Numerical simulation on drag and heat reduction of hypersonic spike-aerodisk-self-coupled stamping lateral jet concept

被引:0
|
作者
Wang, Ziyu [1 ]
Fang, Shuzhou [1 ]
Guo, Jian [1 ]
Ni, Zijian [1 ]
机构
[1] School of Aerospace Engineering, Beijing Institute of Technology, Beijing,100081, China
来源
关键词
D O I
10.13224/j.cnki.jasp.20220775
中图分类号
学科分类号
摘要
引用
收藏
相关论文
共 21 条
  • [21] Coupled fluid-thermal analysis of the reduction mechanism for the drag and heat flux induced by jet interaction in a hypersonic reusable launch vehicle
    Meng, Yu-shan
    Wang, Zhong-wei
    Huang, Wei
    Niu, Yao-bin
    Yan, Li
    AIP ADVANCES, 2022, 12 (10)