One-dimensional steady conduction and thermal resistance

Fourier's law, thermal resistance networks for plane, cylindrical and spherical layers with convection, overall U, contact resistance and the critical radius of insulation, with worked numericals.

Drafted with Aria, reviewed by the AiCanCode.org team. Spotted an error? Use Give Feedback at the bottom of the page.

Why it matters

Heat leaking through a car's roof and doors loads the air-conditioner; heat flowing through cylinder liners, exhaust pipes, brake pads and battery-pack walls decides their temperatures. The thermal-resistance network turns all of these into simple series and parallel circuits, and it is the backbone of every steady heat-transfer problem in GATE, including fins, heat exchangers and insulation.

Key ideas

Fourier's law. The conduction heat flux is proportional to the temperature gradient and flows from hot to cold: q″ = −k dT/dx. The minus sign makes heat flow positive in the direction of decreasing temperature. Thermal conductivity k (W/m·K) ranges from about 400 for copper, around 45–50 for carbon steel, about 1 for glass, down to 0.03–0.05 for insulation foams.

One-dimensional, steady. "Steady" means temperatures do not change with time; "one-dimensional" means temperature varies in one coordinate only (x for a wall, r for a pipe or sphere). With no heat generation and constant k:

  • In a plane wall the temperature profile is linear and the heat rate is the same at every x.
  • In a cylinder or sphere the heat rate is constant with r but the flux falls as area grows, so the profile is logarithmic (cylinder) or hyperbolic (sphere), not linear.

Thermal resistance. Since Q = ΔT/R, every mode of heat transfer can be written as a resistance (K/W):

  • Conduction through a plane wall: L/(kA).
  • Convection at a surface: 1/(hA).
  • Radiation (linearised): 1/(h_r A). Layers in series add their resistances; parallel paths (for example a stud and the insulation beside it) combine like parallel resistors. The same heat rate passes through each series layer, so the largest temperature drop occurs across the largest resistance.

Overall heat transfer coefficient. For a wall between two fluids, U = 1/(R_total A), so Q = U A ΔT_overall. For a pipe, U must be referred to a specific area (inner or outer).

Contact resistance. Real surfaces touch only at asperities, so a joint adds a resistance R″_c (m²·K/W) that depends on pressure, roughness and interface material. Thermal paste in electronics and battery modules reduces it. Values come from data books.

Critical radius of insulation. Adding insulation to a small pipe or wire increases the conduction resistance but also increases the outer surface area, lowering the convection resistance. Heat loss is maximum when the outer radius equals r_c = k/h (cylinder) or 2k/h (sphere). For pipes with r_o > r_c insulation always reduces heat loss; for thin electric wires, a coating up to r_c actually helps cooling.

Variable conductivity. If k = k₀(1 + βT), the plane-wall result still holds with k evaluated at the mean temperature.

Formulas

Q = −k A dT/dx — Q: heat rate, W; k: W/m·K; A: area normal to flow, m²; dT/dx: K/m.

R_wall = L / (k A) — plane wall of thickness L (m).

R_conv = 1 / (h A) — h: convection coefficient, W/m²·K.

R_cyl = ln(r₂/r₁) / (2π k L) — cylindrical shell, length L (m).

R_sph = (r₂ − r₁) / (4π k r₁ r₂) — spherical shell.

Q = (T_∞1 − T_∞2) / ΣR — series network.

1/R_parallel = 1/R_a + 1/R_b — parallel paths.

U = 1 / (A ΣR) — W/m²·K; for a plane wall per unit area: 1/U = 1/h₁ + Σ L/k + 1/h₂.

r_c = k / h (cylinder), r_c = 2k / h (sphere) — critical radius of insulation, m.

k_m = k₀ [1 + β (T₁ + T₂)/2] — mean conductivity for linearly varying k.

