Bio-inspired Flapping Wing Aerodynamics: A Review

被引:1
|
作者
De Manabendra, M. [1 ]
Sudhakar, Y. [2 ]
Gadde, Srinidhi [3 ]
Shanmugam, Deepthi [4 ]
Vengadesan, S. [5 ]
机构
[1] CSIR Natl Aerosp Labs, Syst Engn Div, Old Airport Rd, Bengaluru 560017, Karnataka, India
[2] Indian Inst Technol Goa, Sch Mech Sci, Farmagudi 403401, Goa, India
[3] Univ Twente, Water Resources Dept, Enschede, Netherlands
[4] Univ West England, Sch Engn, Frenchay Campus, Bristol BS161QY, England
[5] Indian Inst Technol Madras, Dept Appl Mech & Biomed Engn, Chennai, India
关键词
Delayed stall; Rotational circulation; Wake capture; Tandem wing; Gust effect; Ground effect; Immersed boundary method; LEADING-EDGE VORTICES; HOVERING INSECT FLIGHT; QUASI-STEADY MODEL; THRUST GENERATION; LIFT; ROTATION; FLOW; AIRFOIL; VORTEX; CLAP;
D O I
10.1007/s41745-024-00420-0
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
The design of micro aerial vehicles has been long inspired by biological flyers such as birds and insects. The aerodynamic principles of flapping wing flights are complex due to the rapid wing motion and the inherent complex vortex dynamics. Several experimental and numerical investigations have been carried out in the past decades to uncover the mechanisms responsible for the improved aerodynamic capability of flapping wings. This paper provides an overview of the aerodynamics of flapping insect wings. After providing a brief overview of the aerodynamics of a single wing, we discuss how the vortex dynamics are altered in the case of tandem wings. A significant challenge to designing a stable MAV is the environmental effects stemming from the gust and ground presence. In this paper, we present how the force generation is altered due to such effects. Moreover, we point out unsolved research questions on insect flight whose answers could greatly help to improve the design of flapping wing MAVs.
引用
收藏
页码:181 / 203
页数:23
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