EduKG
← Back

Conduction convection and radiation

Learning objectives

  • Outcome

    Classify everyday situations by the dominant heat-transfer mechanism: conduction, convection, or radiation.

  • Outcome

    Calculate the heat passing through a flat wall using Fourier's law Q=λAΔTtdQ = \frac{\lambda A \Delta T t}{d}.

  • Outcome

    Explain with a microscopic model why conduction and convection require matter, while radiation can occur in a vacuum.

  • Outcome

    Compare heat-transfer rates for two configurations (e.g., single vs double glazing) and justify the conclusion with an equation.

Understand the idea

Heat transfer: conduction, convection, and radiation

Text

Heat transfer is the transport of internal energy from a body at higher temperature to one at lower temperature.

Conduction occurs through the interaction and collisions of particles of matter, so it is possible in solids, liquids, and gases but not in a vacuum. The heat passing through a flat wall is described by Fourier's law:

Q=λAΔTtd,Q = \frac{\lambda A \Delta T t}{d},

where λ\lambda is the thermal conductivity, AA is the area, dd is the thickness, and tt is the time.

Convection is energy transport by flows of liquid or gas that arise because of density differences between heated and cooler layers; it is possible only in fluids. Radiation is energy transport by electromagnetic waves, which needs no medium and can occur in a vacuum; for example, the Sun's energy reaches Earth through space. In real processes these mechanisms often act simultaneously, but one may dominate.

Worked examples

Direct

Problem

Heat passes through a window pane of area A=1.5 m2A = 1.5\ \text{m}^2 and thickness d=4 mmd = 4\ \text{mm}. The temperature difference between the inner and outer surfaces is ΔT=20 K\Delta T = 20\ \text{K}, and the thermal conductivity of glass is λ=0.8 W/(m⋅K)\lambda = 0.8\ \text{W/(m·K)}. How much heat passes through the pane in t=1 ht = 1\ \text{h}? Assume a steady process.

Solution

Use Fourier's law for conduction:

Q=λAΔTtd.Q = \frac{\lambda A \Delta T t}{d}.

Convert the data to SI: d=4 mm=0.004 md = 4\ \text{mm} = 0.004\ \text{m}, t=1 h=3600 st = 1\ \text{h} = 3600\ \text{s}.
Substitute the values:

Q=0.8⋅1.5⋅20⋅36000.004.Q = \frac{0.8 \cdot 1.5 \cdot 20 \cdot 3600}{0.004}.

Calculate:

0.8⋅1.5=1.2,1.2⋅20=24,24⋅3600=86 400,86 4000.004=21 600 000.0.8 \cdot 1.5 = 1.2,\quad 1.2 \cdot 20 = 24,\quad 24 \cdot 3600 = 86\,400,\quad \frac{86\,400}{0.004} = 21\,600\,000.

Answer: Q=2.16⋅107 JQ = 2.16 \cdot 10^7\ \text{J} (or 21.6 MJ21.6\ \text{MJ}).

Application

Problem

A house wall has area A=20 m2A = 20\ \text{m}^2, thickness d=0.25 md = 0.25\ \text{m}, and thermal conductivity λ=0.7 W/(m⋅K)\lambda = 0.7\ \text{W/(m·K)}. The inside temperature is t1=20 ∘Ct_1 = 20\ ^\circ\text{C} and the outside temperature is t2=−10 ∘Ct_2 = -10\ ^\circ\text{C}. Find the heat-loss power due to conduction alone. Explain why the real losses may be larger.

Solution

Temperature difference: ΔT=20−(−10)=30 K\Delta T = 20 - (-10) = 30\ \text{K}.
For steady-state conduction, the power is

P=Qt=λAΔTd.P = \frac{Q}{t} = \frac{\lambda A \Delta T}{d}.

Substitute:

P=0.7⋅20⋅300.25=1680 W.P = \frac{0.7 \cdot 20 \cdot 30}{0.25} = 1680\ \text{W}.

This estimates the conduction power through the wall if the 30 K30\ \text{K} temperature difference applies to the wall surfaces. If 20 ∘C20\ ^\circ\text{C} and −10 ∘C-10\ ^\circ\text{C} are air temperatures, then convection and radiation occur at the wall surfaces. In steady state, these surface processes do not add in parallel to conduction through the wall; they are in series, and the same heat flux passes through the surface films and the wall. Therefore, part of the temperature difference is taken up by the surface films, the wall-surface temperatures differ from the air temperatures, and using the full air temperature difference of 30 K30\ \text{K} gives an upper-bound estimate for conduction through the wall, not a lower bound. Real heat losses can be larger because of thermal bridges, air leakage, windows, ventilation, and other loss paths.

