A new sonic box formulation for oscillating swept thick wings in transonic flow.
The present work shows a mathematical model for unsteady linearized potential flow around thin wings having swept leading and trailing edges and over thick wings with swept and unswept leading edges. Doublet integrals are obtained for the three dimensional case. The wings are supposed to be describi...
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| Format: | Others |
| Language: | English |
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Instituto Tecnológico de Aeronáutica
2004
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| Online Access: | http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=86 |