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Analysis of Influencing Factors of Boundary Layer Transition During Ascent Phase of Hypersonic Vehicle

The transition of the boundary layer is an important issue that must be considered in the design of hypersonic vehicles. During the ascent phase of the vehicle, both the Mach number and the flight altitude increase simultaneously and affect the location of transition jointly. This paper investigated...

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Principais autores: Yiwei TANG, Chao LI, Caihong SU
Formato: Artigo
Idioma:Chinês
Publicado em: China Astronautic Publishing CO., LTD. ; Editorial Office of Physics of Gases 2024-11-01
Colecção:气体物理
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Acesso em linha:http://qtwl.xml-journal.net/cn/article/doi/10.19527/j.cnki.2096-1642.1115
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