Abstract
The effects of a fixed splitter plate mounted on the downstream side of a circular cylinder to reduce aeolian tone is investigated experimentally. The diameter of the cylinder D is 22mm. Three parameters are considered: The length of the plates (L=0.5D, 1.0D, 1.5D), the thickness of the plates (h=1mm and 2mm), and the Reynolds numbers (Re = 2.18×〖10〗^4 ~ 4.94×〖10〗^4 ) based on cylinder diameter. The splitter plates achieve the reduction in aeolian tone at the fundamental vortex shedding frequency and the overall sound pressure level (OASPL) for all cases. The peak values of SPL at the fundamental vortex shedding frequency decrease by about 7.3~15.8 dB with splitter plates behind the cylinder, and the OASPL reduction ranges from 5.7dB to 10.5dB. Meanwhile, the fundamental vortex shedding frequency experiences a slight frequency shift, which means the splitter plate has influence on the vortex shedding process. The harmonic tones, including the first and second harmonics, largely disappear when the splitter plates is attached, except for the plate with L=1.5D and h=1mm. Flow fields derived from particle-image velocimetry experiments and the power spectral density of the streamwise velocity are presented, which helps to identify the modification of the near-field flow dynamics by the splitter plate, and connect that to the observed far-field noise reduction.
Original language | English |
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Title of host publication | 28th AIAA/CEAS Aeroacoustics Conference, 2022 |
Publisher | American Institute of Aeronautics and Astronautics Inc. (AIAA) |
Chapter | Acoustic/Fluid Dynamics Interactions IX: Misc |
Pages | 1-12 |
Number of pages | 12 |
ISBN (Print) | 9781624106644 |
DOIs | |
Publication status | Published - 14 Jun 2022 |
Publication series
Name | AIAA/CEAS Aeroacoustics Conference |
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Publisher | American Institute of Aeronautics and Astronautics |
ISSN (Print) | 1946-7826 |
Bibliographical note
Funding Information:The authors acknowledge the Fluid and Aerodynamics Research Group of University of Bristol. The first author’s PhD grant 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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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)
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