Research on the aerodynamic characteristics of dragonfly leading edge

IF 2 3区 工程技术 Q2 ANATOMY & MORPHOLOGY
Yanjuan Hu, Chengyu Zhu, Qiang Liu, Duanyi Zhu, Jiaheng Xue, Qiang Li, Xiaoqin Zhou
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Abstract

Dragonflies are some of the most stable and maneuverable flying organisms. To explore the mechanism of how dragonfly leading edges enhance flight lift, this article conducts a detailed study on the leading edge veins and the microstructures on them of dragonfly wings. Observations have discovered the special leading edge vein and the regularly distributed microstructures on the leading edge vein. A biomimetic model has been established, and computational fluid dynamics (CFD) simulation analysis has been conducted on the biomimetic model. The analysis explores the effects of microstructure characteristics, distribution patterns, and positions on the aerodynamic characteristics of dragonfly gliding. The analysis shows that the leading edge structure influences the incoming flow, simultaneously promotes the formation of the leading edge vortex (LEV), and increases the lift‐to‐drag ratio by up to 4%. A wing prototype featuring biomimetic microstructures is subsequently fabricated and tested in wind tunnel experiments. Compared with a control group without leading edge structures, the airflow passing through the biomimetic structures is influenced by the shape and arrangement of these structures. The smoother transition of the leading edge vein's shape facilitates the flow of air. The microstructures primarily filter and accelerate the airflow. The spacing of the microstructures affects the stability of the airflow, thereby influencing aerodynamic performance. Additionally, the middle‐row arrangement of microstructures is more beneficial for gliding conditions, while the upper‐row arrangement is more advantageous for flapping conditions. These findings enhance our understanding of insect wings and advance micro aerial vehicle applications.Research HighlightsThis study observed the leading‐edge veins and microstructures of dragonfly wings in detail. Using a biomimetic model and computational fluid dynamics (CFD) simulations, it was found that these leading‐edge structures promote the formation of leading‐edge vortices (LEV), increasing the lift‐to‐drag ratio by up to 4%. Wind tunnel experiments demonstrated that wings with biomimetic microstructures significantly improved airflow smoothness and lift compared with control wings. Additionally, the arrangement of microstructures greatly affects airflow stability and aerodynamic performance, with middle‐row arrangements being more beneficial for gliding and upper‐row arrangements for flapping conditions. These findings enhance our understanding of insect wings and provide innovative guidance for designing efficient micro aerial vehicles.
蜻蜓前缘气动特性研究
蜻蜓是最稳定、最具机动性的飞行生物。为了探索蜻蜓前缘如何增强飞行升力的机理,本文对蜻蜓翅膀的前缘脉络及其上的微结构进行了详细研究。通过观察发现了特殊的前缘脉络和前缘脉络上有规律分布的微结构。建立了生物仿真模型,并对生物仿真模型进行了计算流体动力学(CFD)模拟分析。分析探讨了微结构特征、分布模式和位置对蜻蜓滑翔气动特性的影响。分析表明,前缘结构会影响流入的气流,同时促进前缘涡流(LEV)的形成,并使升阻比最高增加 4%。随后制作了具有仿生微结构的机翼原型,并在风洞实验中进行了测试。与没有前缘结构的对照组相比,通过仿生结构的气流受到这些结构的形状和排列的影响。前缘静脉形状的平滑过渡有利于气流的流动。微结构主要是过滤和加速气流。微结构的间距会影响气流的稳定性,从而影响空气动力性能。此外,微结构的中排排列更有利于滑翔条件,而上排排列则更有利于拍打条件。这些发现加深了我们对昆虫翅膀的了解,推动了微型飞行器的应用。研究亮点这项研究详细观察了蜻蜓翅膀的前缘脉络和微结构。利用生物仿真模型和计算流体动力学(CFD)模拟发现,这些前缘结构促进了前缘涡流(LEV)的形成,使升阻比提高了4%。风洞实验表明,与对照机翼相比,具有仿生微结构的机翼能显著改善气流平滑度和升力。此外,微结构的排列对气流稳定性和空气动力性能有很大影响,中排排列更有利于滑翔,而上排排列则更有利于拍打条件。这些发现加深了我们对昆虫翅膀的了解,并为设计高效微型航空飞行器提供了创新性指导。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Microscopy Research and Technique
Microscopy Research and Technique 医学-解剖学与形态学
CiteScore
5.30
自引率
20.00%
发文量
233
审稿时长
4.7 months
期刊介绍: Microscopy Research and Technique (MRT) publishes articles on all aspects of advanced microscopy original architecture and methodologies with applications in the biological, clinical, chemical, and materials sciences. Original basic and applied research as well as technical papers dealing with the various subsets of microscopy are encouraged. MRT is the right form for those developing new microscopy methods or using the microscope to answer key questions in basic and applied research.
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