Adjoint-based optimization of flapping plates hinged with a trailing-edge flap

被引:21
|
作者
Xu, Min [1 ]
Wei, Mingjun [1 ]
Li, Chengyu [2 ]
Dong, Haibo [2 ]
机构
[1] New Mexico State Univ, Las Cruces, NM 88003 USA
[2] Univ Virginia, Charlottesville, VA 22904 USA
关键词
Flapping wing; Trailing-edge flap; Adjoint-based optimization;
D O I
10.1016/j.taml.2014.12.005
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
It is important to understand the impact of wing-morphing on aerodynamic performance in the study of flapping-wing flight of birds and insects. We use a flapping plate hinged with a trailing-edge flap as a simplified model for flexible/morphing wings in hovering. The trailing-edge flapping motion is optimized by an adjoint-based approach. The optimized configuration suggests that the trailing-edge flap can substantially enhance the overall lift. Further analysis indicates that the lift enhancement by the trailing-edge flapping is from the change of circulation in two ways: the local circulation change by the rotational motion of the flap, and the modification of vortex shedding process by the relative location between the trailing-edge flap and leading-edge main plate. (C) 2015 The Authors. Published by Elsevier Ltd on behalf of The Chinese Society of Theoretical and Applied Mechanics.
引用
收藏
页码:1 / 4
页数:4
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