Wake Behavior Around Flapping Wings of Model Hawkmoth Moving Sideways

Jong-Seob Han, Jae-Hung Han
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Abstract

This study investigated nearwake behaviors around flapping wings moving sideways. A dynamically scaled-up flapping manipulator was installed on a servo-driven towing carriage to give the sideways movement. In the single wing configuration, the wing in the windward side did not encounter any noticeable effects on the aerodynamic characteristics. The wing in the leeward side, on the other hand, experienced a substantial lift augmentation. We found a stretched leading-edge vortex (LEV) on the wing in the leeward side, implying the additional feeding flux into the LEV. In this case, the moving sideways gave a continuous lateral wind, which became the source to maintain the lift augmentation with the less downward component. We also found that the moving sideways rather intensified the interaction between the wake of the wing in the windward side and the contralateral wing, i.e., the wing-wake interaction. Accordingly, the lift augmentation on the wing in the leeward side practically disappeared by the wing-wake interaction. A digital particle image velocimetry for nearwake behaviors found the less developed trailing-edge shear layer and wingroot vortex traces. This implied that the massive downwash induced by the wing in the windward side was the main source to neutralize the lift augmentation on the contralateral wing.
模型飞蛾横向运动时振翅周围的尾迹行为
这项研究调查了扑翼侧向运动时的近尾流行为。在伺服驱动的拖曳架上安装了一个动态放大的扑动机械手来实现横向运动。在单翼结构中,迎风侧的机翼对气动特性没有任何明显的影响。另一方面,背风侧的机翼经历了相当大的升力增强。在机翼下风侧发现了一个被拉伸的前缘涡(LEV),这意味着有额外的进给通量进入了前缘涡。在这种情况下,侧向运动产生了持续的侧向风,这成为维持升力增强的来源,而向下的分量较少。我们还发现侧向运动反而加剧了迎风侧机翼尾流与对侧机翼之间的相互作用,即翼-尾流相互作用。因此,在背风侧机翼上的升力增强在翼-尾流相互作用下几乎消失。近尾流特性的数字粒子图像测速发现了欠发达的尾缘剪切层和翼根涡迹。这意味着迎风侧机翼引起的大量下洗是抵消对侧机翼升力增强的主要来源。
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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