Mitigation of shock-induced flow separation over an axisymmetric flared body using ramped vanes

被引:0
作者
T. Nilavarasan
G. N. Joshi
A. Misra
C. Manisankar
S. B. Verma
机构
[1] Defence Institute of Advanced Technology,Department of Aerospace Engineering
[2] National Aerospace Laboratories,Experimental Aerodynamics Division
来源
Journal of Visualization | 2023年 / 26卷
关键词
Compression corner; Shock–boundary layer interaction; Vortex generator; Flow control; Supersonic flow;
D O I
暂无
中图分类号
学科分类号
摘要
引用
收藏
页码:1279 / 1297
页数:18
相关论文
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