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Onset of orbital motion in a trailing vortex from an oscillating wing

机译:从振荡翼尾涡体中的轨道运动开始

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摘要

The onset and development of orbital motion of a trailing vortex from a wing undergoing small amplitude heaving motion is investigated using stereo particle image velocimetry in conjunction with three-dimensional reconstruction techniques. The effect of Strouhal number is examined via space-time representations of axial and azimuthal vorticity, axial velocity deficit and swirl ratio. At low Strouhal number, the undulation of the vortex remains unidirectional with no amplification in the streamwise direction. In contrast, at high Strouhal number, the amplitude of vortex undulation can increase by up to a factor of ten in the streamwise direction. These large amplitudes occur during orbital motion of the vortex. Irrespective of the value of either the Strouhal number of excitation or the streamwise location along the undulating vortex, generic physical mechanisms occur. Changes in curvature along the vortex are closely related to changes in the axial velocity deficit, extreme values of axial vorticity and swirl ratio and the onset and attenuation of pronounced azimuthal vorticity.
机译:使用立体声粒子图像速度与三维重建技术一起研究了从经历小幅度的振幅气相的翼涡流的轨道运动的起初和发展。通过轴向和方位涡度,轴向速度缺陷和旋涡比的时空表示检查Strouhal数的效果。在低斯特鲁姆数,涡流的下降仍然是单向的,在流动方向上没有放大。相比之下,在高斯特鲁尔数,涡流波动的幅度可以在流动方向上增加到10个倍数。在涡旋的轨道运动期间发生这些大幅度。不管沿波动涡流的斗争次数或流动位置的恒流位的值,发生了通用物理机制。沿涡旋的曲率变化与轴向速度缺陷,极端值的轴向涡度和旋涡比的变化密切相关,以及发作的方位形涡度的发作和衰减。

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