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 language | English |
|---|---|
| Title of host publication | 28th AIAA/CEAS Aeroacoustics Conference, 2022 |
| Publisher | American Institute of Aeronautics and Astronautics Inc. (AIAA) |
| Chapter | Acoustic/Fluid Dynamics Interactions VI: Misc |
| Pages | 1-15 |
| Number of pages | 15 |
| ISBN (Electronic) | 9781624106644 |
| DOIs | |
| Publication status | Published - 13 Jun 2022 |
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.
Fingerprint
Dive into the research topics of 'An experimental study of aeroacoustic and aerodynamic performance of the wavy and vibrissa shaped cylinders'. Together they form a unique fingerprint.Student theses
-
Aerodynamic noise and its passive control of subcritical flow past a cylinder
Chen, G. (Author), Zang, B. (Supervisor) & Azarpeyvand, M. (Supervisor), 1 Oct 2024Student thesis: Doctoral Thesis › Doctor of Philosophy (PhD)
File
Cite this
- APA
- Author
- BIBTEX
- Harvard
- Standard
- RIS
- Vancouver