Generative design of bioinspired wings based on deployable hindwings of Anomala Corpulenta Motschulsky
•The structures and nanomechanical properties of the veins provide inspiration for bionic engineering designs.•This paper presents the simulation analysis of the structural statics and aerodynamics of 3D coupling model (HW-I and HW-II).•The 3D bionic wing (BioW) model was established and optimized u...
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Veröffentlicht in: | Micron (Oxford, England : 1993) England : 1993), 2021-12, Vol.151, p.103150-103150, Article 103150 |
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Sprache: | eng |
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Zusammenfassung: | •The structures and nanomechanical properties of the veins provide inspiration for bionic engineering designs.•This paper presents the simulation analysis of the structural statics and aerodynamics of 3D coupling model (HW-I and HW-II).•The 3D bionic wing (BioW) model was established and optimized using the generative design method.
In view of the application prospect of the hindwing of Anomala Corpulenta Motschulsky in the field of foldable Micro Aerial Vehicles (MAVs), this paper investigated the morphology, macro/microstructure of the hindwing, and the nanomechanical properties of the wing veins and the wing membrane. It revealed the variation of nanohardness and elastic modulus between different veins and different positions of the same wing veins. This paper established a 3D coupling model of the hindwing based on the principle of coupling bionics. This paper presents a simulation analysis of the structural statics (uniform load distribution) and aerodynamics (under different attack angles, flight velocities, and flapping frequencies). Two 3D coupling models (HW-I and HW-II) of the hindwing were discussed the deformation and flight aerodynamic performance of Workbenches and Fluent. On that basis, the bionic wing was generatively designed, and a 3D bionic wing (BioW) model was established using the generative design method. Simulation analyses were performed through structural statics and aerodynamics. The results showed that the stress distribution was relatively uniform and that the overall displacement deformation was minimal for the BioW model. Moreover, the BioW model had better flight efficiency and aerodynamic performance. |
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ISSN: | 0968-4328 1878-4291 |
DOI: | 10.1016/j.micron.2021.103150 |