Development of the method of an electrohydrodynamic force effect on a boundary layer for active control of aerodynamic flows

被引：10
|
作者：
Aleshin, B. S. [1 ]
Khomich, V. Yu. [2 ]
Chernyshev, S. L. [3 ]
机构：
[1] Natl Res Ctr Inst, Zhukovskii, Moscow Oblast, Russia
[2] Russian Acad Sci, Inst Electrophys & Electroenerget, St Petersburg 191186, Russia
[3] Cent Aerohydrodynam Inst, Zhukovskii 140160, Moscow Region, Russia
来源：
DOKLADY PHYSICS | 2016年 / 61卷 / 12期
关键词：
BARRIER DISCHARGE;
D O I：
10.1134/S1028335816120107
中图分类号：
O3 [力学];
学科分类号：
08 ; 0801 ;
摘要：
The results of investigations on the possibility of an electrohydrodynamic force effect on a gas flow implemented with the help of a barrier discharge are presented. A new method of controlling the laminar flow around a base with suppression of instabilities of the incoming flow due to electrohydrodynamic force action on the boundary layer near the forward edge of a swept wing is proposed. An efficient multidischarge actuator system is developed and created for active control of aerodynamic flows with induced-air-flow characteristics exceeding the world analogues.
引用
收藏
页码：601 / 603
页数：3
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