Numerical analysis of the three-dimensional aerodynamics of a hovering rufous hummingbird (Selasphorus rufus)

被引:6
|
作者
Yang, Songyuan [1 ,2 ]
Zhang, Weiping [1 ]
机构
[1] Shanghai Jiao Tong Univ, Shanghai Key Lab Navigat & Locat Based Serv, Natl Key Lab Nano Micro Fabricat Techno,Key Lab T, Dept Micronano Elect,Minist Educ,Sch Elect Inform, Shanghai 200240, Peoples R China
[2] Nanyang Technol Univ, Sch Mech & Aerosp Engn, Singapore 639798, Singapore
关键词
Rufous hummingbird; Selasphorus rufus; Hovering; Aerodynamics; Computational fluid dynamics (CFD); LEADING-EDGE VORTEX; FLIGHT; FORCES; FLOW; KINEMATICS; WINGS;
D O I
10.1007/s10409-015-0450-5
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Hummingbirds have a unique way of hovering. However, only a few published papers have gone into details of the corresponding three-dimensional vortex structures and transient aerodynamic forces. In order to deepen the understanding in these two realms, this article presents an integrated computational fluid dynamics study on the hovering aerodynamics of a rufous hummingbird. The original morphological and kinematic data came from a former researcher's experiments. We found that conical and stable leading-edge vortices (LEVs) with spanwise flow inside their cores existed on the hovering hummingbird's wing surfaces. When the LEVs and other near-field vortices were all shed into the wake after stroke reversals, periodically shed bilateral vortex rings were formed. In addition, a strong downwash was present throughout the flapping cycle. Time histories of lift and drag were also obtained. Combining the three-dimensional flow field and time history of lift, we believe that high lift mechanisms (i.e., rotational circulation and wake capture) which take place at stroke reversals in insect flight was not evident here. For mean lift throughout a whole cycle, it is calculated to be 3.60 g (104.0 % of the weight support). The downstroke and upstroke provide 64.2 % and 35.8 % of the weight support, respectively.
引用
收藏
页码:931 / 943
页数:13
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