Numerical study on flow characteristics of high-pressure capturing wing configuration at subsonic, transonic and supersonic regime

被引：0
|
作者：
Wang, Haoxiang [1 ,2 ]
Li, Guangli [1 ]
Yang, Jing [1 ,2 ]
Xiao, Yao [1 ,2 ]
Wang, Xiaoyong [1 ]
Xu, Yingzhou [1 ,2 ]
Xu, Xiangui [1 ,2 ]
Cui, Kai [1 ,2 ]
机构：
[1] State Key Laboratory of High Temperature Gas Dynamics, Institute of Mechanics, CAS, Beijing,100190, China
[2] School of Engineering Science, University of Chinese Academy of Sciences, Beijing,100049, China
来源：
Lixue Xuebao/Chinese Journal of Theoretical and Applied Mechanics | 2021年 / 53卷 / 11期
关键词：
Structural frames - Supersonic aircraft - Airframes - Shock waves - Flow separation - Fuselages - Angle of attack - Flow fields;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
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页码：3056 / 3070
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