TY - JOUR
T1 - 鸟翼空气动力学机理的研究现状和进展综述
AU - Song, Bi Feng
AU - Lang, Xin Yu
AU - Xue, Dong
AU - Yang, Wen Qing
AU - Bao, Han
AU - Liu, Dan
AU - Wu, Tao
AU - Liu, Kang
AU - Song, Wen Ping
AU - Wang, Yue
N1 - Publisher Copyright:
© 2022 Chinese Academy of Sciences. All rights reserved.
PY - 2022
Y1 - 2022
N2 - First, this paper tries to review, summarize, and analyze the current status and problems of the aerodynamic mechanism research on the independent and coupling effects among the four factors that would affect the aerodynamic characteristics of bird wings—objectively and comprehensively. Second, based on the analysis and study of the current research results, according to the progress and limitations of calculation and experimental means, the paper puts forward the problems, strategies, and methods that need further study. The four main factors considered in this paper include the static geometric shape of the bird’s wing, four kinematic modes, the dynamic chord- and span-wise flexible deformation of the wing, and three kinds of small-scale flow-control structures that have recently attracted more attention. In this paper, in full consideration of wing static geometry appearance, kinematic modes, and dynamic, flexible deformation, by the analysis of the forces and vortex on a bird’s wing, the strategies and methods to further clarify the individual aerodynamic mechanism and function of the three small-scale flow-control structures are proposed. Furthermore, under the condition of mutual coupling among the four factors, the strategies and methods to obtain the aerodynamic mechanism of a real bird wing are also put forward. The viewpoints, methods, and conclusions of this paper have guiding and reference value for improving a bionic aircraft.
AB - First, this paper tries to review, summarize, and analyze the current status and problems of the aerodynamic mechanism research on the independent and coupling effects among the four factors that would affect the aerodynamic characteristics of bird wings—objectively and comprehensively. Second, based on the analysis and study of the current research results, according to the progress and limitations of calculation and experimental means, the paper puts forward the problems, strategies, and methods that need further study. The four main factors considered in this paper include the static geometric shape of the bird’s wing, four kinematic modes, the dynamic chord- and span-wise flexible deformation of the wing, and three kinds of small-scale flow-control structures that have recently attracted more attention. In this paper, in full consideration of wing static geometry appearance, kinematic modes, and dynamic, flexible deformation, by the analysis of the forces and vortex on a bird’s wing, the strategies and methods to further clarify the individual aerodynamic mechanism and function of the three small-scale flow-control structures are proposed. Furthermore, under the condition of mutual coupling among the four factors, the strategies and methods to obtain the aerodynamic mechanism of a real bird wing are also put forward. The viewpoints, methods, and conclusions of this paper have guiding and reference value for improving a bionic aircraft.
KW - alula
KW - bird flight mechanism
KW - flapping wing
KW - leading
KW - trailing edge serrations
KW - wingtip slit
UR - http://www.scopus.com/inward/record.url?scp=85139418958&partnerID=8YFLogxK
U2 - 10.1360/SST-2020-0515
DO - 10.1360/SST-2020-0515
M3 - 文献综述
AN - SCOPUS:85139418958
SN - 1674-7259
VL - 52
SP - 893
EP - 910
JO - Zhongguo Kexue Jishu Kexue/Scientia Sinica Technologica
JF - Zhongguo Kexue Jishu Kexue/Scientia Sinica Technologica
IS - 6
ER -