介电弹性体声学衬垫的建模、设计与优化

IF 1.2 4区 工程技术 Q3 ACOUSTICS International Journal of Aeroacoustics Pub Date : 2023-10-03 DOI:10.1177/1475472x231199187
Chelsea Solano, Louis Cattafesta
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引用次数: 0

摘要

研究了嵌入式介质弹性体(DE)膜声学衬垫的建模、设计和优化问题。当DE受到电压作用时,衬垫的声阻抗被改变,从而导致面内应力的减小。建立了嵌入式介质弹性体声学衬垫的集总单元模型,并在法向入射阻抗管中进行了验证,并对其性能进行了优化。优化成本函数包括(1)在目标频率范围(400 - 1600 Hz)内平均吸收系数的最大化和(2)膜激活时衬里基共振频率变化的最大化。观测到的吸收与预测的很好地吻合。谐振频率的调整需要使用阻抗虚部的谐振数值解,因为由于衬垫声学和DE膜的电力学之间的复杂耦合,不能推导出谐振的简单解析表达式。尽管如此,用集总单元模型预测的谐振频移比用激活的衬垫样品测量的要好,其频移为213 Hz。
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Modeling, design, and optimization of a dielectric elastomer acoustic liner
The modeling, design, and optimization of an embedded dielectric elastomer (DE) membrane acoustic liner is considered. The acoustic impedance of the liner is modified when the DE is subjected to voltage, resulting in a reduction of the in-plane stress. A lumped element model of an embedded dielectric elastomer acoustic liner is derived and validated in a normal incidence impedance tube and is subsequently used to optimize its performance. The optimization cost functions include (1) maximization of the average absorption coefficient over a targeted frequency range, 400 – 1600 Hz and (2) maximization of the change in the liner fundamental resonance frequency when the membrane is activated. Good agreement between measured and predicted absorption is observed. Tuning of the resonant frequency requires a numerical solution for resonance using the imaginary part of the impedance, since a simple analytical expression for resonance cannot be derived due to the complex coupling between the acoustics of the liner and the electro-mechanics of the DE membrane. Nonetheless, resonant frequency shifts predicted with the lumped element model compare favorably to those measured with the activated liner sample, with a shift of 213 Hz.
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来源期刊
International Journal of Aeroacoustics
International Journal of Aeroacoustics ACOUSTICS-ENGINEERING, AEROSPACE
CiteScore
2.10
自引率
10.00%
发文量
38
审稿时长
>12 weeks
期刊介绍: International Journal of Aeroacoustics is a peer-reviewed journal publishing developments in all areas of fundamental and applied aeroacoustics. Fundamental topics include advances in understanding aeroacoustics phenomena; applied topics include all aspects of civil and military aircraft, automobile and high speed train aeroacoustics, and the impact of acoustics on structures. As well as original contributions, state of the art reviews and surveys will be published. Subtopics include, among others, jet mixing noise; screech tones; broadband shock associated noise and methods for suppression; the near-ground acoustic environment of Short Take-Off and Vertical Landing (STOVL) aircraft; weapons bay aeroacoustics, cavity acoustics, closed-loop feedback control of aeroacoustic phenomena; computational aeroacoustics including high fidelity numerical simulations, and analytical acoustics.
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