Phase-Locked PIV Measurements of Vortex Shedding Characteristics Downstream of Straight Circular Finned Cylinders During Acoustic Resonance

Rashidul Islam, Mahmoud Shaaban, A. Mohany
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引用次数: 2

Abstract

Excitation of acoustic resonance by flow perturbation downstream of cylinders can result in hazardous levels of acoustic pressure. Previous studies have shown that straight finned cylinders are susceptible to flow-excited acoustic resonance. In this work, the excitation of acoustic resonance by flow around finned cylinders of different fin parameters including the spacing between the fins, the thickness of the fin, and the height of the fin is investigated. All the investigated finned cylinders have the same equivalent diameter. Phase-locked particle image velocimetry (PIV) measurements are carried out during acoustic resonance to characterize the flow field downstream of the cylinders and identify the influence of the fins on the flow structures at the peak of resonance excitation. Results show that straight circular fins excite acoustic resonance at lower velocities and result in higher sound pressure level compared with a single bare cylinder of the same effective diameter. This behaviour is due to the effect of fin parameters on the strength and the formation length of vortices shed during the acoustic cycle. A brief summary of the results is presented in this paper.
声共振过程中直线型翅片圆柱体下游涡脱落特性的锁相PIV测量
由气瓶下游的流动扰动引起的声共振会导致声压达到危险水平。以往的研究表明,直翅片圆柱体易受流激声共振的影响。本文研究了不同翅片间距、厚度、高度等翅片参数对流动绕翅圆柱声共振的激励作用。所研究的所有翅片圆柱体具有相同的等效直径。在声共振过程中进行锁相粒子图像测速(PIV)测量,以表征圆柱体下游的流场,并确定翅片对共振激发峰值时流动结构的影响。结果表明,与相同有效直径的单个裸圆柱体相比,直圆翅片在较低的速度下激发声共振,产生更高的声压级。这种行为是由于翅片参数对声循环过程中涡流强度和形成长度的影响。本文对研究结果作了简要总结。
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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