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Extraction and Reconstruction of Individual Vortex-Shedding Mode from Bistable Flow

机译:双稳流中单个涡旋脱落模式的提取与重构

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摘要

For the flow around a circular cylinder under the synthetic-jet control, a bistable flow has been identified, in which the wake vortex sheds with the symmetric or antisymmetric mode. However, it is difficult to gain insight into the bistable flow due to the complexity with multiple dominant frequencies. Thus, it is aimed to reveal the underlying flow physics of the bistable flow by adopting advanced data-processing techniques. To obtain more accurate dynamic information, total dynamic mode decomposition was employed to extract dynamic modes, spectrum, and mode coefficients to describe the flow dynamics. It was found that the bistable flow contains dual dominant frequencies corresponding to the antisymmetric and symmetric vortex-shedding modes. The mode phi(1,c) for the control case approximates to the mode phi(1,n) for the natural case, representing the antisymmetric-shedding mode. However, the spatial distributions of the mode phi(2,c) are essentially different from those of the mode phi(1,c), representing the symmetric-shedding mode. The influence of the dominant modes phi(1,c) and phi(2,c) of the control case on the relevant physical components and flow structures was investigated in detail. The mode-competition process was illustrated to help understand the formation mechanism of the bistable flow. In particular, the total-dynamic-mode-decomposition reconstruction approach was adopted to recover the flow structures through superposing the zeroth mode and the different dominant modes. As a result, the individual vortex-shedding mode could be effectively isolated from the bistable flow by the total dynamic mode decomposition.
机译:对于在合成射流控制下绕圆柱体的流动,已经确定了双稳态流动,其中尾流涡流以对称或反对称模式脱落。但是,由于具有多个主频率的复杂性,难以深入了解双稳态流。因此,其目的是通过采用先进的数据处理技术来揭示双稳态流的基本流物理学。为了获得更准确的动态信息,采用总动态模式分解来提取动态模式,频谱和模式系数来描述流动动力学。发现双稳态流包含对应于反对称和对称涡流消除模式的双重主导频率。控制案例的模式phi(1,c)近似于自然案例的模式phi(1,n),表示反对称脱落模式。但是,模式phi(2,c)的空间分布与模式phi(1,c)的空间分布本质上不同,代表了对称脱落模式。详细研究了控制案例的主导模式phi(1,c)和phi(2,c)对相关物理组件和流结构的影响。说明了模式竞争过程以帮助理解双稳态流的形成机理。特别地,采用全动态模式分解重建方法,通过叠加零模式和不同的主导模式来恢复流动结构。结果,通过整体动力学模式分解,可以有效地将单个涡流消除模式与双稳态流隔离。

著录项

  • 来源
    《AIAA Journal》 |2017年第7期|2129-2141|共13页
  • 作者

    Wang Lei; Feng Li-Hao;

  • 作者单位

    Beijing Univ Aeronaut & Astronaut, Fluid Mech Key Lab, Educ Minist, Beijing 100191, Peoples R China;

    Beijing Univ Aeronaut & Astronaut, Fluid Mech Key Lab, Educ Minist, Beijing 100191, Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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