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Heat transfer and thermal systems

Resistance of a hollow sphere

Thermal resistance of a complete spherical shell with inner radius ri and outer radius ro, for steady radial conduction with constant conductivity k and no internal generation.

Ref
HTS-01
Rev
v1
Field
Heat transfer and thermal systems
Result
R [K/W]

Radial conduction through a complete spherical shell has a resistance R = (1/ri − 1/ro)/(4πk). It is the sphere equivalent of the plane-wall L/(kA), with the area growing as r². The resistance approaches a finite limit, 1/(4πk ri), as the outer radius grows, because the heat flow spreads over ever larger spheres.

Thermal resistance of a complete spherical shell with inner radius ri and outer radius ro, for steady radial conduction with constant conductivity k and no internal generation.

Calculator

Solve for
K/W
m
0.010.099
m
0.11
W/(m K)
0.01500
  • Heat rate for a 100 K temperature difference62.83 W
  • Limiting resistance for an infinitely thick shell, 1/(4πk ri)3.183 K/W
  • Conduction shape factor, 4π/(1/ri − 1/ro)1.257 m

What drives the result

Each variable is moved across its typical range while the others stay at the values above. The longest bar is the key driver.

Thermal resistance (K/W) current value 1.592 K/W
kThermal conductivityKey driver
0.0015979.6
riInner radius
0.016114.3
roOuter radius
3.02
  • A shell from 0.05 m to 0.1 m resists heat flow with 1.592 K/W, so a 100 K difference drives 62.83 W through it.
  • Even an infinitely thick shell would only reach 3.183 K/W, so insulation beyond a few inner radii adds little to a small sphere.
Chart data as tables

Ranked variables

VariableTypical rangeLowest resultHighest resultSwing (K/W)Local stepChange in result
k Thermal conductivity0.01 to 500 W/(m K)0.00159279.5879.58+10%−9.09 %
ri Inner radius0.01 to 0.099 m0.0160814.3214.31+10%−18.2 %
ro Outer radius0.1 to 1 m1.5923.0241.432+10%+9.09 %

Sweep of Outer radius

Outer radius (m)Thermal resistance (K/W)
0.11.592
0.21252.434
0.3252.693
0.43752.819
0.552.894
0.66252.943
0.7752.978
0.88753.004
13.024

Sweep one variable

Thermal resistance (K/W)Hover, touch, or use the arrow keys on the chart
1.522.53 0.10.30.50.70.9 Outer radius (m) now 1.592

Variables and how each one contributes

R

Thermal resistance

Result · K/W

What the equation gives you. Everything else feeds it.

ri

Inner radius

m · typical 0.01 to 0.099

The inner radius of the shell, in m. A larger inner radius shrinks the gap and the inner area grows, so the resistance falls. Raising it by 10 % (to 0.055) moves the result by −18.2 %, from 1.592 to 1.302 K/W.

ro

Outer radius

m · typical 0.1 to 1

The outer radius of the shell, in m. A thicker shell raises the resistance, with falling returns because it approaches a limit. Raising it by 10 % (to 0.11) moves the result by +9.09 %, from 1.592 to 1.736 K/W.

k

Thermal conductivity

W/(m K) · typical 0.01 to 500

The thermal conductivity of the shell, in W/(m K). A higher conductivity lowers the resistance in inverse proportion. Raising it by 10 % (to 0.55) moves the result by −9.09 %, from 1.592 to 1.447 K/W.

Worked example with the values above

  1. Radius term: 1/ri − 1/ro = 1/0.05 − 1/0.1 = 10 1/m.
  2. Denominator: 4πk = 4π × 0.5 = 6.2832 W/(m K).
  3. R = 10 / 6.2832 = 1.5915 K/W.

Assumptions and limits

  • Steady state, constant properties unless the page states a temperature law, and no internal heat generation.
  • One-dimensional conduction in the stated geometry, with no edge or end losses.

Common mistakes

  • Using diameters where radii are needed.
  • Using °C in a formula that needs an absolute temperature, or leaving a temperature difference out of the heat rate.
  • Applying a plane-wall formula to a curved wall when the thickness is not small compared with the radius.

Statistics and uncertainty

Thermal conductivities are rarely known better than 5 % to 10 %, and contact resistances can vary by a factor of two between nominally identical joints. Treat results as estimates unless the inputs were measured.

Where it is used

  • Insulation sizing for vessels, pipes and walls.
  • Estimating interface and layer temperatures in composite constructions.

Maths you need

  • Fourier’s law: q″ = −k dT/dx
  • Thermal resistance: R = ΔT/Q, in K/W
  • Series and parallel paths: resistances add in series; conductances add in parallel

Related formulas

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