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contributor authorGang He
contributor authorFeiyu Zhu
contributor authorYuan Ning
contributor authorHu Yang
date accessioned2025-08-17T22:30:22Z
date available2025-08-17T22:30:22Z
date copyright1/1/2025 12:00:00 AM
date issued2025
identifier otherJAEEEZ.ASENG-5673.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4307029
description abstractThe passive deformation of the flexible wing plays a crucial role in enabling insects to generate high lift and efficient flight. This study aims to investigate the impact of wing vein flexibility distributions on the aerodynamic characteristics of an imitation dragonfly wing during flapping forward flight. The structural deformation and the flow field characteristics of the flapping wing model under different degrees of freedom are studied for three cases: uniform flexibility, nonuniform flexibility, and rigidity. The nonuniform flexible distribution is modeled by command flow, and the bidirectional fluid–structure coupling technology is used to model the interaction between structure and fluid. The results indicate that the nonuniform flexible distribution can significantly improve the peak thrust coefficients and time-averaged thrust coefficients in the flapping condition, as well as the thrust duration in the flapping-torsion condition. In the former condition, the flexible wing primarily exhibits spreading deformation. In the latter condition, it involves both spreading and chordal bending deformation. Based on the vortex theory, it is observed that the flexible wing generates stronger and wider vortices compared with the rigid wing, forming a vortex ring that contributes to the wing’s high lift. Consequently, the flexible wing exhibits superior aerodynamic performance. The numerical examples suggest that the nonuniform flexible distribution is optimal for the imitation dragonfly wing.
publisherAmerican Society of Civil Engineers
titleEffects of Wing Vein Flexibility on the Aerodynamic Characteristics of Dragonfly-Like Wings in Forward Flight
typeJournal Article
journal volume38
journal issue1
journal titleJournal of Aerospace Engineering
identifier doi10.1061/JAEEEZ.ASENG-5673
journal fristpage04024105-1
journal lastpage04024105-15
page15
treeJournal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 001
contenttypeFulltext


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