Transfer

Problem

A spacecraft is in a vacuum and generates internal power P=500 WP = 500\ \text{W}. The outer surface area is A=2 m2A = 2\ \text{m}^2, and the emissivity is ε=0.8\varepsilon = 0.8. Describe which heat-transfer mechanisms can remove heat from the spacecraft and which are impossible. Estimate the equilibrium surface temperature if it radiates to deep space, taking the space temperature to be close to 0 K0\ \text{K}. Use P=εσAT4P = \varepsilon \sigma A T^4, σ=5.67⋅10−8 W/(m2⋅K4)\sigma = 5.67 \cdot 10^{-8}\ \text{W/(m}^2\text{·K}^4).

Solution

In a vacuum, conduction and convection are impossible because there is no matter to carry energy by collisions or flows. Only radiation remains: the surface emits electromagnetic waves.
From the balance condition Prad=PP_{\text{rad}} = P:

εσAT4=P.\varepsilon \sigma A T^4 = P.

Therefore,

T=(PεσA)1/4.T = \left(\frac{P}{\varepsilon \sigma A}\right)^{1/4}.

Substitute:

T=(5000.8⋅5.67⋅10−8⋅2)1/4=(5.51⋅109)1/4≈272 K.T = \left(\frac{500}{0.8 \cdot 5.67 \cdot 10^{-8} \cdot 2}\right)^{1/4} = \left(5.51 \cdot 10^9\right)^{1/4} \approx 272\ \text{K}.

This is about −1 ∘C-1\ ^\circ\text{C}. In practice, one must also account for absorbed solar radiation and Earth's thermal radiation.

Practice

Text

Safe self-study investigation.

Simulation: open an interactive heat-transfer model (e.g., PhET “Heat Transfer” or similar) and observe how heat spreads through a solid, how a convection loop forms in a fluid, and how radiation carries energy through a vacuum. For each mechanism, record: (1) whether a medium is needed, (2) what carries the energy, (3) how the temperature difference affects it.

Safe home experiment: pour warm (not boiling) water into two identical mugs. Wrap one in light paper and the other in dark paper. Measure the temperature after 5 and 10 minutes. Explain why the dark surface may cool differently. Do not use boiling water or an open flame.

Visual reference

Purpose

Show the three heat-transfer mechanisms side by side and highlight their key differences: the need for a medium, the microscopic energy carrier, and the role of temperature difference.

Representation

A three-panel diagram.

Left: a metal rod heated at one end; particles are shown as circles with vibration arrows, and collision arrows go from the hot end to the cold end. Label: “conduction, Q=λAΔTtdQ = \frac{\lambda A \Delta T t}{d}”.

Center: a vessel with liquid; near the heater at the bottom the liquid rises, and near the cold wall it sinks, forming a closed loop with arrows. Label: “convection, only in a fluid”.

Right: the Sun, with wavy arrows through empty space (vacuum) to Earth. Label: “radiation, no medium needed”.

Real-world examples

Hot spoon in a pot

Scenario

While soup is boiling, the water in the pot is at about 100 ∘C100\ ^\circ\text{C}. A metal spoon left in the pot heats up so that after 2 min2\ \text{min} the handle near the upper end reaches 45 ∘C45\ ^\circ\text{C}, even though the kitchen air is only 22 ∘C22\ ^\circ\text{C}.

Connection

Heat from the hot water is transferred to the spoon by conduction: rapid atomic vibrations and free electrons in the metal pass internal energy along the spoon. In the water itself, convection operates: heated layers rise and cooler layers sink. Radiation from the stove and water also warms nearby surfaces.

Smartphone heating during gaming

Scenario

A smartphone draws 5 W5\ \text{W} while gaming and warms to 42 ∘C42\ ^\circ\text{C} at a room temperature of 22 ∘C22\ ^\circ\text{C}. Its aluminium body with area 0.01 m20.01\ \text{m}^2 transfers heat to the air; without this removal the chip temperature would exceed 80 ∘C80\ ^\circ\text{C}.

Connection

Inside the phone, heat moves by conduction from the chip to the case. From the case surface, energy is carried away by convection: air near the warm surface becomes less dense and rises, while cooler air takes its place. Part of the energy leaves by radiation in the infrared range because the case is warmer than the room.

Thermos with tea

Scenario

Tea at 90 ∘C90\ ^\circ\text{C} is poured into a thermos; after 4 h4\ \text{h} its temperature drops to 70 ∘C70\ ^\circ\text{C} at a kitchen temperature of 20 ∘C20\ ^\circ\text{C}. The glass flask has double silvered walls, and the air between them is pumped out.

Connection

The vacuum between the walls almost eliminates conduction and convection: there are few particles to transfer energy or form flows. The silver coating reduces radiation by reflecting infrared waves back toward the tea. The remaining heat loss occurs through the stopper and thin walls.