EEngiGrind
← All problems
MechanicalHeat TransfermediumFE ExamCoursework

Heat Flow Through a Composite Wall

A wall of area A=1.0 m2A = 1.0\ \text{m}^2 consists of two layers in series:

  • Brick: 200 mm200\ \text{mm} thick, k=0.70 W/m⋅Kk = 0.70\ \text{W/m·K}
  • Insulation: 50 mm50\ \text{mm} thick, k=0.040 W/m⋅Kk = 0.040\ \text{W/m·K}

The temperature difference across the whole wall is ΔT=25 K\Delta T = 25\ \text{K}. Neglect surface convection resistances.

Find the rate of heat transfer through the wall.

Given
L1200 mmBrick thickness
k10.7 W/m*KBrick conductivity
L250 mmInsulation thickness
k20.04 W/m*KInsulation conductivity
ΔT25 KOverall temperature difference
Hint 1

Treat this as a resistance network: layers in series add.

Hint 2

Thermal resistance of a slab is R = L/(kA).

Hint 3

Convert thicknesses to metres, then Q = ΔT/R_total.

Worked solution — try the problem first

Layers in series add their thermal resistances, exactly like resistors in a circuit:

R=LkA,Rtotal=R1+R2,Q=ΔTRtotalR = \frac{L}{kA}, \qquad R_{total} = R_1 + R_2, \qquad Q = \frac{\Delta T}{R_{total}}

Brick: R1=0.2000.70×1.0=0.2857 K/WR_1 = \frac{0.200}{0.70 \times 1.0} = 0.2857\ \text{K/W}

Insulation: R2=0.0500.040×1.0=1.250 K/WR_2 = \frac{0.050}{0.040 \times 1.0} = 1.250\ \text{K/W}

Total: Rtotal=0.2857+1.250=1.5357 K/WR_{total} = 0.2857 + 1.250 = 1.5357\ \text{K/W}

Heat flow: Q=251.5357=16.28 WQ = \frac{25}{1.5357} = 16.28\ \text{W}

Q=16.3 W\boxed{Q = 16.3\ \text{W}}

Note the dominance of the insulation. At one quarter the thickness, it contributes 81% of the total resistance — because its conductivity is 17.5× lower. This is why a thin insulating layer transforms a wall's performance.

Concepts:ConductionThermal resistanceComposite wallsFourier's law

Sign in to submit

Grading needs an account so your progress, attempts, and daily quota can be tracked. The problem statement and worked solution stay open to everyone.

Create an account