掠流作用下双亥姆霍兹谐振器系统的声学性能

IF 1.2 4区 工程技术 Q3 ACOUSTICS International Journal of Aeroacoustics Pub Date : 2023-01-02 DOI:10.1177/1475472X221150175
Rong Xue, C. Mak, Dizi Wu, K. W. Ma
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引用次数: 0

摘要

亥姆霍兹谐振器广泛用于航空发动机系统的降噪。通过串联一对hr(颈-腔-颈-腔),形成双hr系统。研究了颈部长度、空腔体积和流动马赫数对双hr系统降噪性能的影响。通过三维数值模拟计算了传输损耗结果。传输损耗(TL)结果表明,第二颈部长度会影响第二共振频率和传输损耗最大值。与大流量相比,小流量条件下改变腔体体积对噪声衰减能力有显著影响。流动马赫数对第一个TL峰的影响比对第二个TL峰的影响更显著。研究结果揭示了双hr系统的几何参数、掠掠流量与降噪性能之间的关系,可为航空发动机双hr系统的设计提供指导。
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The acoustic performance of a dual Helmholtz resonators system in the presence of a grazing flow
Helmholtz resonators (HR) are widely used in aero-engine systems for noise reduction. By connecting a pair of HRs in series (neck-cavity-neck-cavity), a dual HRs system is formed. This study investigated the influence of neck length, cavity volume and flow Mach number on the noise attenuation performance of a dual HRs system. A three-dimensional numerical simulation was performed to calculate the transmission loss results. The transmission loss (TL) results indicated that the second neck length can influence the second resonance frequency and TL max . Changing the cavity volume significantly influences the noise attenuation ability under lower flow rate conditions compared to higher flow rate conditions. The flow Mach number had a more significant impact on the first TL peak than on the second TL peak. This study shows the relationship between the geometric parameters, grazing flow and noise attenuation performance of a dual HRs system and could provide guidance in designing suitable dual HRs for aero-engine systems.
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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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