Effects of general boundary conditions on vibro-acoustic responses of the panel-cavity system induced by a turbulent boundary layer

被引:3
|
作者
Xiao, Heye [1 ]
Xu, Chi Z. [2 ]
Yu, Pei X. [2 ]
Gu, Jin T. [3 ]
Sui, Dan [2 ]
Zhou, Jie [2 ]
机构
[1] Northwestern Polytech Univ, Unmanned Syst Res Inst, Xian, Peoples R China
[2] Northwestern Polytech Univ, Sch Aeronaut, 127 Youyi West Rd, Xian 710072, Peoples R China
[3] Aviat Ind Corp China Ltd, Aircraft Design & Res Inst 1, Xian, Peoples R China
基金
中国国家自然科学基金;
关键词
panel-cavity system; boundary conditions; turbulent boundary layer; vibro-acoustic; power spectrum density; STRUCTURAL RESPONSE; SOUND-TRANSMISSION; RECTANGULAR CAVITY; PLATES;
D O I
10.1177/10775463211066724
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
This study proposes an analytical method for building a vibro-acoustic model of a panel-cavity system induced by a turbulent boundary layer (TBL) excitation, which is used to study the influences of boundary conditions on the vibro-acoustic responses of the system. In the theoretic model, the elastic restraints at the plate's edges and the wall impedance of the cavity wall are considered at the same time. Based on the mode expansion, the vibro-acoustic response function of the vibro-acoustic model is built to present the coupling between the TBL and the system constructed by the panel and the cavity. Then, the model is validated by comparing it with the previous study, which shows good agreements. Finally, the effects of the boundary conditions, such as stiffness, damping, and impedance, on the mean quadratic velocity spectra and radiated sound power of the panel-cavity system are studied. It is demonstrated that the decrease of the boundary stiffness makes the radiated sound power of the panel drop above the frequency of the panel third mode. The boundary damping of the panel decreases the vibro-acoustic response of the panel-cavity system by working as an attenuation factor of the boundary. Furthermore, the increase of the radiated sound power with different wall impedances is due to the coupling between the structural mode of the panel and the acoustic mode of the cavity, or the resonance of acoustic mode in the vibration propagation direction.
引用
收藏
页码:1564 / 1576
页数:13
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