Control of vortical structures on a flapping wing via a sinusoidal leading-edge

被引:24
|
作者
Ozen, C. A. [1 ]
Rockwell, D. [1 ]
机构
[1] Lehigh Univ, Dept Mech Engn & Mech, Packard Lab 356, Bethlehem, PA 18015 USA
关键词
STALL;
D O I
10.1063/1.3304539
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The flow structure generated by a flapping wing in the form of a plate is fundamentally altered if the leading-edge has a sinusoidal shape. It is possible to attenuate both the positive and negative spanwise flows along the plate surface, as well as the onset and development of large-scale concentrations of positive and negative streamwise vorticities at inboard locations. These alterations of the inboard flow structure have an insignificant influence on the structure of the tip vortex. (C) 2010 American Institute of Physics. [doi:10.1063/1.3304539]
引用
收藏
页码:1 / 3
页数:3
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