Delaying the Chaotic Onset in the Flow-Field of Flapping Foil With Flexible Aft Tail

C. Shah, Dipanjan Majumdar, Sunetra Sarkar
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Abstract

The present study is focused on examining the flow-field dynamics of a flapping foil with a flexible aft tail as compared to a rigid configuration where tail flexibility is infinite. The flow around the oscillating body is governed by the incompressible Navier-Stokes equations. An in-house Fluid-Structure Interaction solver has been developed following a discrete forcing type Immersed Boundary Method coupled with an inextensible filament structural model. The flapping amplitude is considered as a bifurcation parameter, and as the bifurcation parameter is increased, the periodic wake transitions into the chaotic patterns. The periodic to chaotic transition happens through an intermittency route. However, the elliptic foil with flexible aft tail exhibits chaotic onsets much later compared to the foil with a rigid tail. Time series analysis techniques, such as frequency spectra and recurrence plots, have been used to establish the intermittency and the chaotic dynamics conclusively.
延迟柔性尾翼扑翼流场混沌起始的研究
本文主要研究了具有柔性尾翼的扑翼与具有无限柔性尾翼的刚性尾翼的流场动力学特性。围绕振荡体的流动由不可压缩的纳维-斯托克斯方程控制。采用离散强迫浸入边界法结合不可扩展细丝结构模型,开发了一种内部流固耦合求解器。将扑动幅值作为分岔参数,随着分岔参数的增大,周期尾迹转变为混沌模式。周期性到混沌的转变是通过间歇路径发生的。然而,具有柔性尾尾的椭圆型翼比具有刚性尾的椭圆型翼表现出更晚的混沌起动。时间序列分析技术,如频谱和递归图,已被用来确定间歇性和混沌动力学。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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