Analytical and numerical prediction of acoustic radiation from a panel under turbulent boundary layer excitation
The vibroacoustic response of a simply supported panel excited by turbulent flow is analytically and numerically investigated. In the analytical model, the radiated sound power is described in terms of the cross spectrum density of the wall pressure field and sensitivity functions for the acoustic p...
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Published in | Journal of sound and vibration Vol. 479; p. 115372 |
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Main Authors | , , , , , , , |
Format | Journal Article |
Language | English |
Published |
Amsterdam
Elsevier Ltd
04.08.2020
Elsevier Science Ltd Elsevier |
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Online Access | Get full text |
ISSN | 0022-460X 1095-8568 |
DOI | 10.1016/j.jsv.2020.115372 |
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Abstract | The vibroacoustic response of a simply supported panel excited by turbulent flow is analytically and numerically investigated. In the analytical model, the radiated sound power is described in terms of the cross spectrum density of the wall pressure field and sensitivity functions for the acoustic pressure and fluid particle velocity. For the numerical model, a hybrid approach based on the finite element method is described in which the cross spectrum of the wall pressure field is represented by a set of uncorrelated wall plane waves. Realisations of the wall pressure field are used as deterministic input loads to the panel. The structural and acoustic responses of the panel subject to turbulent boundary layer excitation are then obtained from an ensemble average of the different realisations. Analytical and numerical results are compared with experimental data measured in an anechoic wind tunnel, showing good agreement. The effect of adding stiffeners on the vibroacoustic response of the panel is also examined using the proposed numerical approach. |
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AbstractList | The vibroacoustic response of a simply supported panel excited by turbulent flow is analytically and numerically investigated. In the analytical model, the radiated sound power is described in terms of the cross spectrum density of the wall pressure field and sensitivity functions for the acoustic pressure and fluid particle velocity. For the numerical model, a hybrid approach based on the finite element method is described in which the cross spectrum of the wall pressure field is represented by a set of uncorrelated wall plane waves. Realisations of the wall pressure field are used as deterministic input loads to the panel. The structural and acoustic responses of the panel subject to turbulent boundary layer excitation are then obtained from an ensemble average of the different realisations. Analytical and numerical results are compared with experimental data measured in an anechoic wind tunnel, showing good agreement. The effect of adding stiffeners on the vibroacoustic response of the panel is also examined using the proposed numerical approach. |
ArticleNumber | 115372 |
Author | Skvortsov, A. Maxit, L. Croaker, P. Atalla, N. Kessissoglou, N. Karimi, M. Robin, O. Marburg, S. |
Author_xml | – sequence: 1 givenname: M. surname: Karimi fullname: Karimi, M. email: Mahmoud.karimi@uts.edu.au organization: Centre for Audio, Acoustics and Vibration, University of Technology Sydney, Sydney, Australia – sequence: 2 givenname: L. surname: Maxit fullname: Maxit, L. organization: Univ Lyon, INSA–Lyon, Laboratoire Vibrations-Acoustique (LVA), 25 bis, av. Jean Capelle, F-69621, Villeurbanne Cedex, France – sequence: 3 givenname: P. surname: Croaker fullname: Croaker, P. organization: Maritime Division, Defence Science and Technology, Melbourne, Australia – sequence: 4 givenname: O. surname: Robin fullname: Robin, O. organization: Groupe d'Acoustique de l'Université de Sherbrooke, Université de Sherbrooke, Sherbrooke, J1K 2R1, Canada – sequence: 5 givenname: A. surname: Skvortsov fullname: Skvortsov, A. organization: Maritime Division, Defence Science and Technology, Melbourne, Australia – sequence: 6 givenname: S. surname: Marburg fullname: Marburg, S. organization: Chair of Vibroacoustics of Vehicles and Machines, Department of Mechanical Engineering, Technische Universität München, München, Germany – sequence: 7 givenname: N. surname: Atalla fullname: Atalla, N. organization: Groupe d'Acoustique de l'Université de Sherbrooke, Université de Sherbrooke, Sherbrooke, J1K 2R1, Canada – sequence: 8 givenname: N. surname: Kessissoglou fullname: Kessissoglou, N. organization: School of Mechanical and Manufacturing Engineering, UNSW Sydney, Australia |
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Keywords | Turbulent boundary layer Uncorrelated wall plane waves Wall pressure field Acoustic radiation radiated noise pressure field synthesis vibroacoustic numerical method turbulent flow turbulent boundary layer flow noise |
Language | English |
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Snippet | The vibroacoustic response of a simply supported panel excited by turbulent flow is analytically and numerically investigated. In the analytical model, the... |
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SubjectTerms | Acoustic radiation Acoustics Boundary layer Computational fluid dynamics Excitation Finite element method Fluid flow Mathematical analysis Mathematical models Mechanics Numerical analysis Numerical models Numerical prediction Physics Plane waves Radiation Sound waves Stiffeners Turbulent boundary layer Turbulent flow Uncorrelated wall plane waves Wall pressure Wall pressure field Wind tunnels |
Title | Analytical and numerical prediction of acoustic radiation from a panel under turbulent boundary layer excitation |
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