Worked examples

Example 1 (standard, composite car door). A door panel consists of 1 mm steel (k = 45 W/m·K), 20 mm foam insulation (k = 0.04 W/m·K) and 5 mm plastic trim (k = 0.2 W/m·K). Outside air is at 45 °C with h = 25 W/m²·K (moving vehicle); cabin air is at 25 °C with h = 8 W/m²·K. Find the heat gain per m² and the U value. Neglect radiation and contact resistance.

  1. Resistances per m² (A = 1 m²): outside convection 1/25 = 0.0400; steel 0.001/45 = 0.00002; foam 0.020/0.04 = 0.5000; trim 0.005/0.2 = 0.0250; inside convection 1/8 = 0.1250 K/W.
  2. ΣR = 0.0400 + 0.00002 + 0.5000 + 0.0250 + 0.1250 = 0.6900 K/W.
  3. Q = ΔT/ΣR = (45 − 25)/0.6900 = 29.0 W per m².
  4. U = 1/ΣR = 1.45 W/m²·K.
  5. Temperature drop across the foam = 29.0 × 0.5 = 14.5 K, about 72% of the total; the steel's drop is negligible (0.0006 K). Insulation dominates, so adding steel thickness is pointless.

Example 2 (GATE level, insulated pipe). A steel pipe (k = 45 W/m·K) of inner radius 25 mm and outer radius 30 mm carries a fluid at 150 °C (h_i = 500 W/m²·K). It is covered with 20 mm of insulation (k = 0.06 W/m·K) and exposed to air at 30 °C (h_o = 10 W/m²·K). Find the heat loss per metre, the outer surface temperature, and the loss if the pipe were bare.

  1. Inside convection: 1/(h_i 2π r_i L) = 1/(500 × 2π × 0.025 × 1) = 0.01273 K/W.
  2. Pipe wall: ln(r₂/r₁)/(2πkL) = ln(30/25)/(2π × 45) = 0.00064 K/W.
  3. Insulation: ln(50/30)/(2π × 0.06) = 1.35501 K/W.
  4. Outside convection: 1/(10 × 2π × 0.05) = 0.31831 K/W.
  5. ΣR = 1.68669 K/W; Q = (150 − 30)/1.68669 = 71.1 W per metre.
  6. Outer surface temperature = 30 + 71.1 × 0.31831 = 52.6 °C.
  7. Bare pipe: outside resistance 1/(10 × 2π × 0.03) = 0.53052 K/W; Q = 120/(0.01273 + 0.00064 + 0.53052) = 220.6 W/m. Insulation cuts the loss by about 68%.
  8. Critical radius r_c = k/h = 0.06/10 = 6 mm, far below the 30 mm pipe, so any thickness of this insulation reduces heat loss.

Common mistakes

  • Using the plane-wall formula L/(kA) for a thick pipe; use ln(r₂/r₁)/(2πkL).
  • Dropping the convection resistances, which are often the largest terms.
  • Using diameters inside ln when the formula has radii (the ratio is the same, but mixing a diameter with a radius is not).
  • Applying the critical-radius idea to large pipes, where insulation always helps.
  • Forgetting that the heat rate, not the heat flux, is constant through cylindrical layers.
  • Mixing mm and m in L/k.

For GATE ME

Expect composite-wall and composite-cylinder numericals (heat rate, interface temperatures, overall U), critical radius of insulation and the effect of adding insulation to a wire or pipe, walls with variable conductivity, and MCQs on temperature profiles in walls, cylinders and spheres. Practise drawing the resistance network first; most errors come from leaving out a resistance.

Quick check

  1. What is the resistance of a 0.1 m thick wall with k = 0.5 W/m·K and area 2 m²?
  2. In a composite wall, which layer has the largest temperature drop?
  3. A wire has k_insulation = 0.2 W/m·K and h = 10 W/m²·K. What is the critical radius?
  4. Is the steady temperature profile in a cylindrical shell linear?

