A review of bird-like flapping wing with high aspect ratio

被引:20
作者
Xie, Changchuan [1 ]
Gao, Nongyue [1 ]
Meng, Yang [1 ]
Wu, Yue [1 ]
Yang, Chao [1 ]
机构
[1] Beihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China
关键词
Aeroelasticity; Bird-like flapping wing; Flapping motion; High aspect ratio; Modeling; Nonlinear; VORTEX-LATTICE METHOD; MICRO AIR VEHICLE; LEADING-EDGE VORTEX; AERODYNAMIC PERFORMANCE; NONLINEAR AEROELASTICITY; UNSTEADY AERODYNAMICS; PROPULSIVE EFFICIENCY; NUMERICAL-SIMULATION; FLIGHT FEATHERS; ANIMAL FLIGHT;
D O I
10.1016/j.cja.2022.06.009
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Bird-like flapping-wing vehicles with a high aspect ratio have the potential to fulfill mis-sions given to micro air vehicles, such as high-altitude reconnaissance, surveillance, rescue, and bird group guidance, due to their good loading and long endurance capacities. Biologists and aeronau-tical researchers have explored the mystery of avian flight and made efforts to reproduce flapping flight in bioinspired aircraft for decades. However, the cognitive depth from theory to practice is still very limited. The mechanism of generating sufficient lift and thrust during avian flight is still not fully understood. Moving wings with unique biological structures such as feathers make mod-eling, simulation, experimentation, and analysis much more difficult. This paper reviews the research progress on bird-like flapping wings from flight mechanisms to modeling. Commonly used numerical computing methods are briefly compared. The aeroelastic problems are also highlighted. The results of the investigation show that a leading-edge vortex can be found during avian flight. Its induction and maintenance may have a close relationship with wing configuration, kinematics and deformation. The present models of flapping wings are mainly two-dimensional airfoils or three-dimensional single root-jointed geometric plates, which still exhibit large differences from real bird wings. Aeroelasticity is encouraged to consider the nonignorable effect on aerodynamic perfor-mance due to large-scale nonlinear deformation. Introducing appropriate flexibility can improve the peak values and efficiencies of lift and thrust, but the detailed conclusions always have strong background dependence.(c) 2022 Chinese Society of Aeronautics and Astronautics. Production and hosting by Elsevier Ltd. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).
引用
收藏
页码:22 / 44
页数:23
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