AN EXAMPLE OF ACTIVE CIRCULATION CONTROL OF THE UNSTEADY SEPARATED FLOW PAST A SEMIINFINITE PLATE

被引:23
作者
CORTELEZZI, L
LEONARD, A
DOYLE, JC
机构
[1] CALTECH,GRAD AERONAUT LABS,PASADENA,CA 91125
[2] CALTECH,DEPT ELECT ENGN,PASADENA,CA 91125
[3] CALTECH,DEPT ENGN SCI,PASADENA,CA 91125
关键词
D O I
10.1017/S0022112094003460
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Active circulation control of the two-dimensional unsteady separated flow past a semi-infinite plate with transverse motion is considered. The rolling-up of the separated shear layer is modelled by a point vortex whose time-dependent circulation is predicted by an unsteady Kutta condition. A suitable vortex shedding mechanism introduced. A control strategy able to maintain constant circulation when a vortex is present is derived. An exact solution for the nonlinear controller is then obtained. Dynamical systems analysis is used to explore the performance of the controlled system. The control strategy is applied to a class of flows and the results are discussed. A procedure to determine the position and the circulation of the vortex, knowing the velocity signature on the plate, is derived. Finally, a physical explanation of the control mechanism is presented.
引用
收藏
页码:127 / 154
页数:28
相关论文
共 16 条
[1]  
[Anonymous], 1990, INTRO APPL NONLINEAR
[2]   EFFECT OF LEADING-EDGE SEPARATION ON THE LIFT OF A DELTA-WING [J].
BROWN, CE ;
MICHAEL, WH .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1954, 21 (10) :690-&
[3]   INVISCID MODEL OF 2-DIMENSIONAL VORTEX SHEDDING [J].
CLEMENTS, RR .
JOURNAL OF FLUID MECHANICS, 1973, 57 (FEB6) :321-&
[4]   POINT VORTEX MODEL OF THE UNSTEADY SEPARATED FLOW PAST A SEMIINFINITE PLATE WITH TRANSVERSE MOTION [J].
CORTELEZZI, L ;
LEONARD, A .
FLUID DYNAMICS RESEARCH, 1993, 11 (06) :263-295
[5]  
CORTELEZZI L, 1993, UNPUB PHYS FLUIDS
[6]  
DOYLE JC, 1992, FEEDBACK CONTROL THE
[7]   ROBUSTNESS IN THE PRESENCE OF MIXED PARAMETRIC UNCERTAINTY AND UNMODELED DYNAMICS [J].
FAN, MKH ;
TITS, AL ;
DOYLE, JC .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1991, 36 (01) :25-38
[8]  
GADELHAK M, 1991, T ASME, V113, P5
[10]  
KOOCHESFAHANI MM, 1988, 1ST NATL FLUID DYN C