Development of methodologies of aeroelastic analysis for the design of flexible aircraft wings
This work deals with several computational methodologies for the aeroelastic study of flexible aircraft wings on a preliminary design phase. An in-house vortex lattice method code named VLM4FW has been implemented with correction of sidewash and backwash effects to take into account the aeroelastic...
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| Format: | Others |
| Language: | English |
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Instituto Tecnológico de Aeronáutica
1201
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| Online Access: | http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=3372 |