Transient growth instability cancelation by a plasma actuator array

被引:53
作者
Hanson, Ronald E. [1 ]
Lavoie, Philippe [1 ]
Naguib, Ahmed M. [2 ]
Morrison, Jonathan F. [3 ]
机构
[1] Univ Toronto, Inst Aerosp Studies, Toronto, ON M3H 5T6, Canada
[2] Michigan State Univ, Dept Mech Engn, E Lansing, MI 48824 USA
[3] Univ London Imperial Coll Sci Technol & Med, Dept Aeronaut, London SW7 2AZ, England
基金
加拿大自然科学与工程研究理事会; 英国工程与自然科学研究理事会; 美国国家科学基金会;
关键词
LAMINAR BOUNDARY-LAYER; AMPLITUDE STREAMWISE VORTICITY; FLOW-CONTROL; OPTIMAL PERTURBATIONS; KLEBANOFF MODES; ACTIVE CONTROL; UPSTREAM FLOW; TRANSITION; DISTURBANCES; TURBULENCE;
D O I
10.1007/s00348-010-0877-1
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
This study investigates an actuation scheme that can be integrated as part of a feedback control system in the laboratory for the purpose of negating the transient growth instability in a Blasius boundary layer and delaying transition. The actuators investigated here consist of a spanwise array of symmetric plasma actuators, which are capable of generating spanwise-periodic counter-rotating vortices. Three different actuator geometries are investigated, resulting in 45, 67 and 70% reduction of the total disturbance energy produced inside the boundary layer by an array of roughness elements. It is demonstrated that the control effectiveness of the actuators can be significantly improved by optimizing the geometry of the array.
引用
收藏
页码:1339 / 1348
页数:10
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