...
首页> 外文期刊>Journal of visualization >Wake modes behind a streamwisely oscillating cylinder at constant and ramping frequencies
【24h】

Wake modes behind a streamwisely oscillating cylinder at constant and ramping frequencies

机译:在恒定和倾斜频率下,在流式振荡圆柱体后面的唤醒模式

获取原文
获取原文并翻译 | 示例

摘要

In this paper, the wake modes behind a circular cylinder under streamwisely forcing oscillating motion are studied at Reynolds number Re = 360-460 which are observed by laser-induced fluorescence flow visualization technique. The forcing frequency fe ranges from 0 to 6.85 fs , where fs is the vortex shedding frequency behind a stationary cylinder, and the forcing amplitude A/d=0.2,0.5,1.0, where d is the cylinder diameter. Both time-invariant and linearly ramping fe are investigated. Following our previous modal notation, the following conclusions can be drawn: firstly, three rarely reported modes in numerical studies, C-I, C-II and S-III, are now confirmed in experiments (though with differentiable appearance in their far wake behaviour) at higher A and/or fe ranges and the envelope lines of S modes and C modes, yielded from a vortex circulation model, are shown to be dependent on the peak relative velocity of the free stream to the cylinder surface. So is the occurrence of the S-II mode. Secondly, near the demarcation of A modes and S-I mode, wake mode undergoes constant transition in a stochastic manner at fixed Re, A and fe. Thirdly, a typical hysteretic effect can be observed when the oscillation frequency of the cylinder ramps up and down in a linear way, and the extent of delay is dependent on the ramping rate k. Finally, mode switching during frequency ramping obeys a unidirectional order. During k0 (ramp-down), when S-I (Type-II) mode switches to A-IV mode, or A-IV to A-III, the flow structure downstream is affected by the upstream and the entire wake flow eventually switched, which is classified as slow switches. In contrast, during k0 (ramp-up), a clear and abrupt switch can be observed in the wake when A-IV or A-III switch to S-I (Type-II) modes, which are jump switches.
机译:在本文中,研究了在雷诺数Re = 360-460的作用下,圆柱体在流向强迫振荡运动下的唤醒模式,该模式通过激光诱导荧光流动可视化技术进行观察。强迫频率fe的范围是0到6.85 fs,其中fs是静止圆柱体后面的涡流脱落频率,强迫振幅A / d = 0.2,0.5,1.0,其中d是圆柱体直径。同时研究了时不变和线性斜率fe。遵循我们以前的模态符号,可以得出以下结论:首先,现在在实验中证实了三种罕见的数值研究模式CI,C-II和S-III(尽管在远距离行为上具有可区别的外观)。由涡流循环模型得出的更高的A和/或fe范围以及S模式和C模式的包络线显示取决于自由流与圆柱体表面的峰值相对速度。 S-II模式的发生也是如此。其次,在A模式和S-I模式的界限附近,唤醒模式在固定的Re,A和fe处以随机的方式经历恒定的转变。第三,当气缸的振荡频率以线性方式向上和向下倾斜时,可以观察到典型的磁滞效应,并且延迟的程度取决于倾斜率k。最后,在频率斜坡上升期间的模式切换服从单向指令。在k <0(下降)期间,​​当SI(类型II)模式切换为A-IV模式,或从A-IV切换为A-III时,下游的流结构会受到上游的影响,最终整个尾流会切换,被归类为慢速开关。相反,在k> 0(加速)期间,当A-IV或A-III切换到S-I(类型II)模式(跳变开关)时,可以在唤醒时观察到清晰而突然的开关。

著录项

  • 来源
    《Journal of visualization 》 |2019年第3期| 505-527| 共23页
  • 作者单位

    Tsinghua Univ, Sch Aerosp Engn, AML, Zhongguancun North St, Beijing 100084, Peoples R China|China Aerodynam Res & Dev Ctr, Mianyang, Peoples R China;

    Tsinghua Univ, Sch Aerosp Engn, AML, Zhongguancun North St, Beijing 100084, Peoples R China;

    Univ Durham, Dept Engn, Durham DH1 3LE, England;

    Tsinghua Univ, Sch Aerosp Engn, AML, Zhongguancun North St, Beijing 100084, Peoples R China;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Streamwise oscillation; Vortex shedding; Wake;

    机译:流向振荡;涡旋脱落;唤醒;

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号