Aerothermodynamic study of UHTC-based thermal protection systems

By R. Savino, M. De Stefano Fumo, D. Paterna, M. Serpico. 2005

208 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Applied Mathematics, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/daeea80a432e998cfafdcae6f8296c01e8dff656

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1. T. Parthasarathy
2. R. Rapp
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4. M. Opeka
5. W. Fahrenholtz

Citations in the corpus

• Ablation behavior of ZrB2-SiC ultra high temperature ceramics under simulated atmospheric re-entry conditions (2008, unknown): “to endure higher surface temperatures [9–12].”
• A Model for the Oxidation of ZrB2, HfB2 and TiB2 (Postprint) (2007, background): “Components in high-flow environments, such as the leading edge of a hypersonic vehicle, are subjected to very high temperatures and require that the geometric integrity be maintained during service [1,2].”