Numerical study on the generation position of screech tone in axisymmetric supersonic jet based on modal decomposition

被引：0
|
作者：
Li, Hu [1 ,2 ]
Luo, Yong [1 ,2 ]
Han, Shuaibin [1 ,2 ]
Wang, Yimin [1 ,2 ]
Wu, Conghai [1 ,2 ]
Liu, Xuliang [1 ,2 ]
机构：
[1] State Key Laboratory of Aerodynamics, China Aerodynamics Research and Development Center, Mianyang,621000, China
[2] Computational Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang,621000, China
来源：
Lixue Xuebao/Chinese Journal of Theoretical and Applied Mechanics | 2022年 / 54卷 / 04期
关键词：
Compendex;
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学科分类号：
摘要：
Navier Stokes equations
引用
收藏
页码：975 / 990
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