An experimental study of aeroacoustic and aerodynamic performance of the wavy and vibrissa shaped cylinders

Research output: Chapter in Book/Report/Conference proceedingConference Contribution (Conference Proceeding)

2 Citations (Scopus)

Abstract

This paper presents an experimental study on the effectiveness of sinusoidal wavy-shaped and vibrissa-shaped cylinders as a passive control method on mitigating the aerodynamic noise of flow past a cylinder. A total of five differently-shaped cylinders with similar total volume, namely a circular cylinder with 22mm diameter, two sinusoidal wavy cylinders with different wavelengths (λ = 27.5mm and 55mm), one elliptical cylinder and one vibrissa-shaped cylinder, have been investigated in this study. Far-field noise measurements for all the cylinders have been performed at free-stream velocities from 8m/s to 35m/s. The results show that compared with the circular cylinder, wavy cylinders effectively achieve a overall noise reduction over a wide range of Strouhal number (0.1 < St < 2), especially prominent at the tonal peak of the vortex shedding frequency (i.e., St = 0.2). The result also shows that the smaller wavelength performs better than that of the larger. The elliptical cylinder results in slight noise reduction and a shift in the tonal peak frequencies. The vibrissa-shaped cylinder is the most effective among all, producing significant noise reduction over a wide St range albeit a small noise increase is observed at low Strouhal number of St < 0.12. To further understand the underlying noise reduction mechanism, time-resolved PIV measurements has also been carried out. Both the instantaneous and time-averaged velocity profile are compared with the baseline circular cylinder. The noise reduction in the wavy- and vibrissa-shaped cylinders is likely to be due to the modification and breakdown of the large-scale vortex shedding structures in the cylinder wake.
Original languageEnglish
Title of host publication28th AIAA/CEAS Aeroacoustics Conference, 2022
PublisherAmerican Institute of Aeronautics and Astronautics Inc. (AIAA)
ChapterAcoustic/Fluid Dynamics Interactions VI: Misc
Pages1-15
Number of pages15
ISBN (Electronic)9781624106644
DOIs
Publication statusPublished - 14 Jun 2022

Publication series

NameAIAA/CEAS Aeroacoustics Conference
PublisherAIAA
ISSN (Print)1946-7826

Bibliographical note

Funding Information:
The second author is funded by the China Scholarship Council (CSC)-University of Bristol (UoB) PhD Scholarship.

Publisher Copyright:
© 2022, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.

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