Scaling of flow separation on a pitching low aspect ratio plate

被引:18
|
作者
Yilmaz, T. [1 ]
Ol, M. [2 ]
Rockwell, D. [1 ]
机构
[1] Lehigh Univ, Dept Mech Engn & Mech, Bethlehem, PA 18015 USA
[2] USAF, Res Lab, Air Vehicles Directorate, Wright Patterson AFB, OH 45433 USA
关键词
Aerodynamics; Unsteady flow; Vortices; Flow-structure interaction; Separated flows; Visualization; WAKE STRUCTURE; PERFORMANCE;
D O I
10.1016/j.jfluidstructs.2010.07.003
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
We use two different dye injection approaches, in two different water tunnels, to visualize the formation and subsequent evolution of leading-edge vortices and related separated structures, for a pitching low aspect ratio plate. The motion is a smoothed linear pitch ramp from 0 degrees to 40 degrees incidence, brief hold, and return to 0 degrees, executed at reduced pitch rates ranging from 0.1 to 0.35 and about various pivot locations. All cases evince a leading edge vortex with pronounced axial flow, which leads to formation of large-scale, three-dimensional flow structures, culminating in a large vortical structure centered at the wing symmetry plane. Pitch is also compared to plunge, where the plunge-induced angle of attack is taken as the geometric pitch incidence angle, ignoring pitch-rate effects. At successively increasing values of convective time C/U, the three-dimensional patterns of the flow structure are remarkably similar for the pitching and plunging motions. The similarity of these patterns persists, though they are shifted in time, for variation of either the location of the pitching axis or the dimensionless pitch rate. (C) 2010 Elsevier Ltd. All rights reserved.
引用
收藏
页码:1034 / 1041
页数:8
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