首页|Aerodynamic Performance of Three Flapping Wings with Unequal Spacing in Tandem Formation

Aerodynamic Performance of Three Flapping Wings with Unequal Spacing in Tandem Formation

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To better understand the aerodynamic reasons for highly organized movements of flying organisms,the three-flapping wing system in tandem formation was studied numerically in this paper.Different from previous relevant studies on the multiple flapping wings that are equally spaced,this study emphasizes the impact of unequal spacing between individuals on the aerodynamics of each individual wing as well as the whole system.It is found that swapping the distance between the first and second wing with the distance between the second wing and the rearmost wing does not affect the overall aerodynamic performance,but significantly changes the distribution of aerodynamic benefits across each wing.During the whole flap-ping cycle,three effects are at play.The narrow channel effect and the downwash effect can promote and weaken the wing lift,respectively,while the wake capture effect can boost the thrust.It also shows that these effects could be manipulated by changing the spacing between adjacent wings.These findings provide a novel way for flow control in tandem formation flight and are also inspiring for designing the formation flight of bionic aircraft.

Three flapping wingsUnequal spacingAerodynamic performanceTandem formation

Min Chang、Ziyi Xu、Zengshuang Chen、Li Li、Xueguang Meng

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Unmanned System Research Institute,National Key Laboratory of Unmanned Aerial Vehicle Technology,Northwestern Polytechnical University,Xi'an 710072,People's Republic of China

State Key Laboratory for Strength and Vibration of Mechanical Structures,School of Aerospace Engineering,Xi'an Jiaotong University,Xi'an 710049,People's Republic of China

Xi'an Aeronautics Computing Technique Research Institute,Aviation Industry Corporation of China,Xi'an 710076,People's Republic of China

国家自然科学基金Shaanxi key research and development program

121722762022ZDLGY02-07

2024

仿生工程学报(英文版)
吉林大学

仿生工程学报(英文版)

CSTPCDEI
影响因子:0.837
ISSN:1672-6529
年,卷(期):2024.21(4)
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