【2h】

The vortex wake of a hovering model hawkmoth

机译:盘旋式鹰蛾的旋涡唤醒

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摘要

Visualization experiments with Manduca sexta have revealed the presence of a leading-edge vortex and a highly three-dimensional flow pattern. To further investigate this important discovery, a scaled-up robotic insect was built (the 'flapper') which could mimic the complex movements of the wings of a hovering hawkmoth. Smoke released from the leading edge of the flapper wing revealed a small but strong leading-edge vortex on the downstroke. This vortex had a high axial flow velocity and was stable, separating from the wing at approximately 75 per cent of the wing length. It connected to a large, tangled tip vortex, extending back to a combining stopping and starting vortex from pronation. At the end of the downstroke, the wake could be approximated as one vortex ring per wing. Based on the size and velocity of the vortex rings, the mean lift force during the downstroke was estimated to be about 1.5 times the body weight of a hawkmoth, confirming that the downstroke is the main provider of lift force.
机译:Manduca sexta的可视化实验已经揭示了前沿涡流和高度三维流动模式的存在。为了进一步研究这一重要发现,人们制造了一种可以模仿鹰蛾盘旋翅膀的复杂运动的大型昆虫(“挡板”)。从挡板机翼前缘释放的烟雾在下风时显示出很小但很强的前缘涡流。该涡流具有较高的轴向流速,并且很稳定,在机翼长度的大约75%处与机翼分开。它与一个大的,纠结的尖端涡旋相连,并从内旋一直延伸到停止和起始涡旋的组合。在下冲程结束时,尾流可以近似为每个机翼一个涡流环。根据涡流环的大小和速度,在下冲程期间的平均举升力估计约为鹰蛾体重的1.5倍,这证实了下冲程是举升力的主要来源。

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