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Engineering guide

This module calculates steady-state heat conduction according to the VDI Heat Atlas (VDI-Wärmeatlas, 12th edition 2019) for the classic basic geometries: plane walls and plates, hollow cylinders (pipes), and hollow spheres – each also in multilayer form – as well as fins, rods, and wires. In addition, two-dimensional conduction problems can be handled via shape factors, for example buried pipes or bodies with oval and rectangular cross-sections.

Calculating steady-state heat conduction is one of the fundamental tasks of equipment and plant engineering: temperature profiles in vessel and furnace walls, heat flows through pipe walls and insulation layers, the effectiveness of fins on heating and cooling surfaces, or the wall temperatures of multilayer structures. From thermal conductivity, layer thickness, and area, the conduction resistance of each layer is obtained; the series connection of the resistances yields the heat flow and the intermediate temperatures.

The module follows the relations from section E1 of the VDI Heat Atlas and provides the results in a form that can be used directly in overall heat transfer and heat loss calculations (for instance with the module for the heat loss of walls and pipework).

VDI-Wärmeatlas, 12. Auflage 2019 · VDI · Wärmeübertragung

Scope

  • Steady conduction of heat

Typical workflow

  1. Define the geometry

    First, the basic geometry is chosen: plane wall, hollow cylinder, or hollow sphere, in single or multilayer form – alternatively a fin, a rod, or a two-dimensional case with a shape factor. The geometry determines which conduction equation is applied.

  2. Specify dimensions and material properties

    For each layer, the thickness or the inside and outside diameters and the thermal conductivity at the governing mean temperature are entered. For temperature-dependent conductivity, the value at the mean layer temperature is used, which may require a short iteration.

  3. Set the boundary conditions

    The surface or wall temperatures on both sides, or a prescribed heat flow, serve as the thermal boundary conditions. This fully determines the steady-state conduction problem.

  4. Calculate the resistances and the heat flow

    For each layer, the conduction resistance is formed – proportional to the thickness for the plane wall, with the logarithm of the diameter ratio for the hollow cylinder, and with the difference of the reciprocal radii for the hollow sphere. The series connection yields the total resistance and from it the heat flow.

  5. Evaluate the temperature profile and special cases

    From the heat flow and the individual resistances, the temperatures at the layer boundaries follow. For fins and rods, the fin efficiency and the temperature profile along the fin are additionally calculated; for two-dimensional cases, the heat flow is determined via the shape factor of the arrangement.

Frequently asked questions

When may I calculate steady-state, and when do I need a transient analysis?

Steady-state calculation requires that the boundary conditions do not change with time, or only slowly compared with the thermal time constant of the component. This is satisfied for continuous operating states of furnaces, pipework, and vessels. Start-up and shutdown, batch processes, or upset scenarios, on the other hand, require a transient analysis, because there the heat storage in the wall dominates the behavior.

Why is the logarithm of the diameter ratio used for a pipe?

In a hollow cylinder, the area available for heat flow grows with the radius, so the heat flux decreases toward the outside. Integrating the Fourier equation over the radius therefore yields the resistance R = ln(d_a/d_i)/(2·π·λ·L) per pipe length. The approximation using a mean area is permissible only for thin-walled pipes; for thick-walled layers such as insulation it leads to significant errors.

How do I deal with contact resistances between the layers?

The ideal series connection assumes full-area contact between the layers. Real interfaces – for instance between a pipe and a slipped-on insulation shell, or between a wall and its cladding – have air gaps that act as an additional resistance. In insulation calculations, this usually acts favorably (more resistance), but in cooling tasks it is dangerous, because the heat removal is overestimated. When in doubt, contact resistances should be applied conservatively.

What does the fin efficiency express?

The fin efficiency is the ratio of the heat flow actually dissipated through the fin to the heat flow the fin would dissipate if it were entirely at the base temperature. It decreases with increasing fin height, increasing heat transfer coefficient, and decreasing thermal conductivity of the fin material. Long, thin fins made of poorly conducting material therefore add hardly any extra duty – fin design is always an optimum between area and efficiency.

Worked example

A pipe is insulated with a 50 mm thick mineral wool shell. The insulation starts at the pipe outside diameter of 88.9 mm; its surface temperatures are 150 °C on the inside and 40 °C on the outside. The thermal conductivity of the mineral wool at the mean temperature is 0.05 W/(m·K). Find the heat flow per unit length through the insulation layer.

Given

Inside diameter of the insulation layer d188.9 mm
Outside diameter of the insulation layer d2188.9 mm
Inner surface temperature ϑ1150 °C
Outer surface temperature ϑ240 °C
Thermal conductivity λ0.05 W/(m·K)

Solution

Formula for the hollow cylinder

For steady-state heat conduction through a cylindrical layer, the heat flow per unit length is:

ql = 2 · π · λ · (ϑ1 − ϑ2) / ln(d2/d1)

Insert the diameter ratio

ln(d2/d1) = ln(188.9 / 88.9) = ln(2.125) = 0.7537

Calculate the heat flow

ql = 2 · π · 0.05 W/(m·K) · (150 − 40) K / 0.7537

ql = 34.56 / 0.7537 W/m ≈ 45.9 W/m

About 46 W per meter of pipe thus flow through the insulation layer. The temperature profile within the layer is logarithmic over the radius.

Result

Heat flow per unit length q_l≈ 45.9 W/m
Calculation basis: Fourier heat conduction equation for the hollow cylinder, q_l = 2πλΔϑ/ln(d2/d1), VDI Heat Atlas section E1 (steady-state heat conduction)

Technical content source: LV-Solved-Problems-Content 628d313247e7