The control of flow separation by periodic excitation

被引:683
作者
Greenblatt, D [1 ]
Wygnanski, IJ [1 ]
机构
[1] Tel Aviv Univ, Fac Engn, Dept Fluid Mech & Heat Transfer, IL-69978 Tel Aviv, Israel
关键词
D O I
10.1016/S0376-0421(00)00008-7
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper presents a review of the control of flow separation from solid surfaces by periodic excitation. The emphasis is placed on experimentation relating to hydrodynamic excitation, although acoustic methods as well as traditional boundary layer control, such as steady blowing and suction, are discussed in order to provide an appropriate historical context for recent developments. The review examines some aspects of the excited plane mixing-layer and shows how its development lays the foundation for a basic understanding of the problem. Flow attachment to, and separation from, a deflected flap is then shown to be a paradigm for isolating controlling parameters as well as understanding the basic mechanisms involved. Particular attention is paid to separation control on airfoils by considering controlling parameters such as optimum reduced frequencies and excitation levels, performance enhancement, efficiency, reduction of post-stall unsteadiness, compressibility and other important features. Additional topics covered include excitation of separation bubbles, control and exploitation of diffuser hows, three-dimensional effects, the influence of longitudinal curvature and possible applications to unmanned air vehicles. The review closes with some recent developments in the control and understanding of incompressible dynamic stall, specifically illustrating the control of dynamic stall on oscillating airfoils and identifying the crucial time-scale disparity between dynamic stall and periodic excitation. (C) 2000 Elsevier Science Ltd. All rights reserved.
引用
收藏
页码:487 / 545
页数:59
相关论文
共 214 条
[1]  
ADDINGTON GA, 1992, 922628GP AIAA
[2]  
Ahuja K. K., 1984, AIAA Paper No. 84-2298
[3]  
Ahuja K. K., 1983, 830726 AIAA
[4]  
AMITAY M, 1998, 36 AER SCI M EXH REN
[5]  
Anderson J.D., 1989, INTRO FLIGHT
[6]  
ATTINELLO JS, 1952, DR1745 BUR AER RES D
[7]  
ATTINELLO JS, 1961, BOUNDARY LAYER FLOW, V1, P463
[8]  
BACHAR T, 1998, APS M
[9]  
BACHAR T, 1998, ALTERNATING FLOW GEN
[10]   SEPARATION CONTROL ON AN AIRFOIL BY PERIODIC FORCING [J].
BARSEVER, A .
AIAA JOURNAL, 1989, 27 (06) :820-821