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The Theoretical Research for the Rotor/Fuselage Unsteady Aerodynamic Interaction Problem
Based on coupled unsteady panel/free-wake method, a universal analysis model was established, which provides a good prediction for the rotor/fuselage unsteady aerodynamic interaction. Considering the deficiencies of the traditional time-marching rotor free-wake algorithms, notably on stability and e...
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| Publicado no: | Journal of Aerospace Technology and Management |
|---|---|
| Main Authors: | , , |
| Formato: | Artigo |
| Idioma: | Inglês |
| Publicado em: |
Ministério da Defesa
2016
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| Assuntos: | |
| Acesso em linha: | https://www.redalyc.org/articulo.oa?id=309446752004 https://www.redalyc.org/journal/3094/309446752004/ https://www.redalyc.org/journal/3094/309446752004/html/ https://www.redalyc.org/journal/3094/309446752004/309446752004.epub https://www.redalyc.org/journal/3094/309446752004/movil |
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