Numerical Analysis of Shock Control Bumps for Delaying Transonic Buffet Boundary on a Swept Wing
Transonic shock buffet is a complex flow phenomenon characterized by self-sustained shock oscillations, which severely limits the flight envelope of modern civil aircraft. While Shock Control Bumps (SCBs) have been widely studied for drag reduction, their potential for delaying the buffet boundary o...
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| Principais autores: | , , |
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| Formato: | Artigo |
| Idioma: | Inglês |
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MDPI AG
2026-01-01
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| Colecção: | Aerospace |
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| Acesso em linha: | https://www.mdpi.com/2226-4310/13/1/98 |
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