A scaling procedure for panel vibro-acoustic response induced by turbulent boundary layer-Reference-Cited by-同舟云学术

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A scaling procedure for panel vibro-acoustic response induced by turbulent boundary layer

Published:2016-10 Issue: Volume:380 Page:165-179
ISSN:0022-460X
Container-title:Journal of Sound and Vibration
language:en
Short-container-title:Journal of Sound and Vibration

Author:

Xiaojian Zhao,Bangcheng AI,Ziqiang Liu,Dun Li

Funder

National Key Basic Research and Development Program of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Acoustics and Ultrasonics,Condensed Matter Physics

Reference24 articles.

1. Boundary layer induced noise in aircraft, part I: the flat plate model;Graham;Journal of Sound and Vibration,1996

2. Boundary layer induced noise in aircraft, part II: the trimmed flat plate model;Graham;Journal of Sound and Vibration,1996

3. A comparison of models for the wavenumber–frequency spectrum of turbulent boundary layer pressures;Graham;Journal of Sound and Vibration,1997

4. An analytical solution for the self and mutual radiation resistances of a rectangular plate;Li;Journal of Sound and Vibration,2001

5. A wavenumber approach to modeling the response of a randomly excited panel, part I: general theory;Maury;Journal of Sound and Vibration,2002

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1. Effects of general boundary conditions on vibro-acoustic responses of the panel-cavity system induced by a turbulent boundary layer;Journal of Vibration and Control;2022-02-10

2. Spatial correlation effect of a multidimensional force on vibration suppression;Aerospace Science and Technology;2021-10

3. Model updating of a scaled piping system and vibration attenuation via locally resonant bandgap formation;International Journal of Mechanical Sciences;2021-03

4. A Hybrid UWPW-FEM Technique for Vibroacoustic Analysis of Panels Subject to a Turbulent Boundary Layer Excitation;Flinovia—Flow Induced Noise and Vibration Issues and Aspects-III;2021

5. Analytical and numerical prediction of acoustic radiation from a panel under turbulent boundary layer excitation;Journal of Sound and Vibration;2020-08

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