Thrust performance of a flexible low-aspect-ratio pitching plate

被引:61
|
作者
Dai, Hu [1 ]
Luo, Haoxiang [1 ]
de Sousa, Paulo J. S. A. Ferreira [1 ]
Doyle, James F. [2 ]
机构
[1] Vanderbilt Univ, Dept Mech Engn, Nashville, TN 37235 USA
[2] Purdue Univ, Sch Aeronaut & Astronaut, W Lafayette, IN 47907 USA
基金
美国国家科学基金会;
关键词
WAKE STRUCTURE; OSCILLATING FOILS; FLAPPING FOIL; AIRFOIL; GENERATION; EFFICIENCY; PANEL;
D O I
10.1063/1.4764047
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
We numerically investigate the hydrodynamic performance of an elastic plate of aspect ratio 0.54 and mass ratio 0.1 that pitches around its leading edge in a free stream at Reynolds number 640. It is found that for the rigid plate and the flexible plate with the first-mode deformation, the thrust coefficient nearly collapses onto the same curve when plotted against the Strouhal number that is defined using the tail excursion. Exceptions are found when the plate is overly flexible and higher deformation modes take place. On the other hand, the flexible plate has significantly higher power efficiency than the rigid plate at the same Strouhal number. Like the rigid plate, wake transition is observed for the flexible plate as the Strouhal number is varied. Specifically, at low Strouhal numbers (St < 0.28) the wake consists of a chain of interlocked horseshoe-shape vortices; at high Strouhal numbers (St > 0.28), the wake turns into two trains of closed vortex rings with hairpin legs. (C) 2012 American Institute of Physics. [http://dx.doi.org/10.1063/1.4764047]
引用
收藏
页数:9
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