Aerodynamics-informed parametric method for rapid waverider design based on the second-order curved shock theoryOA
Aerodynamics-informed parametric method for rapid waverider design based on the second-order curved shock theory
Yiqi TANG;Xiaogang ZHENG;Chongguang SHI;Chengxiang ZHU;Yancheng YOU
School of Aerospace Engineering,Xiamen University,Xiamen 361102,ChinaSchool of Aerospace Engineering,Xiamen University,Xiamen 361102,ChinaSchool of Aerospace Engineering,Xiamen University,Xiamen 361102,ChinaSchool of Aerospace Engineering,Xiamen University,Xiamen 361102,ChinaSchool of Aerospace Engineering,Xiamen University,Xiamen 361102,China
Analytical expressionsCurved shock theoryHypersonic vehiclesRapid waverider design
Analytical expressionsCurved shock theoryHypersonic vehiclesRapid waverider design
《中国航空学报（英文版）》 2026 (3)
1-23,23
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).
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