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Flow Visualization of Rhinoceros Beetle (Trypoxylus dichotomus) in Free Flight

机译:犀牛甲虫(Trypoxylus dichotomus)在自由飞行中的流动可视化

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摘要

Aerodynamic characteristics of the beetle,Trypoxylus dichotomus,which has a pair of elytra (forewings) and flexible hind wings,are investigated.Visualization experiments were conducted for various flight conditions of a beetle,Trypoxylus dichotomus:free,tethered,hovering,forward and climbing flights.Leading edge,trailing edge and tip vortices on both wings were observed clearly.The leading edge vortex was stable and remained on the top surface of the elytron for a wide interval during the downstroke of free forward flight.Hence,the elytron may have a considerable role in lift force generation of the beetle.In addition,we reveal a suction phenomenon between the gaps of the hind wing and the elytron in upstroke that may improve the positive lift force on the hind wing.We also found the reverse clap-fling mechanism of the T.dichotomus beetle in hovering flight.The hind wings touch together at the beginning of the upstroke.The vortex generation,shedding and interaction give a better understanding of the detailed aerodynamic mechanism of beetle flight.
机译:研究了具有一对鞘翅(前翅)和后肢柔性翼的甲虫Trypoxylus dichotomus的气动特性。针对甲虫,Trypoxylus dichotomus的各种飞行条件进行了可视化实验:自由,系留,悬停,盘旋,向前和爬清楚地观察到了两个机翼上的前缘,后缘和尖端涡旋。前缘涡旋是稳定的,并且在自由向前飞行的下降过程中在电子升速器的顶面上保持了很宽的间隔。因此,电子升速器可能具有此外,我们还揭示了上翼后翼与elytron间隙之间的吸力现象,可以改善后翼上的正升力。我们还发现了反向拍打- T.dichotomus甲虫在盘旋飞行中的逃逸机制。后翼在上冲程开始时相互接触。涡流的产生,脱落和相互作用提供了更好的下潜了解甲虫飞行的详细空气动力学机理。

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  • 来源
    《仿生工程学报(英文版)》 |2012年第3期|304-314|共11页
  • 作者单位

    Department of Aerospace Information Engineering, Konkuk University, Seoul 143-701, Republic of Korea;

    Costal Engineering and Ocean Energy Research Department, Korea Ocean Research and Development Institute,454 Haeanro Sangrok-gu Ansan 426-744, Republic of Korea;

    Department of Aerospace Information Engineering, Konkuk University, Seoul 143-701, Republic of Korea;

    Department of Advanced Technology Fusion, Konkuk University, Seoul 143-701, Republic of Korea;

    Department of Aerospace Information Engineering, Konkuk University, Seoul 143-701, Republic of Korea;

    Department of Mechanical Engineering, Sungkyunkwan University, Suwon 440-746, Republic of Korea;

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