中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid

Aerodynamic performance of a bio-inspired flapping wing with local sweep morphing

文献类型:期刊论文

作者Wang, Chunyu1,2; Liu, Yi1,2; Xu, Duo1,2; Wang, Shizhao1,2; Xu D(徐多); Wang SZ(王士召); Xu D(徐多); Wang SZ(王士召); Wang SZ(王士召); Wang SZ(王士召)
刊名PHYSICS OF FLUIDS
出版日期2022-05-01
卷号34期号:5页码:16
ISSN号1070-6631
DOI10.1063/5.0090718
通讯作者Wang, Shizhao(wangsz@lnm.imech.ac.cn)
英文摘要Birds and bats frequently reconfigure their wing planform through a combination of flapping and local sweep morphing, suggesting a possible approach for improving the performance of micro aerial vehicles. We explore the effects of combined flapping and local sweep morphing on aerodynamic performance by employing a bio-inspired two-jointed flapping wing with local sweep morphing. The bio-inspired wing consists of inner and outer sections, which flap around the root joint (shoulder) and the midspan joint (wrist), respectively. The aerodynamic forces and the unsteady vortex structures are evaluated by numerically solving the incompressible Navier-Stokes equations. The results show that combined flapping and local sweep morphing can significantly enhance the aerodynamic performance. In particular, the average lift coefficient is 1.50 times greater than that of simple gliding with single local sweep morphing. Combined flapping and local sweep morphing also have a relatively high pitch moment and shift the aerodynamic center position backward, producing advantages in terms of maneuverability/agility and stability. We find that the vortex structures associated with the combined motion feature midspan vortices, which arise from the leading-edge vortices of the inner wing and contribute to the enhanced aerodynamic performance. We show that the kinematics of combined flapping and local sweep morphing can be further optimized if the midspan vortices are captured by the outer wing. Published under an exclusive license by AIP Publishing.& nbsp;& nbsp;
WOS关键词WIDE-RANGE ; FLIGHT ; DESIGN ; KINEMATICS ; LIFT ; AIRCRAFT ; VORTICES ; PLATE ; MODEL ; RATIO
资助项目National Natural Science Foundation of China (NSFC) Basic Science Center Program for Multiscale Problems in Nonlinear Mechanics[11988102] ; NSFC[11922214] ; NSFC[91752118]
WOS研究方向Mechanics ; Physics
语种英语
WOS记录号WOS:000795706900009
资助机构National Natural Science Foundation of China (NSFC) Basic Science Center Program for Multiscale Problems in Nonlinear Mechanics ; NSFC
源URL[http://dspace.imech.ac.cn/handle/311007/89384]  
专题力学研究所_非线性力学国家重点实验室
通讯作者Wang, Shizhao
作者单位1.Univ Chinese Acad Sci, Sch Engn Sci, Beijing 101408, Peoples R China
2.Chinese Acad Sci, Inst Mech, State Key Lab Nonlinear Mech, Beijing 100190, Peoples R China
推荐引用方式
GB/T 7714
Wang, Chunyu,Liu, Yi,Xu, Duo,et al.

Aerodynamic performance of a bio-inspired flapping wing with local sweep morphing

[J]. PHYSICS OF FLUIDS,2022,34(5):16.
APA Wang, Chunyu.,Liu, Yi.,Xu, Duo.,Wang, Shizhao.,徐多.,...&Wang SZ.(2022).

Aerodynamic performance of a bio-inspired flapping wing with local sweep morphing

.PHYSICS OF FLUIDS,34(5),16.
MLA Wang, Chunyu,et al."

Aerodynamic performance of a bio-inspired flapping wing with local sweep morphing

".PHYSICS OF FLUIDS 34.5(2022):16.

入库方式: OAI收割

来源:力学研究所

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