A numerical study on shock wave - boundary layer interaction flows
This thesis addresses the important problem of shock wave--boundary layer interaction (SBLI) flows for aerospace engineering applications. Moreover, the work emphasizes the need for high fidelity simulations for the appropriate treatment of such flows. In this context, RANS solvers appear as a cost...
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| Format: | Others |
| Language: | English |
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Instituto Tecnológico de Aeronáutica
2013
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| Online Access: | http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2883 |