Answers: 1. 0.1/(0.5 × 2) = 0.1 K/W. 2. The one with the largest thermal resistance. 3. 0.2/10 = 0.02 m = 20 mm. 4. No, it is logarithmic in r.

Try answering each one aloud before you open it.

  1. 1.What is one-dimensional steady conduction?Concept

    Steady means temperatures at every point do not change with time; one-dimensional means temperature varies in only one coordinate, such as x through a large wall or r through a long pipe. Then the heat rate through each layer is constant. With constant conductivity and no heat generation, the temperature profile is linear in a plane wall, logarithmic in a cylinder and hyperbolic (varying as 1/r) in a sphere, because the area changes with radius. With heat generation or variable conductivity, the profile curves even in a plane wall.

  2. 2.Explain the concept of thermal resistance in the context of heat conduction.Concept

    Thermal resistance is a measure of a material's ability to resist the flow of heat. It is analogous to electrical resistance in circuits. In the context of heat conduction, thermal resistance is calculated as the ratio of the temperature difference across the material to the heat transfer rate. It is expressed in units of K/W (Kelvin per Watt).

  3. 3.How is the thermal resistance of a plane wall calculated?Concept

    The thermal resistance of a plane wall is calculated using the formula R = L / (k·A), where R is the thermal resistance, L is the thickness of the wall, k is the thermal conductivity of the material, and A is the cross-sectional area perpendicular to the heat flow.

  4. 4.Why is thermal conductivity important in determining thermal resistance?Application

    Thermal conductivity is a material property that indicates how well a material can conduct heat. It is a key factor in determining thermal resistance because it directly affects how easily heat can pass through a material. A higher thermal conductivity means lower thermal resistance, allowing more heat to flow through the material.

  5. 5.What happens to the thermal resistance if the thickness of a material is doubled?Application

    If the thickness of a material is doubled, the thermal resistance also doubles. This is because thermal resistance is directly proportional to the thickness of the material, as given by the formula R = L / (k·A). Doubling L results in doubling R, assuming thermal conductivity and area remain constant.

  6. 6.Explain why metals generally have lower thermal resistance compared to non-metals.Application

    Metals generally have lower thermal resistance compared to non-metals because they have higher thermal conductivity. The free electrons in metals facilitate the transfer of heat, allowing them to conduct heat more efficiently. This results in lower thermal resistance, making metals good conductors of heat.

  7. 7.How does the concept of thermal resistance apply to composite walls?Application

    In composite walls, which consist of multiple layers of different materials, the total thermal resistance is the sum of the thermal resistances of each layer. This is similar to resistors in series in an electrical circuit. The overall heat transfer rate is determined by the total thermal resistance, which accounts for the resistance of each material layer.

  8. 8.Calculate the thermal resistance of a wall with a thickness of 0.1 m, a thermal conductivity of 0.5 W/m·K, and a cross-sectional area of 10 m².Numerical

    To calculate the thermal resistance, use the formula R = L / (k·A). Here, L = 0.1 m, k = 0.5 W/m·K, and A = 10 m². Therefore, R = 0.1 / (0.5 × 10) = 0.1 / 5 = 0.02 K/W.

  9. 9.A composite wall consists of two layers: one with a thermal resistance of 0.1 K/W and another with 0.2 K/W. What is the total thermal resistance of the wall?Numerical

    The total thermal resistance of a composite wall is the sum of the thermal resistances of each layer. Therefore, the total thermal resistance is 0.1 K/W + 0.2 K/W = 0.3 K/W.

  10. 10.What is the effect of increasing the cross-sectional area on the thermal resistance of a material?Application

    Increasing the cross-sectional area of a material decreases its thermal resistance. This is because thermal resistance is inversely proportional to the area, as given by the formula R = L / (k·A). A larger area allows more heat to flow through, reducing the resistance to heat flow.

Finished this topic? Mark it so your progress, study plan and readiness keep up.

Stuck on something here?