VVT42 - Non-gray radiation exchange between two parallel plates
| Radiation calculation method | Test case |
|---|---|
| Deterministic | SVTEST288 |
| Monte Carlo | SVTEST289 |
Description
The purpose of this validation test is to determine the equilibrium temperature of a thermally free plate and compare the result with a theoretical prediction for non-gray radiative exchange between two parallel plates.
Geometry
The geometry consists of two centered parallel square plates, each with an area of 1 m2. The plates are separated by a distance of 0.1 m, such that see each other with a view factor of 0.826997.
Simulation model
Both plates are meshed with quadrilateral thin shell element. One plate is held at a prescribed temperature, while the second plate is allowed to reach radiative equilibrium. The top surface emissivity is defined as a function of wavelength in the field table:
| Band | Wavelength range | Plate 1 emissivity | Plate 2 emissivity |
|---|---|---|---|
| 1 | 0 to 40 | 0.1 | 0.3 |
| 2 | 40 to 80 | 0.25 | 0.25 |
| 3 | 80 to 120 | 0.15 | 0.2 |
| 4 | 120 to 1200 | 0.05 | 0.18 |

- Material: Steel
- Density: 7820 kg/m3
The following boundary conditions are applied:
- Temperature constraint applied to the element 1 with a value of T1 = 60 K.
- Radiation: All Radiation with the
Include Radiative Environment option selected using:
- Deterministic with element subdivision equal to 5
- Monte Carlo with 15 000 number of rays and selected Calculate View Factors only
- Hemicube Rendering
This model uses the Simcenter 3D Space Systems Thermal solver.
The following solution options are set:
- Solution Type = Steady State
- Radiative Environment Temperature: Tenv = 0 K
The following radiation solver parameters are set:
- Bands = Specify Wavelength
- Wavelength Breakpoint Table = [0, 40, 80, 120, 1200]
Theory
At equilibrium, the net heat transfer rate to the free plate is zero. Therefore, the radiative heat transfer rate emitted by plate 2 is equal to the radiative heat transfer rate absorbed by plate 2:
The emitted heat rate from plate 2 is:
The absorbed heat rate by plate 2 is:
where:
- σ = 5.670374419 × 10-8 W/m2·K4 is the Stefan-Boltzmann constant.
- A1 and A2 are the areas of plates 1 and 2, respectively.
- T1 is the prescribed temperature of plate 1.
- T2 is the equilibrium temperature of plate 2.
- VF12 is the view factor from plate 1 to plate 2.
- VF21 is the view factor from plate 2 to plate 1.
- ε1g is the emissivity of plate 1 in radiation band g.
- ε2g is the emissivity of plate 2 in radiation band g.
- pg(T) is the blackbody radiation fraction in band g at temperature T.
The equilibrium temperature T2=46.04 K is obtained by iteratively solving the nonlinear equation Q2,emit(T2)−Q2,abs(T2)=0, because the blackbody radiation fractions pg(T2) depend on the unknown temperature T2.
The blackbody radiation fractions for the four bands at T1=60 K and T2=46.04 K are found using the radiation function table [20]:
| Band | Wavelength range | pg(60) | pg(46.04) |
|---|---|---|---|
| 1 | 0 to 40 | 0.1403 | 0.0444 |
| 2 | 40 to 80 | 0.4673 | 0.3760 |
| 3 | 80 to 120 | 0.2116 | 0.2730 |
| 4 | 120 to 1200 | 0.1804 | 0.3058 |
Results
The following table compares the temperature computed by the thermal solver with the theoretical temperature obtained by iteratively solving the nonlinear equation. Simulation results using deterministic and Monte Carlo methods are in agreement with theoretical values. The Hemicube method shows a larger discrepancy, which is likely due to view-factor discretization and resolution effects associated with closely spaced parallel plates.
| Radiation calculation method | T2,sim(K) | T2,theory(K) | Error (%) |
|---|---|---|---|
| Deterministic | 46.6 | 46.04 | 1.22 |
| Monte Carlo with view factor only calculation | 46.04 | 46.04 | 0 |
| Hemicube Rendering | 55.64 | 46.04 | 20.85 |
