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首页> 外文期刊>The Journal of Experimental Biology >Hovering flight in hummingbird hawkmoths: kinematics, wake dynamics and aerodynamic power
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Hovering flight in hummingbird hawkmoths: kinematics, wake dynamics and aerodynamic power

机译:在蜂鸟霍克马舍斯皮徘徊:运动学,唤醒动力学和空气动力

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Hovering insects are divided into two categories: 'normal' hoverers that move the wing symmetrically in a horizontal stroke plane, and those with an inclined stroke plane. Normal hoverers have been suggested to support their weight during both downstroke and upstroke, shedding vortex rings each half-stroke. Insects with an inclined stroke plane should, according to theory, produce flight forces only during downstroke, and only generate one set of vortices. The type of hovering is thus linked to the power required to hover. Previous efforts to characterize the wake of hovering insects have used low-resolution experimental techniques or simulated the flow using computational fluid dynamics, and so it remains to be determined whether insect wakes can be represented by any of the suggested models. Here, we used tomographic particle image velocimetry, with a horizontal measurement volume placed below the animals, to show that the wake shed by hovering hawkmoths is best described as a series of bilateral, stacked vortex 'rings'. While the upstroke is aerodynamically active, despite an inclined stroke plane, it produces weaker vortices than the downstroke. In addition, compared with the near wake, the far wake lacks structure and is less concentrated. Both near and far wakes are clearly affected by vortex interactions, suggesting caution is required when interpreting wake topologies. We also estimated induced power (P-ind) from downwash velocities in the wake. Standard models predicted a P-ind more than double that from our wake measurements. Our results thus question some model assumptions and we propose a reevaluation of the model parameters.
机译:悬停昆虫分为两类:“正常”的悬停昆虫在水平冲程平面上对称地移动翅膀,而那些在倾斜冲程平面上移动翅膀。正常的悬停者被建议在下冲程和上冲程期间支撑自己的重量,每半冲程都会脱落漩涡环。根据理论,具有倾斜冲程平面的昆虫应该只在向下冲程时产生飞行力,并且只产生一组漩涡。因此,悬停的类型与悬停所需的功率有关。以前描述悬停昆虫尾迹的工作都使用了低分辨率的实验技术,或者使用计算流体力学模拟了流动,因此,昆虫尾迹是否可以用任何建议的模型来表示还有待确定。在这里,我们使用层析粒子图像测速技术,在动物下方放置一个水平测量体积,以表明盘旋飞蛾脱落的尾迹最好描述为一系列双边堆叠的涡旋“环”。虽然上升冲程在空气动力学上是活跃的,但尽管有倾斜的冲程平面,它产生的涡流比下降冲程弱。此外,与近尾迹相比,远尾迹缺乏结构,集中度较低。近尾迹和远尾迹都明显受到涡旋相互作用的影响,这表明在解释尾迹拓扑时需要谨慎。我们还根据尾流中的下洗速度估算了诱导功率(P-ind)。标准模型预测的P-ind是我们尾流测量结果的两倍多。因此,我们的结果质疑了一些模型假设,并建议重新评估模型参数。

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