蜻蜓向前飞行的比例力学模型的力测量

W. Lai, J. Yan, M. Motamed, S. Green
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引用次数: 15

摘要

为了研究昆虫尺度扑翼的气动现象和飞行性能,建立了一个动态缩放的扑翼模型。该机构由两个机翼组成,每个机翼有3个旋转自由度,安装在一个线性平台上,以便在充满液体的水箱中进行平移。每个机翼都配备了一个传感器,用于即时测量随时间变化的力和扭矩。这种设置允许一个翅膀被指定为前翼,另一个被指定为后翼,以便分析它们之间的相互作用,以了解四翼昆虫的飞行。该装置是多功能的,足以探索一系列的机翼形态以及操作翼的轨迹参数
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Force measurements on a scaled mechanical model of dragonfly in forward flight
A dynamically scaled flapping-wing model has been developed to investigate the aerodynamic phenomena and flight performance of insect-scale flapping wings. The mechanism consists of two wings, each having 3 rotational degrees of freedom, mounted on a linear stage to permit translation in a fluid-filled tank. Each wing is equipped with a sensor for instantaneous measurement of the time-varying forces and torques. The setup permits one wing to be designated as the fore wing and the other as the hind wing so that interactions between them can be analysed to understand flight for four-winged insects. The apparatus is versatile enough to explore a range of wing morphologies as well as operational wing trajectory parameters
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