Direct numerical simulation of supersonic boundary layer transition induced by gap-type roughness
Abstract The transition of the supersonic boundary layer induced by roughness is a highly intricate process. Gaining a profound understanding of the transition phenomena and mechanisms is crucial for accurate prediction and control. In this study, to delve into the flow mechanisms of a transition in...
Kaydedildi:
| Asıl Yazarlar: | , , , , , |
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| Materyal Türü: | Artigo |
| Dil: | Inglês |
| Baskı/Yayın Bilgisi: |
SpringerOpen
2024-07-01
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| Seri Bilgileri: | Advances in Aerodynamics |
| Konular: | |
| Online Erişim: | https://doi.org/10.1186/s42774-024-00177-1 |
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