}^{-1}\)

Solution
A brass boiler has a base area of 0.15 m² and thickness 1.0 cm. It boils water at the rate of 6.0 kg/min when placed on a gas stove. Estimate the temperature of the part of the flame in contact with the boiler.
Thermal conductivity of brass \[k = 109\ \text{J s}^{-1}\text{m}^{-1}\text{K}^{-1}\] Heat of vaporisation of water \[L = 2256 \times 10^{3}\ \text{J kg}^{-1}\]
Progress: Question 18 of 20

Q19 Explain why :
(a) a body with large reflectivity is a poor emitter
(b) a brass tumbler feels much colder than a wooden tray on a chilly day
(c) an optical pyrometer calibrated for an ideal black body gives too low a value for the temperature of a red-hot iron piece in the open, but gives the correct temperature when the same piece is in a furnace
(d) the earth without its atmosphere would be inhospitably cold
(e) heating systems based on circulation of steam are more efficient in warming a building than those based on circulation of hot water

Solution
Brief Theory

Thermal radiation and heat transfer depend on properties such as emissivity, absorptivity, reflectivity, thermal conductivity, and latent heat. Kirchhoff’s law of radiation states that good absorbers are also good emitters at a given temperature.


(a) A body with large reflectivity is a poor emitter

If a body reflects most of the radiation incident on it, it absorbs very little energy. According to Kirchhoff’s law of thermal radiation,

$$ \text{Good absorber} \Rightarrow \text{Good emitter} $$

Therefore, a body that absorbs little radiation (high reflectivity) also emits little radiation, making it a poor emitter.


(b) Brass tumbler feels colder than a wooden tray

Although both objects may be at the same temperature, brass is a good conductor of heat while wood is a poor conductor.

  • Brass rapidly draws heat from the hand → skin cools quickly → strong cold sensation.
  • Wood removes heat slowly → weaker cooling sensation.
Wood (Poor conductor) Brass (Good conductor) Heat flows faster
(c) Optical pyrometer reading error

An optical pyrometer determines temperature by comparing radiation intensity with that of an ideal black body.

  • A red-hot iron piece in open air is not a perfect black body.
  • Its emissivity is less than 1 → it emits less radiation than a black body.
  • The pyrometer therefore interprets the radiation as a lower temperature.

Inside a furnace, multiple reflections make the object behave almost like a black body, so the pyrometer reads the correct temperature.


(d) Earth without atmosphere would be extremely cold

The atmosphere absorbs part of the infrared radiation emitted by the earth and re-radiates it back to the surface.

This greenhouse effect reduces heat loss to space. Without the atmosphere:

  • Most heat would escape directly into space.
  • Night temperatures would drop drastically.

Hence the earth would become extremely cold and unsuitable for life.


(e) Steam heating systems are more efficient

Steam releases a large amount of heat when it condenses into water. This heat is called latent heat of condensation.

  • Steam carries large thermal energy.
  • During condensation it releases latent heat efficiently.
  • This transfers more heat to the surroundings than hot water.
Steam Condenses Condensation releases large latent heat → better heating
Progress: Question 19 of 20

Q20 A body cools from 80 °C to 50 °C in 5 minutes. Calculate the time it takes to cool from 60 °C to 30 °C. The temperature of the surroundings is 20 °C.

Solution
Brief Theory

According to Newton’s law of cooling, the rate of loss of heat of a body is proportional to the difference between its temperature and the surrounding temperature.

Mathematically, $$ T - T_s = (T_0 - T_s)e^{-kt} $$ where
  • \(T\) = temperature at time \(t\)
  • \(T_s\) = surrounding temperature
  • \(T_0\) = initial temperature
  • \(k\) = cooling constant

Given Data
  • Initial temperature \(T_0 = 80^\circ C\)
  • Temperature after 5 min = \(50^\circ C\)
  • Surrounding temperature \(T_s = 20^\circ C\)

Step-1: Determine the cooling constant \(k\)
Using $$ T - T_s = (T_0 - T_s)e^{-kt} $$ Substitute \(t=5\) min: $$ 50 - 20 = (80 - 20)e^{-5k} $$ $$ 30 = 60e^{-5k} $$ $$ e^{-5k} = \frac{1}{2} $$ Taking natural logarithm, $$ -5k = \ln\!\left(\frac12\right) $$ $$ k = \frac{\ln 2}{5} $$
Step-2: Cooling from \(60^\circ C\) to \(30^\circ C\)
Let time required be \(t\). $$ 30 - 20 = (60 - 20)e^{-kt} $$ $$ 10 = 40e^{-kt} $$ $$ e^{-kt} = \frac{1}{4} $$ Taking logarithm, $$ -kt = \ln\!\left(\frac14\right) = -\ln4 $$ $$ t = \frac{\ln4}{k} $$
Step-3: Substitute value of \(k\)
$$ k = \frac{\ln2}{5} $$ $$ t = \frac{\ln4}{\ln2/5} $$ $$ t = \frac{2\ln2}{\ln2/5} $$ $$ t = 10\ \text{minutes} $$
Final Answer
$$ \boxed{t = 10\ \text{minutes}} $$
Conceptual Illustration
Time Temperature 80°C 50°C 30°C Surroundings 20°C

The temperature difference between the body and surroundings decreases exponentially with time according to Newton’s law of cooling.

Progress: Question 20 of 20
Top

🧠 Exam Concept Snapshot

Calorimetry Heat Lost = Heat Gained
Newton Cooling $$T-T_s=(T_0-T_s)e^{-kt}$$
Latent Heat $$Q=mL$$

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    Frequently Asked Questions

    Temperature is a measure of the degree of hotness or coldness of a body and determines the direction of heat flow.

    Heat is a form of energy transferred from one body to another due to a temperature difference.

    No

    Thermal equilibrium is the state in which bodies in contact attain the same temperature and no net heat transfer occurs.

    If two systems are each in thermal equilibrium with a third system

    It forms the basis of temperature measurement and the construction of thermometers.

    Thermal expansion is the increase in dimensions of a substance when its temperature rises.

    Linear expansion

    It is the fractional change in length per unit original length per unit rise in temperature.

    Change in length is given by \( \Delta L = L_0 \alpha \Delta T \).

    Areal expansion is the increase in surface area of a solid due to rise in temperature.

    Volumetric expansion is the increase in volume of a substance with temperature.

    For isotropic solids

    To allow thermal expansion and prevent buckling during high temperatures.

    Water contracts on heating from \(0^\circ\text{C}\) to \(4^\circ\text{C}\) and expands beyond \(4^\circ\text{C}\).

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