Unsteady shock front waviness in shock-buffet of transonic aircraft
Abstract The unsteady transonic aerodynamics of a wing-body configuration is investigated by solving the Unsteady Reynolds-averaged Navier-Stokes equations closed with the full Reynolds Stress Model. This work presents the prediction of flow field characteristics during deep shock-buffet penetration...
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| Principais autores: | , , , |
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| Formato: | Artigo |
| Idioma: | Inglês |
| Publicado em: |
SpringerOpen
2020-04-01
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| Colecção: | Advances in Aerodynamics |
| Assuntos: | |
| Acesso em linha: | http://link.springer.com/article/10.1186/s42774-020-00034-x |
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