Gas Kinetic Scheme Coupled with High-Speed Modifications for Hypersonic Transition Flow Simulations
The issue of hypersonic boundary layer transition prediction is a critical aerodynamic concern that must be addressed during the aerodynamic design process of high-speed vehicles. In this context, we propose an advanced mesoscopic method that couples the gas kinetic scheme (GKS) with the Langtry–Men...
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| Автори: | , , , , , |
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| Формат: | Artigo |
| Мова: | Inglês |
| Опубліковано: |
MDPI AG
2024-02-01
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| Серія: | Entropy |
| Предмети: | |
| Онлайн доступ: | https://www.mdpi.com/1099-4300/26/2/173 |
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