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蜻蜓转弯飞行时的翅膀运动学测量与空气动力学

Wing kinematics measurement and aerodynamics of a dragonfly in turning flight.

作者信息

Li Chengyu, Dong Haibo

机构信息

Department of Mechanical and Aerospace Engineering, University of Virginia, Charlottesville, VA 22904, United States of America.

出版信息

Bioinspir Biomim. 2017 Feb 3;12(2):026001. doi: 10.1088/1748-3190/aa5761.

DOI:10.1088/1748-3190/aa5761
PMID:28059781
Abstract

This study integrates high-speed photogrammetry, 3D surface reconstruction, and computational fluid dynamics to explore a dragonfly (Erythemis Simplicicollis) in free flight. Asymmetric wing kinematics and the associated aerodynamic characteristics of a turning dragonfly are analyzed in detail. Quantitative measurements of wing kinematics show that compared to the outer wings, the inner wings sweep more slowly with a higher angle of attack during the downstroke, whereas they flap faster with a lower angle of attack during the upstroke. The inner-outer asymmetries of wing deviations result in an oval wingtip trajectory for the inner wings and a figure-eight wingtip trajectory for the outer wings. Unsteady aerodynamics calculations indicate significantly asymmetrical force production between the inner and outer wings, especially for the forewings. Specifically, the magnitude of the drag force on the inner forewing is approximately 2.8 times greater than that on the outer forewing during the downstroke. In the upstroke, the outer forewing generates approximately 1.9 times greater peak thrust than the inner forewing. To keep the body aloft, the forewings contribute approximately 64% of the total lift, whereas the hindwings provide 36%. The effect of forewing-hindwing interaction on the aerodynamic performance is also examined. It is found that the hindwings can benefit from this interaction by decreasing power consumption by 13% without sacrificing force generation.

摘要

本研究整合了高速摄影测量、三维表面重建和计算流体动力学,以探究自由飞行中的蜻蜓(红斑蜻)。详细分析了转弯蜻蜓的不对称翅膀运动学及相关空气动力学特性。翅膀运动学的定量测量表明,与外翅相比,内翅在向下冲程期间扫动较慢,但攻角较高,而在向上冲程期间拍动较快,但攻角较低。翅膀偏差的内外不对称导致内翅的翼尖轨迹呈椭圆形,外翅的翼尖轨迹呈8字形。非定常空气动力学计算表明,内翅和外翅之间的力产生明显不对称,尤其是前翅。具体而言,在向下冲程期间,内前翅上的阻力大小约比外前翅大2.8倍。在向上冲程中,外前翅产生的峰值推力比内前翅大约大1.9倍。为了使身体保持在空中,前翅贡献了总升力的约64%,而后翅提供了36%。还研究了前翅与后翅相互作用对空气动力学性能的影响。研究发现,后翅可以通过这种相互作用受益,在不牺牲力产生的情况下将功耗降低13%。

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