Simulation of sound generated by large-scale vortices in a shear layer by hybrid DVM/APE approach
Simulation of sound generated by large-scale vortices in a shear layer by hybrid DVM/APE approach
In this paper, sound generated by large-scale votices in a two-dimensional low-Mach number turbulent shear layer is investigated. A hybrid DVM/APE (Discrete-Vortex Model and Acoustic Perturbation Equations) approach is proposed to study this vortex sound phenomenon. A discrete-vortex model is used to simulate unsteady fluid motions of the trailing edge shear layer. A conformal mapping is applied to solve the 2D inviscid flow near the half plane, which is originally used for the problem of a slit geometry. At the trailing edge of the plane, the effect of fluid's viscosity is imposed by a vortex shedding model and Kutta condition. The unsteady flow field is obtained after DVM simulation. The background mean flow field is acquired by a time-average algorithm. Then, acoustic perturbation equations are solved to obtain the acoustic field by CAA approaches with both acoustic sources and the background mean flow field determined from the results of DVM. Results demonstrate that this hybrid DVM/APE method is a feasible approach to simulate sound generated by the motions of vortices.
American Institute of Aeronautics and Astronautics
Jing, Xiaodong
9bd7313a-4ab2-4387-839e-4c1583f61531
Wu, Long
9787473b-a81a-47ce-a696-22afa8c2204b
Dai, Xiwen
a961b65c-1ab2-429c-8720-bf128289e9a5
Song, Minna
6e5f016b-8bb7-4b5c-b451-a8897d537092
Sun, Xiaofeng
87a75751-8d01-440e-a234-02d4a6436ef6
Jing, Xiaodong
9bd7313a-4ab2-4387-839e-4c1583f61531
Wu, Long
9787473b-a81a-47ce-a696-22afa8c2204b
Dai, Xiwen
a961b65c-1ab2-429c-8720-bf128289e9a5
Song, Minna
6e5f016b-8bb7-4b5c-b451-a8897d537092
Sun, Xiaofeng
87a75751-8d01-440e-a234-02d4a6436ef6
Jing, Xiaodong, Wu, Long, Dai, Xiwen, Song, Minna and Sun, Xiaofeng
(2014)
Simulation of sound generated by large-scale vortices in a shear layer by hybrid DVM/APE approach.
In 20th AIAA/CEAS Aeroacoustics Conference.
American Institute of Aeronautics and Astronautics..
(doi:10.2514/6.2014-3293).
Record type:
Conference or Workshop Item
(Paper)
Abstract
In this paper, sound generated by large-scale votices in a two-dimensional low-Mach number turbulent shear layer is investigated. A hybrid DVM/APE (Discrete-Vortex Model and Acoustic Perturbation Equations) approach is proposed to study this vortex sound phenomenon. A discrete-vortex model is used to simulate unsteady fluid motions of the trailing edge shear layer. A conformal mapping is applied to solve the 2D inviscid flow near the half plane, which is originally used for the problem of a slit geometry. At the trailing edge of the plane, the effect of fluid's viscosity is imposed by a vortex shedding model and Kutta condition. The unsteady flow field is obtained after DVM simulation. The background mean flow field is acquired by a time-average algorithm. Then, acoustic perturbation equations are solved to obtain the acoustic field by CAA approaches with both acoustic sources and the background mean flow field determined from the results of DVM. Results demonstrate that this hybrid DVM/APE method is a feasible approach to simulate sound generated by the motions of vortices.
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e-pub ahead of print date: 13 June 2014
Venue - Dates:
20th AIAA/CEAS Aeroacoustics Conference 2014, , Atlanta, GA, United States, 2014-06-16 - 2014-06-20
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Local EPrints ID: 485879
URI: http://eprints.soton.ac.uk/id/eprint/485879
PURE UUID: 42c67b22-199a-4ec9-b8fc-a0ef97ad5e8f
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Date deposited: 03 Jan 2024 19:33
Last modified: 18 Mar 2024 03:51
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Author:
Xiaodong Jing
Author:
Long Wu
Author:
Xiwen Dai
Author:
Minna Song
Author:
Xiaofeng Sun
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