The Prediction of Noise from Turbulent Boundary Layers Attached to Porous Media

Elisha R. Pager, Steven A. E. Miller
{"title":"The Prediction of Noise from Turbulent Boundary Layers Attached to Porous Media","authors":"Elisha R. Pager, Steven A. E. Miller","doi":"10.2514/6.2018-3297","DOIUrl":null,"url":null,"abstract":"Aerospace vehicles, wind tunnel test section walls, and other structures often contain porosity that alters the turbulent boundary layer and radiated noise. A semi-empirical mathematical model is developed to predict and analyze the acoustic radiation from turbulent boundary layers over porous media. The model is an acoustic analogy that depends on local flow-field statistics. These statistics are calculated through a steady Reynoldsaveraged Navier-Stokes computational fluid dynamics solver that includes porous material. Acoustic predictions are conducted for four subsonic Mach numbers without a pressure gradient. At each Mach number, four porosities with constant liner depth and porous turbulent length scale are examined along with the non-porous solution. The flow-field is validated through comparison with acoustic measurement. Predictions are conducted to ascertain changes in acoustic radiation with varying porosity. We find that noise is amplified or reduced in a non-intuitive way with the introduction of porosity, variation of frequency, and increase of Mach number.","PeriodicalId":429337,"journal":{"name":"2018 AIAA/CEAS Aeroacoustics Conference","volume":"2 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2018-06-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2018 AIAA/CEAS Aeroacoustics Conference","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.2514/6.2018-3297","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 1

Abstract

Aerospace vehicles, wind tunnel test section walls, and other structures often contain porosity that alters the turbulent boundary layer and radiated noise. A semi-empirical mathematical model is developed to predict and analyze the acoustic radiation from turbulent boundary layers over porous media. The model is an acoustic analogy that depends on local flow-field statistics. These statistics are calculated through a steady Reynoldsaveraged Navier-Stokes computational fluid dynamics solver that includes porous material. Acoustic predictions are conducted for four subsonic Mach numbers without a pressure gradient. At each Mach number, four porosities with constant liner depth and porous turbulent length scale are examined along with the non-porous solution. The flow-field is validated through comparison with acoustic measurement. Predictions are conducted to ascertain changes in acoustic radiation with varying porosity. We find that noise is amplified or reduced in a non-intuitive way with the introduction of porosity, variation of frequency, and increase of Mach number.
查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
多孔介质附著湍流边界层的噪声预测
航空航天飞行器、风洞试验段壁和其他结构通常含有孔隙,这些孔隙会改变湍流边界层和辐射噪声。建立了一种预测和分析多孔介质湍流边界层声辐射的半经验数学模型。该模型是基于局部流场统计的声学类比。这些统计数据是通过包括多孔材料在内的稳定reynolds平均Navier-Stokes计算流体动力学求解器计算出来的。在没有压力梯度的情况下,对四个亚音速马赫数进行了声学预测。在每个马赫数下,研究了四种具有恒定衬里深度和多孔湍流长度尺度的孔隙率以及非多孔溶液。通过与声学测量结果的对比,验证了流场的正确性。预测是为了确定不同孔隙度下声辐射的变化。我们发现,随着孔隙度的引入、频率的变化和马赫数的增加,噪声以非直观的方式被放大或减小。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 去求助
来源期刊
自引率
0.00%
发文量
0
期刊最新文献
Correction: The Dynamic Response of a Pinhole Microphone under Flows of Varying Shear Stress Correction: Effects of Free Stream Disturbance on the Development of the Compressible Flow around a Square Cylinder at Subsonic Mach Numbers Withdrawal: Experimental Investigation on Circular Cylinders with Metal Foam for Noise Reduction Withdrawal: Experimental investigation of the effect of slat deflection angle variation on aerodynamic noise characteristic Correction: Unsteady coherent surface-pressure fluctuations from time-averaged flow data with given two-point statistics
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 联系我们:info@booksci.cn
Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。
Copyright © 2023 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1