An unstructured grid approach to the solution of axisymmetric launch vehicle flows.
A study of the flowfield around axisymmetric launch vehicles in different flight conditions and configurations is performed in this work. Particularly, the VLS second stage flight configuration is analyzed considering the case with and without a propulsive jet in the vehicle base. Among the differen...
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| Format: | Others |
| Language: | English |
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Instituto Tecnológico de Aeronáutica
2001
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| Online Access: | http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2444 |