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Flow visualization and unsteady aerodynamics in the flight of the hawkmoth Manduca sexta

机译:鹰蛾Manduca sexta飞行中的流动可视化和非定常空气动力学

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摘要

The aerodynamic mechanisms employed durng the flight of the hawkmoth, Manduca sexta, have been investigated through smoke visualization studies with tethered moths. Details of the flow around the wings and of the overall wake structure were recorded as stereophotographs and high-speed video sequences. The changes in flow which accompanied increases in flight speed from 0.4 to 5.7 m s-1 were analysed. The wake consists of an alternating series of horizontal and vertical vortex rings which are generated by successive down- and upstrokes, respectively. The downstroke produces significantly more lift than the upstroke due to a leading-edge vortex which is stabilized by a radia flow moving out towards the wingtip. The leading-edge vortex grew in size with increasing forward flight velocity. Such a phenomenon is proposed as a likely mechanism for lift enhancement in many insect groups. During supination, vorticity is shed from the leading edge as postulated in the 'flex' mechanism. This vorticity would enhance upstroke lift if it was recaptured diring subsequent translation, but it is not. Instead, the vorticity is left behind and the upstroke circulation builds up slowly. A small jet provides additional thrust as the trailing edges approach at the end of the upstroke. The stereophotographs also suggest that the bound circulation may not be reversed between half strokes at the fastest flight speeds.
机译:通过使用束缚飞蛾的烟雾可视化研究,已经研究了鹰蛾(Manduca sexta)飞行过程中采用的空气动力学机制。机翼周围的气流和整个尾流结构的细节都记录为立体照片和高速视频序列。分析了伴随飞行速度从0.4 m s s -1 增加的流量变化。尾流由交替的一系列水平和垂直涡流环组成,分别由连续的向下和向上冲程产生。由于前沿涡流通过向翼尖向外移动的辐射流而稳定,因此向下冲程产生的升力比向上冲程产生的升力要大得多。前沿涡流的大小随着向前飞行速度的增加而增大。提出这种现象是许多昆虫群体中增强提举的可能机制。在旋后期间,如“挠性”机制所假定的那样,涡流从前缘掉落。如果旋涡被重新捕获而导致随后的平移,则涡旋将增强上扬,但事实并非如此。取而代之的是,涡度被遗留下来,而上冲程循环逐渐建立。当后缘在上冲程结束时接近时,一股小射流会提供额外的推力。立体照片还表明,在最快的飞行速度下,半冲程之间的束缚循环可能不会逆转。

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