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Numerical solutions are provided for a transient temperature rise in a composite sandwich structure that is induced by a dithering or rotating laser beam. Here we consider using E-glass or C-glass fibers as skin materials whereas the core can be selected from a variety of materials including balsa wood, honeycomb, cork and C-foam. Our results provide insights in engineering sandwich-structured composite as heat shields. More specifically, it is shown that (1) carbon fibers are better skin materials than E-glass fibers; (2) sandwichstructured composite with carbon fiber skin and honeycomb core is most promising.

Transient temperature rises in a sandwich-structured composite induced by a dithering or rotating laser beam