Structural acoustic control of plates with variable boundary conditions: Design methodology

被引:9
|
作者
Sprofera, Joseph D.
Cabell, Randolph H.
Gibbs, Gary P.
Clark, Robert L.
机构
[1] Duke Univ, Pratt Sch Engn, Durham, NC 27708 USA
[2] NASA Langley Res Ctr, Struct Acoust Branch, Hampton, VA 23681 USA
[3] NASA Langley Res Ctr, Quiet Aircraft Technol Project, Hampton, VA 23681 USA
来源
基金
美国国家航空航天局;
关键词
D O I
10.1121/1.2739404
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
A method for optimizing a structural acoustic control system subject to variations in plate boundary conditions is provided. The assumed modes method is used to build a plate model with varying levels of rotational boundary stiffness to simulate the dynamics of a plate with uncertain edge conditions. A transducer placement scoring process, involving Hankel singular values, is combined with a genetic optimization routine to find spatial locations robust to boundary condition variation. Predicted frequency response characteristics are examined, and theoretically optimized results are discussed in relation to the range of boundary conditions investigated. Modeled results indicate that it is possible to minimize the impact of uncertain boundary conditions in active structural acoustic control by optimizing the placement of transducers with respect to those uncertainties. (c) 2007 Acoustical Society of America.
引用
收藏
页码:271 / 279
页数:9
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