首页|期刊导航|中国航空学报（英文版）|Aerodynamics-informed parametric method for rapid waverider design based on the second-order curved shock theory
中国航空学报（英文版）2026，Vol.39Issue(3)：1-23,23.DOI:10.1016/j.cja.2025.103932
Aerodynamics-informed parametric method for rapid waverider design based on the second-order curved shock theory
Aerodynamics-informed parametric method for rapid waverider design based on the second-order curved shock theory
摘要
关键词
Analytical expressions/Curved shock theory/Hypersonic vehicles/Rapid waverider designKey words
Analytical expressions/Curved shock theory/Hypersonic vehicles/Rapid waverider design引用本文复制引用
Yiqi TANG,Xiaogang ZHENG,Chongguang SHI,Chengxiang ZHU,Yancheng YOU..Aerodynamics-informed parametric method for rapid waverider design based on the second-order curved shock theory[J].中国航空学报（英文版）,2026,39(3):1-23,23.基金项目
This work was supported by the National Natural Science Foundation of China(Nos.U21B6003,U20A2069,and 12202372)and the China Postdoctoral Science Foundation(No.2022M712653). （Nos.U21B6003,U20A2069,and 12202372）
