空气动力学学报2025，Vol.43Issue(2)：1-26,26.DOI:10.7638/kqdlxxb-2024.0044
可悬停仿生扑翼微型飞行器气动设计综述
A review of aerodynamic design for hover-capable flapping-wing micro air vehicles
摘要
Abstract
Hover-capable flapping-wing micro air vehicles(FWMAVs),inspired by insects or hummingbirds,exhibit remarkable flight characteristics such as hovering capability,high aerodynamic efficiency at low Reynolds numbers,and strong stealthiness,offering diverse potential applications in disaster rescue,emergency response,and environmental monitoring.However,the aerodynamic forces and efficiency of their flapping wings still lag considerably behind those of their biological counterparts,adversely affecting the endurance and payload capacity of FWMAVs and significantly limiting their practical applications.This paper provides a comprehensive overview of hover-capable FWMAVs,with a focus on current research progress,theoretical and experimental methods for aerodynamic analysis,the high-lift mechanisms of insects and their applications in FWMAVs,as well as aerodynamic design methods and performance evaluation of flapping wings.The review highlights key design parameters for achieving high lift,high aerodynamic efficiency,and low noise,and elucidates the impact of these parameters on the performance of FWMAVs.Finally,future trends in aerodynamic design for hover-capable FWMAVs are discussed,offering valuable guidance for future research in this field.关键词
扑翼微型飞行器/气动设计/仿生扑翼/空气动力学/可悬停飞行Key words
flapping wing micro air vehicles/aerodynamic design/biomimetic wing/aerodynamics/hover-capable flight引用本文复制引用
程诚,陈隆,张艳来,吴江浩..可悬停仿生扑翼微型飞行器气动设计综述[J].空气动力学学报,2025,43(2):1-26,26.基金项目
国家自然科学基金面上项目(12072013) （12072013）
