VVT28 - Heat flow through insulation with temperature dependent conductivity

Solution Test case
Finite volume method SVTEST260
Finite element method SVTEST261

Description

The purpose of this validation test is to determine the temperature distribution through a 2-D insulation with variable conductivity. The steady-state temperatures predicted by the solver are compared with the analytical solutions.

Geometry

The insulation is modeled as a 2-D solid rectangular plate of height H = 1 m and width L = 0.7 m.

Simulation model

This model uses the Thermal solution type.

The surface of the plate is meshed with 2D linear quadrilateral elements with the size of 50 mm.

The meshed elements have the following material and physical properties:

  • Material: Bronze.
  • Thermal conductivity: W/mC

    with W/m and K-1.

  • Thickness: 10 mm

The following boundary conditions are applied:

  • Temperature constraint on the left edge of the plate with a value of T 1 = 600C.
  • Temperature constraint on the right edge of the plate with a value of T 2 = 400C.

The default solver parameters are selected.

Theory

For one-dimensional, steady-state conduction in a plane wall with no heat generation and a linearly variable thermal conductivity, the Fourier's law of heat conduction is expressed as:

where:

  • q' is the rate of conduction heat transfer.
  • A is the plane wall area.
  • k(T) is the variable thermal conductivity of the material.
  • kav is the average value of the thermal conductivity given by:

For a linearly varying thermal conductivity:

Integrating the Fourier's law equation:

Performing the integration:

From this equation and substituting q' with its expression as a function of kav:

which is a quadratic equation in the unknown temperature T. Using the quadratic formula, the temperature distribution T(x) in the wall is determined to be:

The proper sign of the square root term ( + or -) is determined from the requirement that the temperature at any point within the medium must remain between T1 and T2.

Results

The following tables compare the computed nodal temperatures with theoretical values. The x location for each case is determined by the x-coordinate of the nodes.

Finite volume method Finite volume method
x (m) Ttheory (°C) Tsim (°C) Tsim (°C)
0 600.0000 600.0000 600.0000
0.05 586.5077 586.5077 586.5077
0.1 572.9057 572.9057 572.9057
0.15 559.1912 559.1912 559.1912
0.2 545.3614 545.3614 545.3614
0.25 531.4133 531.4133 531.4133
0.3 517.3439 517.3439 517.3439
0.35 503.1499 503.1499 503.1499
0.4 488.8280 488.8279 488.8279
0.45 474.3746 474.3745 474.3745
0.5 459.7860 459.7860 459.7860
0.55 445.0584 445.0584 445.0584
0.6 430.1878 430.1877 430.1877
0.65 415.1698 415.1697 415.1697
0.7 400.0000 400.0000 400.0000

The numerical results for finite volume and finite element methods are the same as the theoretical solution for the first three decimal digits.