Analytical Modeling of the Vibro-Acoustic Response of a Double-Walled Cylindrical Shell With Microperforation Excited by Turbulent Boundary Layer Pressure Fluctuations

被引:10
|
作者
Zhang, Qunlin [1 ]
Mao, Yijun [1 ]
Qi, Datong [1 ]
机构
[1] Xi An Jiao Tong Univ, Sch Energy & Power Engn, Xian 710049, Shaanxi, Peoples R China
基金
中国国家自然科学基金;
关键词
double-walled cylindrical shell; vibro-acoustic; perforation; AIRPLANE FUSELAGE STRUCTURE; SOUND-TRANSMISSION LOSS; WAVE-NUMBER APPROACH; INDUCED NOISE; VIBRATION MEASUREMENTS; AIRCRAFT; PANEL; ABSORPTION; FLOW; RADIATION;
D O I
10.1115/1.4038035
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
An analytical model is developed to investigate the vibro-acoustic response of a double-walled cylindrical shell with the inner wall perforated when excited by the external turbulent boundary layer (TBL) pressure fluctuations. The shell motion is governed by the Donnell's thin shell theory, and the mean particle velocity model is employed to describe the boundary condition between the microperforated shell and fluid media. Numerical results indicate that the transmission loss (TL) for the configuration of microperforating the inner wall could be larger than that for the conventional solid double-walled cylindrical shell with and without the core of porous material over a wide frequency range. Comparison between TL results with excitations from the TBL and the acoustic diffuse field (ADF) shows that with the thought of microperforating the inner shell, to reduce the acoustical excitation will be of more importance than the flow excitation over the ring frequency for a quiet interior space. Parametric studies illustrate that the perforation ratio is the main factor affecting the sound insulation performance through the total reactance.
引用
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页数:13
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