Trigger mechanism for a singing cavitating tip vortex

IF 3.6 2区 工程技术 Q1 MECHANICS
Zhaohui Qian , Yongshun Zeng , Xiaoxing Peng , Xianwu Luo
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Abstract

The discrete tone radiated from tip vortex cavitation (TVC), known as ‘vortex singing’, was recognized in 1989, but its triggering remains unclear for over thirty years. In this study, the desinent cavitation number and viscous correction are applied to describe the dynamics of cavitation bubbles and the dispersion relation of cavity interfacial waves. The wavenumber-frequency spectrum of the cavity radius from the experiment in CSSRC indicates that singing waves predominantly consist of the stationary double helical modes (kθ = 2- and -2+) and the breathing mode (kθ = 0-), rather than standing waves as assumed in previous literatures. Moreover, two trigger mechanisms, expressed by two triggering lines, are proposed: the twisted TVC, initially at rest, is driven into motion through the corrected natural frequency (fn) due to the step change of the far-field pressure. Subsequently, the frequency associated with the zero-group-velocity point (zgv) at kθ = 0- is excited through i, the frequency at the intersection of dispersion curves at kθ = 0- and -2+, or j, the frequency at the intersection of dispersion curves at kθ = 0- and 2-, corresponding to two types of the vortex singing triggering. These solutions, without empirical parameters, are validated using singing conditions provided by CSSRC and G.T.H., respectively. Furthermore, the coherence and the cross-power spectral density spectrum indicates a large-scale breathing wave propagating along the singing cavity surface and travelling from downstream to hydrofoil tip, providing us a comprehensive understanding for the triggering of vortex singing.

Abstract Image

用于歌唱空化尖端涡流的触发机制
1989 年,人们认识到了由尖端涡旋空化(TVC)辐射出的离散音调,这种音调被称为 "涡旋歌唱",但三十多年来,其触发原因仍不清楚。在这项研究中,应用了 Desinent 空化数和粘性修正来描述空化气泡的动力学和空腔界面波的弥散关系。来自 CSSRC 实验的空腔半径的波数-频率谱表明,歌唱波主要由静止的双螺旋模式(kθ = 2- 和 -2+)和呼吸模式(kθ = 0-)组成,而不是之前文献中假设的驻波。此外,还提出了由两条触发线表示的两种触发机制:扭曲的 TVC 最初处于静止状态,由于远场压力的阶跃变化,通过校正固有频率(fn)被驱动运动。随后,与 kθ = 0- 处的零组速度点 (ῶzgv)相关的频率通过 kθ = 0- 和 -2+ 处频散曲线交点的频率ῶi 或 kθ = 0- 和 2- 处频散曲线交点的频率ῶj 被激发,对应于两种类型的涡唱触发。这些不含经验参数的解分别利用 CSSRC 和 G.T.H. 提供的歌唱条件进行了验证。此外,相干性和交叉功率谱密度频谱表明有一个大尺度呼吸波沿歌唱腔表面传播,并从下游向水翼顶端传播,这为我们全面理解涡旋歌唱的触发提供了依据。
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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来源期刊
CiteScore
7.30
自引率
10.50%
发文量
244
审稿时长
4 months
期刊介绍: The International Journal of Multiphase Flow publishes analytical, numerical and experimental articles of lasting interest. The scope of the journal includes all aspects of mass, momentum and energy exchange phenomena among different phases such as occur in disperse flows, gas–liquid and liquid–liquid flows, flows in porous media, boiling, granular flows and others. The journal publishes full papers, brief communications and conference announcements.
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