Multilayer and thermal protection system modeling
This lesson introduces multi-layer shell modeling to efficiently represent layered thermal structures, including thermal protection systems and insulation, using 2D meshes with through-thickness heat transfer.
This lesson may include hands-on exercises. Review the Discussion section for background information or click the button to proceed to the practical section.
Discussion
Multilayer and thermal protection system modeling allows you to represent complex layered structures using efficient 2D representations instead of detailed 3D solid meshes. Multi-layer shells enable the modeling of multiple materials, thicknesses, and thermal properties within a single mesh while still capturing through-thickness and in-plane heat transfer behavior.
Multi-layer shells can be defined as uniform or non-uniform. Uniform shells use identical material properties and thickness for all layers, while non-uniform shells allow each layer to be defined individually. Heat transfer through the stack is modeled by conduction between layers, with radiation and convection applied only on the top and bottom layers.
The thermal solver treats multi-layer shells by computing conduction through intermediate layers while limiting radiation and convection to the top and bottom layers only. Couplings between multi-layer shells and other meshes are established through the layer closest to the connected geometry. For uniform multi-layer shells, in-plane conduction is calculated only in the central layer, whereas non-uniform multi-layer shells support in-plane conduction in every layer.
Post-processing capabilities allow you to review temperature results for each layer in the stack. For multi-layer shells with more than three layers, results are displayed by ply, from the bottom layer to the top layer. For simpler stacks, top and bottom viewing options are used.
By using multi-layer shells, you can efficiently model layered thermal systems with reduced computational cost while preserving the accuracy needed for spacecraft thermal analysis.
Hands-on material
To gain experience with the topics discussed here, complete the following:
