Analytical Modeling of the Vibro-Acoustic Response of a Double-Walled Cylindrical Shell With Microperforation Excited by Turbulent Boundary Layer Pressure Fluctuations
Author:
Affiliation:
1. School of Energy and Power Engineering, Xi’an Jiaotong University, Xi’an, Shaanxi 710049, China e-mail:
Abstract
Funder
National Natural Science Foundation of China
Publisher
ASME International
Subject
General Engineering
Link
http://asmedigitalcollection.asme.org/vibrationacoustics/article-pdf/doi/10.1115/1.4038035/6349087/vib_140_02_021012.pdf
Reference42 articles.
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2. Use of Correlation Technique for Estimating In-Flight Noise Radiated by Wing-Mounted Jet Engines on a Fuselage;J. Sound Vib.,1971
3. Vibration Measurements of an Airplane Fuselage Structure—I: Turbulent Boundary Layer Excitation;J. Sound Vib.,1972
4. Vibration Measurements of an Airplane Fuselage Structure—II: Jet Noise Excitation;J. Sound Vib.,1972
5. Boundary Layer Induced Noise in Aircraft—Part I: The Flat Plate Model;J. Sound Vib.,1996
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