Aerodynamic effects of flexibility in flapping wings

被引:224
|
作者
Zhao, Liang [1 ]
Huang, Qingfeng [1 ]
Deng, Xinyan [1 ]
Sane, Sanjay P. [2 ]
机构
[1] Univ Delaware, Dept Mech Engn, Spencer Lab 126, Newark, DE 19716 USA
[2] Tata Inst Fundamental Res, Natl Ctr Biol Sci, Bangalore 560065, Karnataka, India
基金
美国国家科学基金会;
关键词
flexible wings; flapping flight; aerodynamics; FLUID-STRUCTURE INTERACTION; HOVERING INSECT FLIGHT; UNSTEADY AERODYNAMICS; FUNCTIONAL-MORPHOLOGY; FLEXURAL STIFFNESS; REVOLVING WINGS; FLEXIBLE WINGS; FORCE; KINEMATICS; MODEL;
D O I
10.1098/rsif.2009.0200
中图分类号
O [数理科学和化学]; P [天文学、地球科学]; Q [生物科学]; N [自然科学总论];
学科分类号
07 ; 0710 ; 09 ;
摘要
Recent work on the aerodynamics of flapping flight reveals fundamental differences in the mechanisms of aerodynamic force generation between fixed and flapping wings. When fixed wings translate at high angles of attack, they periodically generate and shed leading and trailing edge vortices as reflected in their fluctuating aerodynamic force traces and associated flow visualization. In contrast, wings flapping at high angles of attack generate stable leading edge vorticity, which persists throughout the duration of the stroke and enhances mean aerodynamic forces. Here, we show that aerodynamic forces can be controlled by altering the trailing edge flexibility of a flapping wing. We used a dynamically scaled mechanical model of flapping flight (Re approximate to 2000) to measure the aerodynamic forces on flapping wings of variable flexural stiffness (EI). For low to medium angles of attack, as flexibility of the wing increases, its ability to generate aerodynamic forces decreases monotonically but its lift-to-drag ratios remain approximately constant. The instantaneous force traces reveal no major differences in the underlying modes of force generation for flexible and rigid wings, but the magnitude of force, the angle of net force vector and centre of pressure all vary systematically with wing flexibility. Even a rudimentary framework of wing veins is sufficient to restore the ability of flexible wings to generate forces at near-rigid values. Thus, the magnitude of force generation can be controlled by modulating the trailing edge flexibility and thereby controlling the magnitude of the leading edge vorticity. To characterize this, we have generated a detailed database of aerodynamic forces as a function of several variables including material properties, kinematics, aerodynamic forces and centre of pressure, which can also be used to help validate computational models of aeroelastic flapping wings. These experiments will also be useful for wing design for small robotic insects and, to a limited extent, in understanding the aerodynamics of flapping insect wings.
引用
收藏
页码:485 / 497
页数:13
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