中国航空学报(英文版)2024,Vol.37Issue(2) :259-269.DOI:10.1016/j.cja.2023.09.030

Reynolds-number scaling analysis on lift generation of a flapping and passive rotating wing with an inhomogeneous mass distribution

Suyang QIN Haotian HANG Yang XIANG Hong LIU
中国航空学报(英文版)2024,Vol.37Issue(2) :259-269.DOI:10.1016/j.cja.2023.09.030

Reynolds-number scaling analysis on lift generation of a flapping and passive rotating wing with an inhomogeneous mass distribution

Suyang QIN 1Haotian HANG 1Yang XIANG 1Hong LIU1
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作者信息

  • 1. J.C.Wu Center for Aerodynamics,School of Aeronautics and Astronautics,Shanghai Jiao Tong University,Shanghai 200240,China
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Abstract

Insects usually fly by passively rotating wings,which has been applied to the design of flapping-wing Micro-Air Vehicles(MAVs)to reduce mechanical complexity.In this paper,a robotic passive rotating-wing model is designed to investigate wing kinematics and lift generation,which are measured by a high-speed camera and a force transducer,respectively.In addition,flow fields are measured using the Particle Image Velocimetry(PIV).Experimental results demonstrate that passive rotating motion has a coordinative relationship with actively stroking motion.As the stroke amplitude or frequency increases,the rotating amplitude is enlarged.To characterize the active stroking motion,a driving Reynolds number Redriving is defined,which varies from 68 to 366 in this study.Moving the gravity center of the wing towards trailing edge induces the increase of additional torque M,which decreases the wing rotating amplitude and promotes the advance of wing rotation.We find that the timing of wing rotation is gradually delayed and the mean lift coefficient CL mono-tonously decreases as Redriying increases.By increasing the additional torque M,CL is slightly improved and approaches to the lift coefficient of a real fruit fly at driving Re approximately equal to 230.The instantaneous lifts combined with the vortical structures further demonstrate that the lift generation associated with wing rotation is mainly attributed to the growth of the Leading-Edge Vortex(LEV)and the passive wake capture mechanism.Passive wake capture is influenced by LEV,reversal stroke motion and wing additional torque together,which can only maintain the lift at a high level for a considerable period.The high-lift generation mechanisms of flapping and passive rotating flight could shed light on the simplified design of MAVs and the improvement of their aerodynamic performance.

Key words

Flapping flight/Unsteady lift/Passive rotation/Vortex flow/Leading-edge vortex

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基金项目

National Nature Science Foundation of China(12102259)

National Nature Science Foundation of China(12202273)

China Postdoctoral Science Foundation(2018M642007)

出版年

2024
中国航空学报(英文版)
中国航空学会

中国航空学报(英文版)

CSTPCDEI
影响因子:0.847
ISSN:1000-9361
参考文献量4
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