On the behavior of upwind schemes applied to three-dimensional supersonic and hypersonic cold gas flow simulations of aerospace configurations.
The present work describes the efforts towards the implementation of upwind schemes to simulate supersonic and hypersonic cold gás flows. The class of flux vector splitting schemes has been chosen, and the particular methods implemented are the van Leer and Liou schemes. Results for different freest...
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| Format: | Others |
| Language: | English |
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Instituto Tecnológico de Aeronáutica
2007
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| Online Access: | http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=397 |