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Heat transfer and thermal systems

Temperature within a cylindrical wall

Steady radial temperature profile in a cylindrical wall with fixed temperatures Ti and To at radii ri and ro, for uniform conductivity and no generation or end effects.

Ref
HTS-05
Rev
v1
Field
Heat transfer and thermal systems
Result
T [K]

With fixed wall temperatures, steady radial conduction in a cylinder gives a logarithmic temperature profile: T(r) = Ti + (To − Ti) ln(r/ri)/ln(ro/ri). Most of the temperature drop occurs near the inner surface, where the area is smallest and the flux is highest, so the profile is steeper there than a straight line would be.

Steady radial temperature profile in a cylindrical wall with fixed temperatures Ti and To at radii ri and ro, for uniform conductivity and no generation or end effects. The profile is logarithmic, not linear.

Calculator

Solve for
K
K
2501,000
K
2501,000
m
0.0050.02
m
0.080.5
m
0.020.08
  • Fraction of the total drop reached at r0.5
  • Temperature at the same r if the profile were linear366.7 K
  • Temperature at the geometric-mean radius √(ri ro)350 K

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.

Temperature at r (K) current value 350 K
TiInner-surface temperatureKey driver
275650
ToOuter-surface temperature
325700
rRadius of interest
300400
roOuter radius
378
riInner radius
325
  • At r = 0.04 m the wall is at 350 K, 50 % of the way from the inner to the outer temperature.
  • A straight-line profile would give 366.7 K, so the log profile is lower here, because the temperature drops fastest where the area is smallest, near the inner wall.
Chart data as tables

Ranked variables

VariableTypical rangeLowest resultHighest resultSwing (K)Local stepChange in result
Ti Inner-surface temperature250 to 1,000 K275650375+10%+5.71 %
To Outer-surface temperature250 to 1,000 K325700375+10%+4.29 %
r Radius of interest0.02 to 0.08 m300400100+10%−1.96 %
ro Outer radius0.08 to 0.5 m350378.528.47+10%+0.919 %
ri Inner radius0.005 to 0.02 m32535025+10%+1.05 %

Sweep of Radius of interest

Radius of interest (m)Temperature at r (K)
0.02400
0.0275377
0.035359.6
0.0425345.6
0.05333.9
0.0575323.8
0.065315
0.0725307.1
0.08300

Sweep one variable

Temperature at r (K)Hover, touch, or use the arrow keys on the chart
300320340360380400 0.020.030.040.050.060.070.08 Radius of interest (m) now 350

Variables and how each one contributes

T

Temperature at r

Result · K

What the equation gives you. Everything else feeds it.

Ti

Inner-surface temperature

K · typical 250 to 1,000

The temperature at the inner radius, in K. Raises the temperature at every radius, most near the inner wall. Raising it by 10 % (to 440) moves the result by +5.71 %, from 350 to 370 K.

To

Outer-surface temperature

K · typical 250 to 1,000

The temperature at the outer radius, in K. Raises the temperature at every radius, most near the outer wall. Raising it by 10 % (to 330) moves the result by +4.29 %, from 350 to 365 K.

ri

Inner radius

m · typical 0.005 to 0.02

The inner radius, in m. A larger inner radius moves the interior point closer to the inner surface in log terms. Raising it by 10 % (to 0.022) moves the result by +1.05 %, from 350 to 353.7 K.

ro

Outer radius

m · typical 0.08 to 0.5

The outer radius, in m. A larger outer radius spreads the log range, so the point at r sits nearer the inner temperature. Raising it by 10 % (to 0.088) moves the result by +0.919 %, from 350 to 353.2 K.

r

Radius of interest

m · typical 0.02 to 0.08

The radius at which the temperature is wanted, in m. A larger radius moves the temperature from Ti towards To. Raising it by 10 % (to 0.044) moves the result by −1.96 %, from 350 to 343.1 K.

Worked example with the values above

  1. Log terms: ln(r/ri) = ln(0.04/0.02) = 0.69315; ln(ro/ri) = 1.3863.
  2. Fraction of the drop: 0.5.
  3. T = 400 + (300 − 400) × 0.5 = 350 K.

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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