Separation control in duct flows

被引:61
作者
Amitay, M [1 ]
Pitt, D
Glezer, A
机构
[1] Georgia Tech Res Inst, Aerosp & Transportat Lab, Atlanta, GA 30332 USA
[2] Boeing Corp, Struct Dept, St Louis, MO 63134 USA
[3] Georgia Tech Res Inst, Woodruff Sch Mech Engn, Atlanta, GA 30332 USA
来源
JOURNAL OF AIRCRAFT | 2002年 / 39卷 / 04期
关键词
D O I
10.2514/2.2973
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Active control of separation in a duct flow is achieved using an array of fluidic actuators based on synthetic-jet technology. A two-dimensional serpentine duct model is designed to produce controlled separated flow in two configurations, in which the flow is either completely separated or has a separation bubble. An array of synthetic-jet actuators is placed within the separated flow domain in the diffuser section downstream of the onset of separation. Actuation leads to complete flow attachment up to U-in = 75 m/s (M approximate to 0.2) and to partial reattachment up to U-in = 105 m/s (M approximate to 0.3).
引用
收藏
页码:616 / 620
页数:5
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