Aeroelastic studies using system identification techniques
The present work is concerned with studying techniques which would allow the identification of a multiple degree of freedom aeroelastic system from a single computational fluid dynamics (CFD) unsteady simulation. This data is, then, used to generate the root locus for aeroelastic stability analysis...
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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=2864 |