Bio-inspired flapping wing design via a multi-objective optimization approach based on variable periodic Voronoi tessellation

This paper introduces a novel bio-inspired design methodology for flapping wings in Micro Air Vehicles aiming for achieving optimal physical properties and enhanced aerodynamic performance. The wing’s truss structures are derived through a specialized non-periodic, meso-micro scale porous structure optimization technique, termed the “Variable-Periodic Voronoi Tessellation (VPVT)” method. By incorporating critical physical properties such as compliance, natural frequency, and mass transfer efficiency, the VPVT method transforms the complex design metrics into a standard multi-objective optimization process. This approach produces a biomimetic wing design with high geometric fidelity to insect wings. The optimized VPVT design demonstrates notable physical performance improvements over natural wing samples, resulting in a 19.6% increase in stiffness, a 12.5% rise in natural frequency, and a 5.2% enhancement in mass transfer efficiency. Later, the aerodynamic performance is further evaluated via fluid–structure coupling finite element (FE) simulations. Compared to conventional commercial design, the VPVT wing exhibits optimally-tailored local stiffness, resulting in improved aeroelastic behavior during gliding action. Specifically, the FE simulations demonstrate a 7.3% reduction in drag at low angles of attack and a 9.9% increase in lift at high angles of attack. These results indicate the high energy efficiency and maneuverability of the proposed design approach, which enables the design of micro aerial vehicles (MAVs) with long duration and complex maneuverability. • Flapping wing design using a novel multi-objective, bio-inspired modeling method. • The design efficiently mimics pores geometry for nature dragonfly wing. • The improved design in global stiffness, natural frequency, and mass transfer. • The design achieves optimally-tailored local stiffness refer to nature wing. • The local stiffness implicitly improve the aerodynamics performance of wing.

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Publication Details

Journal
International Journal of Mechanical Sciences
Published
2025-03-26
DOI
https://doi.org/10.1016/j.ijmecsci.2025.110160
Citations
7
Primary Topic
Biomimetic flight and propulsion mechanisms
Type
article
Field-Weighted Citation Impact
34.95

Funders

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article

Bio-inspired flapping wing design via a multi-objective optimization approach based on variable periodic Voronoi tessellation

Zhangming Wu, Zeyang Li, Kang Gao
7 citations
International Journal of Mechanical Sciences
Biomimetic flight and propulsion mechanisms
34.95
article

Bio-inspired flapping wing design via a multi-objective optimization approach based on variable periodic Voronoi tessellation

Zhangming Wu, Zeyang Li, Kang Gao
article en
7 citations

Abstract

This paper introduces a novel bio-inspired design methodology for flapping wings in Micro Air Vehicles aiming for achieving optimal physical properties and enhanced aerodynamic performance. The wing’s truss structures are derived through a specialized non-periodic, meso-micro scale porous structure optimization technique, termed the “Variable-Periodic Voronoi Tessellation (VPVT)” method. By incorporating critical physical properties such as compliance, natural frequency, and mass transfer efficiency, the VPVT method transforms the complex design metrics into a standard multi-objective optimization process. This approach produces a biomimetic wing design with high geometric fidelity to insect wings. The optimized VPVT design demonstrates notable physical performance improvements over natural wing samples, resulting in a 19.6% increase in stiffness, a 12.5% rise in natural frequency, and a 5.2% enhancement in mass transfer efficiency. Later, the aerodynamic performance is further evaluated via fluid–structure coupling finite element (FE) simulations. Compared to conventional commercial design, the VPVT wing exhibits optimally-tailored local stiffness, resulting in improved aeroelastic behavior during gliding action. Specifically, the FE simulations demonstrate a 7.3% reduction in drag at low angles of attack and a 9.9% increase in lift at high angles of attack. These results indicate the high energy efficiency and maneuverability of the proposed design approach, which enables the design of micro aerial vehicles (MAVs) with long duration and complex maneuverability. • Flapping wing design using a novel multi-objective, bio-inspired modeling method. • The design efficiently mimics pores geometry for nature dragonfly wing. • The improved design in global stiffness, natural frequency, and mass transfer. • The design achieves optimally-tailored local stiffness refer to nature wing. • The local stiffness implicitly improve the aerodynamics performance of wing.

International Journal of Mechanical SciencesVol. 291-292
Southeast University (CN), Cardiff University (GB)
Cardiff University, Engineering and Physical Sciences Research Council
Openalex Percentile: Top 0%
Biomimetic flight and propulsion mechanisms
34.95
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