Separation flow control by thermal bump in a supersonic airflow

被引：13
作者：
Son, E. [1 ]
Tereshonok, D.
机构：
[1] Russian Acad Sci, Joint Inst High Temp, Moscow 125412, Russia
来源：
EPL | 2012年 / 99卷 / 01期
关键词：
D O I：
10.1209/0295-5075/99/15002
中图分类号：
O4 [物理学];
学科分类号：
0702 ;
摘要：
This paper presents a numerical and theoretical investigation of a flow separation control by a thermal bump (spark discharge) in Mach M = 2 flow over a profile NACA64a212. Copyright (C) EPLA, 2012
引用
收藏
页数：5
相关论文
共 13 条
[1]  
Belocerkovskiy O.M., 1994, MOSCOW NAUKA, V4, P442
[2]  
CORKE T.C., 2006, 44 AIAA AER SCI M IN
[3]  
Golub V.V., 2010, HIGH TEMP-USSR, V6, P48
[4]  
Kartasheva M.A., 2008, VESTNIC SUSU, V10, P36
[5]  
Kazansky P, 2012, 50 AIAA AER SCI M IN
[6]  
KLIMOV A., 2011, 42 AIAA PLASM LAS C, V2, P684
[7]  
Lagno O.G., 2003, THESIS, P240
[8]  
POST M.L., 2004, 42 AIAA AER SCI M IN
[9]   Aerodynamic flow acceleration using paraelectric and peristaltic electrohydrodynamic effects of a One Atmosphere Uniform Glow Discharge Plasma [J].
Roth, JR .
PHYSICS OF PLASMAS, 2003, 10 (05) :2117-2126
[10]   Flow Separation Control by Plasma Actuator with Nanosecond Pulsed-Periodic Discharge [J].
Roupassov, D. V. ;
Nikipelov, A. A. ;
Nudnova, M. M. ;
Starikovskii, A. Yu. .
AIAA JOURNAL, 2009, 47 (01) :168-185
12