In the radiation matrix method, for a system of two radiating surfaces, Equation 6–14 can be expanded as:
(6–47) |
or
(6–48) |
where:
K' cannot be calculated directly since it is a function of the unknowns Ti and Tj. The temperatures from previous iterations are used to calculate K' and the solution is computed iteratively.
For a more general case, Equation 6–12 can be used to construct a single row in the following matrix equation:
(6–49) |
such that:
(6–50) |
(6–51) |
Solving for {Q}:
(6–52) |
and therefore:
(6–53) |
Equation 6–52 is analogous to Equation 6–12 and can be set up for standard matrix equation solution by the process similar to the steps shown in Equation 6–47 and Equation 6–48.
(6–54) |
[K'] now includes T3 terms and is calculated in the same manner as in Equation 6–48). To be able to include radiation effects in elements other than LINK31, MATRIX50 (the substructure element) is used to bring in the radiation matrix. MATRIX50 has an option that instructs the solution phase to calculate [K']. The AUX12 utility is used to create the substructure radiation matrix. AUX12 calculates the effective conductivity matrix, [Kts], in Equation 6–52, as well as the view factors required for finding [Kts]. The user defines flat surfaces to be used in AUX12 by overlaying nodes and elements on the radiating edge of a 2D model or the radiating face of a 3D model.
Two methods are available in the radiation matrix method to calculate the view factors (VTYPE command): Non-Hidden Method and Hidden Method. The governing equations and theory for calculating view factors using these methods are described in Non-Hidden Method and Hidden Method. See aslo Considerations for the Non-hidden Method in the Thermal Analysis Guide and Considerations for the Hidden Method in the Thermal Analysis Guide for a discussion concerning the use of these two methods.
Details of the theory underlying view factor calculations for axisymetric bodies are found in View Factors of Axisymmetric Bodies.
The use of a space node to account for radiation to ambient space is described in Space Node and in Recommendations for Using Space Nodes in the Thermal Analysis Guide.