Numerical analysis on transitions and symmetry-breaking in the wake of a flapping foil

被引:0
|
作者
Guo-Yi He
Qi Wang
Xing Zhang
Shu-Guang Zhang
机构
[1] Nanchang Hangkong University,The School of Aircraft Engineering
[2] Chinese Academy of Sciences,LNM, Institute of Mechanics
[3] Beihang University,The School of Transportation Science and Engineering
来源
Acta Mechanica Sinica | 2012年 / 28卷
关键词
Flapping motion; Immersed boundary method; Wake; Symmetry-breaking;
D O I
暂无
中图分类号
学科分类号
摘要
Flying and marine animals often use flapping wings or tails to generate thrust. In this paper, we will use the simplest flapping model with a sinusoidal pitching motion over a range of frequency and amplitude to investigate the mechanism of thrust generation. Previous work focuses on the Karman vortex street and the reversed Karman vortex street but the transition between two states remains unknown. The present numerical simulation provides a complete scenario of flow patterns from the Karman vortex street to reversed Karman vortex street via aligned vortices and the ultimate state is the deflected Karman vortex street, as the parameters of flapping motions change. The results are in agreement with the previous experiment. We make further discussion on the relationship of the observed states with drag and thrust coefficients and explore the mechanism of enhanced thrust generation using flapping motions.
引用
收藏
页码:1551 / 1556
页数:5
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