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dc.contributor.authorGang He
dc.contributor.authorFeiyu Zhu
dc.contributor.authorYuan Ning
dc.contributor.authorHu Yang
dc.date.accessioned2025-08-17T22:30:22Z
dc.date.available2025-08-17T22:30:22Z
dc.date.copyright1/1/2025 12:00:00 AM
dc.date.issued2025
dc.identifier.otherJAEEEZ.ASENG-5673.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4307029
dc.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.
dc.publisherAmerican Society of Civil Engineers
dc.titleEffects of Wing Vein Flexibility on the Aerodynamic Characteristics of Dragonfly-Like Wings in Forward Flight
dc.typeJournal Article
dc.journal.volume38
dc.journal.issue1
dc.journal.titleJournal of Aerospace Engineering
dc.identifier.doi10.1061/JAEEEZ.ASENG-5673
dc.journal.fristpage04024105-1
dc.journal.lastpage04024105-15
dc.page15
dc.treeJournal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 001
dc.contenttypeFulltext


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