Large-Eddy Simulation of NACA 0015 Airfoil Flow at Reynolds Number of 1.6x106

被引：17
|
作者：
Sato, Makoto [1 ]
Asada, Kengo [2 ,4 ]
Nonomura, Taku [1 ]
Kawai, Soshi [3 ]
Fujii, Kozo [1 ,4 ]
机构：
[1] Japan Aerosp Explorat Agcy, Dept Space Flight Engn, Inst Space & Astronaut Sci, Sagamihara, Kanagawa 2525210, Japan
[2] Univ Tokyo, Dept Aeronaut & Astronaut, Sagamihara, Kanagawa 2525210, Japan
[3] Tohoku Univ, Dept Aerosp Engn, Sendai, Miyagi 9808579, Japan
[4] Tokyo Univ Sci, Dept Informat & Comp Technol, Tokyo 1258585, Japan
来源：
AIAA JOURNAL | 2017年 / 55卷 / 02期
关键词：
ADVERSE-PRESSURE-GRADIENT; TURBULENT-BOUNDARY-LAYER; PLASMA ACTUATOR; SCHEMES;
D O I：
10.2514/1.J054963
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
[No abstract available]
引用
收藏
页码：673 / 679
页数：7
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