Control of unsteady flow separation over a circular cylinder using dielectric-barrier-discharge surface plasma

被引:67
作者
Jukes, Timothy N. [1 ]
Choi, Kwing-So [1 ]
机构
[1] Univ Nottingham, Fac Engn, Nottingham NG7 2RD, England
基金
英国工程与自然科学研究理事会;
关键词
discharges (electric); drag; external flows; flow control; flow separation; flow visualisation; DYNAMIC STALL CONTROL; PERIODIC EXCITATION; ACTUATORS; JET; MECHANISMS; AIRFOIL; WALL;
D O I
10.1063/1.3237151
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Dielectric-barrier-discharge plasma actuators have been used to control the unsteady flow separation over a circular cylinder at Re=15 000 with a view to maximizing the lift with a minimum drag increase. The flow structure was studied using time-resolved particle image velocimetry and flow visualization, while the dynamic lift and drag were simultaneously measured with a two-component force balance. Our results show that the lift can be dramatically increased by a single, short-duration pulse of plasma at carefully chosen location and timing. A peak lift coefficient of 1.24 was observed, showing that the plasma can increase lift by over 300%, with less than 25% increase in drag. Optimal conditions occurred when the actuator was located at 75 degrees from the streamwise axis, with plasma forcing timed to coincide with the retreat of the separation point. This corresponds to the actuator being located 7 degrees upstream of the natural separation point. The peak lift was relatively insensitive to the duration of the plasma.
引用
收藏
页数:15
相关论文
共 28 条
[1]   THE TRANSITION TO TURBULENCE IN THE WAKE OF A CIRCULAR CYLINDER [J].
BLOOR, MS .
JOURNAL OF FLUID MECHANICS, 1964, 19 (02) :290-&
[2]  
CARR L.W., 1977, ANAL DEV DYNAMIC STA
[3]   Control of flow over a bluff body [J].
Choi, Haecheon ;
Jeon, Woo-Pyung ;
Kim, Jinsung .
ANNUAL REVIEW OF FLUID MECHANICS, 2008, 40 :113-139
[4]  
CORKE TC, 2005, 20050563 AIAA
[5]  
Drescher H., 1956, Zeitschrift fur Flugwissenschaften und Weltraumforschung, V4, P17
[6]   Mechanisms and responses of a single dielectric barrier plasma actuator: Plasma morphology [J].
Enloe, CL ;
McLaughlin, TE ;
VanDyken, RD ;
Kachner, KD ;
Jumper, EJ ;
Corke, TC .
AIAA JOURNAL, 2004, 42 (03) :589-594
[7]   MECHANICS O FORMATION REGION OF VORTICES BEHIND BLUFF BODIES [J].
GERRARD, JH .
JOURNAL OF FLUID MECHANICS, 1966, 25 :401-&
[8]   Synthetic jets [J].
Glezer, A ;
Amitay, M .
ANNUAL REVIEW OF FLUID MECHANICS, 2002, 34 :503-529
[9]   Aspects of low- and high-frequency actuation for aerodynamic flow control [J].
Glezer, A ;
Amitay, M ;
Honohan, AM .
AIAA JOURNAL, 2005, 43 (07) :1501-1511
[10]   Dynamic stall control by periodic excitation, part 1: NACA 0015 parametric study [J].
Greenblatt, D ;
Wygnanski, I .
JOURNAL OF AIRCRAFT, 2001, 38 (03) :430-438