均匀和多区域声学衬垫的阻抗降低

IF 1.2 4区 工程技术 Q3 ACOUSTICS International Journal of Aeroacoustics Pub Date : 2021-06-16 DOI:10.1177/1475472X211023855
Michael G. Jones, D. Nark, B. M. Howerton
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引用次数: 1

摘要

本文介绍了基于美国宇航局兰利掠流阻抗管数据的5个均匀和2个多区衬垫的计算结果。使用proony和CHE两种方法,在许多测试条件下推导出每个衬垫的阻抗谱。proony方法是有效的,通常提供准确的结果均匀衬管,但不太适合多区衬管。CHE方法支持对均匀和多区衬垫进行评估,但计算成本要高得多。这些衬垫的结果证明了两种衰减方法的有效性,但也清楚地表明,需要足够的衰减来支持准确的阻抗衰减。对于本研究中考虑的衬垫,数据表明,为了确保高质量的阻抗消减结果,多区衬垫的每个区域大约需要3 dB的衰减。这项研究是为了响应国际航空研究论坛下多个国家实验室合作的两项声学衬垫研究挑战而进行的。
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Impedance eduction for uniform and multizone acoustic liners
This paper presents results for five uniform and two multizone liners based on data acquired in the NASA Langley Grazing Flow Impedance Tube. Two methods, Prony and CHE, are used to educe the impedance spectra for each of these liners for many test conditions. The Prony method is efficient and generally provides accurate results for uniform liners, but is not well suited for multizone liners. The CHE method supports assessment of both uniform and multizone liners, but is much more computationally expensive. The results from these liners demonstrate the efficacy of both eduction methods, but also clearly demonstrate that sufficient attenuation is required to support accurate impedance eduction. For the liners considered in this study, the data indicate approximately 3 dB attenuation is needed for each zone of a multizone liner in order to ensure quality impedance eduction results. This study was conducted in response to two acoustic liner research challenges in support of a collaboration of multiple national laboratories under the International Forum for Aviation Research.
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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.
期刊最新文献
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