A Simulation Method for Fluid–Solid Coupling in the Flexible Wings of MAVs Based on the LBM
In this paper, a fast and accurate simulation method for the large deformation motion of anisotropic complex models is proposed. By establishing a fluid–structure interaction (FSI) coupling model based on the Lattice Boltzmann Method (LBM) and the Central Difference Method, the effect of flexible deformation on the aerodynamic performance of anisotropic wings during flapping is analyzed. The method can provide theoretical guidance and data support for the fluid–solid coupling study and the aerodynamic optimization of Micro Aerial Vehicles (MAVs).
Authors
- Liansong Peng (ORCID: https://orcid.org/0000-0003-4348-2997)
- Chen Wang (ORCID: https://orcid.org/0000-0002-5779-6295)
Institutions
- China Academy of Information and Communications Technology (CN)
Publication Details
- Published
- 2025-01-22
- DOI
- https://doi.org/10.3390/engproc2024080026
- Primary Topic
- Biomimetic flight and propulsion mechanisms
- Type
- article
- Field-Weighted Citation Impact
- 0.00