Lagrangian analysis of bio-inspired vortex ring formation

IF 2.8 Q2 MECHANICS Flow (Cambridge, England) Pub Date : 2021-07-30 DOI:10.1017/flo.2022.9
M. Baskaran, K. Mulleners
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Abstract

Abstract Pulsatile jet propulsion is a highly energy-efficient swimming mode used by various species of aquatic animals that continues to inspire engineers of underwater vehicles. Here, we present a bio-inspired jet propulsor that combines the flexible hull of a jellyfish with the compression motion of a scallop to create individual vortex rings for thrust generation. Similar to the biological jetters, our propulsor generates a nonlinear time-varying exit velocity profile and has a finite volume capacity. The formation process of the vortices generated by this jet profile is analysed using time-resolved velocity field measurements. The transient development of the vortex properties is characterised based on the evolution of ridges in the finite-time Lyapunov exponent field and on local extrema in the pressure field derived from the velocity data. Special attention is directed toward the vortex merging observed in the trailing shear layer. During vortex merging, the Lagrangian vortex boundaries first contract in the streamwise direction before expanding in the normal direction to keep the non-dimensional energy at its minimum value, in agreement with the Kelvin–Benjamin variational principle. The circulation, diameter and translational velocity of the vortex increase due to merging. The vortex merging takes place because the velocity of the trailing vortex is higher than the velocity of the main vortex ring prior to merging. The comparison of the temporal evolution of the Lagrangian vortex boundaries and the pressure-based vortex delimiters confirms that features in the pressure field serve as accurate and robust observables for the vortex formation process.
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仿生涡环形成的拉格朗日分析
摘要脉冲射流推进是一种高效能的游泳模式,被各种水生动物使用,它继续激励着水下航行器的工程师。在这里,我们展示了一种仿生喷气推进器,它将水母的柔性外壳与扇贝的压缩运动结合在一起,创造出用于产生推力的单独涡流环。与生物喷射器类似,我们的推进器产生非线性时变出口速度剖面,并具有有限的体积容量。利用时间分辨速度场测量分析了这种射流轮廓产生的涡流的形成过程。涡流特性的瞬态发展基于有限时间李雅普诺夫指数场中脊的演变和从速度数据导出的压力场中的局部极值来表征。特别注意在尾剪切层中观察到的涡流合并。在涡流合并过程中,拉格朗日涡流边界首先在顺流方向收缩,然后在法线方向膨胀,以将无量纲能量保持在其最小值,这符合开尔文-本杰明变分原理。涡流的环流、直径和平移速度由于合并而增加。涡流合并的发生是因为尾涡的速度高于合并前主涡环的速度。拉格朗日涡旋边界和基于压力的涡旋划界器的时间演变的比较证实,压力场中的特征是涡旋形成过程的精确和稳健的可观测值。
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