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

被引：18

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

页码：673 / 679

页数：7

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