Spatial Direct Numerical Simulation of the Hypersonic Boundary-Layer Stabilization Using Porous Coatings

被引：29
|
作者：
Zhao, R. [1 ]
Wen, C. Y. [2 ]
Long, T. H. [2 ]
Tian, X. D. [2 ]
Zhou, L. [1 ]
Wu, Y. [3 ]
机构：
[1] Beijing Inst Technol, Sch Aerosp Engn, Beijing 100081, Peoples R China
[2] Hong Kong Polytech Univ, Dept Mech Engn, Kowloon, Hong Kong, Peoples R China
[3] Chinese Acad Sci, Comp Network Informat Ctr, Supercomp Ctr, Beijing 100190, Peoples R China
来源：
AIAA JOURNAL | 2019年 / 57卷 / 11期
基金：
中国国家自然科学基金;
关键词：
ACOUSTIC PROPERTIES; TRANSITION; STABILITY; FLOW;
D O I：
10.2514/1.J058467
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
引用
收藏
页码：5061 / 5065
页数：5
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