2   Artículos

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en línea
Fangyou Yu, Zhanbiao Gao, Qifan Zhang, Lianjie Yue and Hao Chen    
Suppressing shock-induced flow separation has been a long-standing problem in the design of supersonic vehicles. To reduce the structural and design complexity of control devices, a passive control technique based on micro-serrations is proposed and its ... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Yuling Li, Lianjie Yue, Chengming He, Wannan Wu and Hao Chen    
The present paper focuses on the Lagrange optimization of shock waves for a two-dimensional hypersonic inlet by limiting the cowl internal angle and inlet length. The results indicate the significant influences of geometric constraints on the configurati... ver más
Revista: Aerospace    Formato: Electrónico

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