A wall-resolved large-eddy simulation of deep cavity flow in acoustic resonance
A wall-resolved large-eddy simulation of deep cavity flow in acoustic resonance
The aeroacoustic source mechanism of a deep rectangular cavity, which has an aspect ratio of and is subjected to a turbulent boundary layer of at a Mach number of 0.2, is investigated by using a high-order accurate large-eddy simulation. The primary aim of this study is to provide an improved understanding of the fluid-acoustic coupling mechanism that triggers a self-sustained acoustic resonance in a deep cavity. Various analysis methods, which include Doak's momentum potential theory that allows for the separation of hydrodynamic and acoustic components, are used to provide highly detailed investigations and findings. The vortex dynamics near the cavity opening region is investigated as the potential primary source of noise generation. In addition, the noise generation mechanism is quantitatively explained by the onset of the separation region near the downstream corner that ensues from the synchronised shear layer-wall interaction. The current work extensively focuses on the fluid-acoustic coupling mechanism, and it is found that the acoustic resonance favourably modulates the hydrodynamic fluctuation near the upstream corner of the cavity. Furthermore, the current study also suggests that nonlinear interactions between fundamental acoustic resonance and higher harmonics are plausible. Based on the discussions provided in this paper, a semi-empirical model to predict the critical free stream velocity at which a strong fluid-acoustic coupling occurs as a function of cavity geometry and inflow boundary-layer property is proposed.
Key words aeroacoustics, flow-structure interactions, turbulence simulation
Ho, You Wei
bf2b7395-c153-453b-85a9-6435741d6b57
Kim, Jae
fedabfc6-312c-40fd-b0c1-7b4a3ca80987
23 April 2021
Ho, You Wei
bf2b7395-c153-453b-85a9-6435741d6b57
Kim, Jae
fedabfc6-312c-40fd-b0c1-7b4a3ca80987
Ho, You Wei and Kim, Jae
(2021)
A wall-resolved large-eddy simulation of deep cavity flow in acoustic resonance.
Journal of Fluid Mechanics, 917, [2100261].
(doi:10.1017/jfm.2021.261).
Abstract
The aeroacoustic source mechanism of a deep rectangular cavity, which has an aspect ratio of and is subjected to a turbulent boundary layer of at a Mach number of 0.2, is investigated by using a high-order accurate large-eddy simulation. The primary aim of this study is to provide an improved understanding of the fluid-acoustic coupling mechanism that triggers a self-sustained acoustic resonance in a deep cavity. Various analysis methods, which include Doak's momentum potential theory that allows for the separation of hydrodynamic and acoustic components, are used to provide highly detailed investigations and findings. The vortex dynamics near the cavity opening region is investigated as the potential primary source of noise generation. In addition, the noise generation mechanism is quantitatively explained by the onset of the separation region near the downstream corner that ensues from the synchronised shear layer-wall interaction. The current work extensively focuses on the fluid-acoustic coupling mechanism, and it is found that the acoustic resonance favourably modulates the hydrodynamic fluctuation near the upstream corner of the cavity. Furthermore, the current study also suggests that nonlinear interactions between fundamental acoustic resonance and higher harmonics are plausible. Based on the discussions provided in this paper, a semi-empirical model to predict the critical free stream velocity at which a strong fluid-acoustic coupling occurs as a function of cavity geometry and inflow boundary-layer property is proposed.
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Accepted/In Press date: 10 March 2021
Published date: 23 April 2021
Keywords:
Key words aeroacoustics, flow-structure interactions, turbulence simulation
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Local EPrints ID: 447786
URI: http://eprints.soton.ac.uk/id/eprint/447786
ISSN: 0022-1120
PURE UUID: 93770776-b603-4e26-95aa-95f3c2cf80b7
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Date deposited: 22 Mar 2021 17:34
Last modified: 17 Mar 2024 06:25
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Author:
You Wei Ho
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