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3D Generalized Inverse Beamforming in wind tunnel aeroacoustic testing: application to a Counter Rotating Open Rotor aircraft model

机译:风洞空气声学测试中的3D广义逆波束成形:在反向旋转开放旋翼飞机模型中的应用

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摘要

Inverse methods are gaining relevance in the aeroacoustic community for their capability to accurately localize and quantify noise sources. Indeed, since modern aircraft are more targeted to the reduction of fuel consumption, and very often some design choices, like Open Rotor (OR) propulsion systems, cause excessive acoustic emissions, accurate knowledge of noise source locations is of fundamental importance. This paper describes the use of an inverse method, namely Generalized Inverse Beamforming (GIBF), to characterize a Counter Rotating Open Rotor (CROR) installed on a 1/7th scale aircraft model. The model was tested in a large Low-Speed Wind Tunnel (WT) at The Pininfarina Aerodynamic and Aeroacoustic Research Center in Turin, Italy, within the framework of the FP7 EU Clean-Sky WENEMOR (Wind tunnel tests for the Evaluation of the installation effects of Noise EMissions of an Open Rotor advanced regional aircraft) project. With respect to previous works already published, the pros and cons of 3D GIBF formulation will be discussed on data collected from an industrial test case. A comparison of L-2 and L-1 norm formulations, as well as multiplicative approach and single array processing in 3D GIBF, will be performed, discussing their differences in terms of source localization accuracy. Since a quantitative analysis on real data cannot be provided because of confidentiality issues, the capability of the present approach to correctly quantify the source strength will be evaluated by considering a synthetic monopole source emitting white noise at different signal-to-noise-ratios (SNRs). Finally, it will be shown that 3D GIBF can provide engineers with more reliable data regarding the acoustic behavior of CROR-based aircrafts, this proving the advantages in exploiting this inverse method in WT aeroacoustic applications. (C) 2020 Elsevier Ltd. All rights reserved.
机译:逆方法因其准确定位和量化噪声源的能力而在航空声学界越来越重要。的确,由于现代飞机的目标更多是减少燃油消耗,并且很多设计选择(例如开放式转子(OR)推进系统)经常会产生过多的声发射,因此准确了解噪声源位置至关重要。本文介绍了一种反向方法,即广义反向波束成形(GIBF),以表征安装在1/7比例飞机模型上的反向旋转开放转子(CROR)的特性。该模型在FP7 EU Clean-Sky WENEMOR框架下在意大利都灵的Pininfarina空气动力学和空气声学研究中心的大型低速风洞(WT)中进行了测试(风洞测试,用于评估安装效果)开放旋翼先进支线飞机的噪声排放”项目)。关于已经发表的以前的作品,将根据从工业测试案例收集的数据来讨论3D GIBF公式的利弊。将进行L-2和L-1规范制定的比较,以及3D GIBF中的乘法方法和单阵列处理,并讨论它们在源定位精度方面的差异。由于由于机密性问题而无法提供对真实数据的定量分析,因此将通过考虑以不同信噪比(SNR)发射白噪声的合成单极子源来评估本方法正确量化源强度的能力。 )。最后,将显示3D GIBF可以为工程师提供有关基于CROR的飞机的声学特性的更可靠数据,这证明了在WT航空声学应用中采用这种逆方法的优势。 (C)2020 Elsevier Ltd.保留所有权利。

著录项

  • 来源
    《Applied Acoustics》 |2020年第6期|107229.1-107229.11|共11页
  • 作者

  • 作者单位

    Univ Politecn Marche Via Brecce Blanche 12 I-60131 Ancona Italy|Karman Inst Fluid Dynam Waterloosesteenweg 72 B-1640 Rhode St Genese Belgium;

    Univ Politecn Marche Via Brecce Blanche 12 I-60131 Ancona Italy;

    Karman Inst Fluid Dynam Waterloosesteenweg 72 B-1640 Rhode St Genese Belgium;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Generalized inverse beamforming; Aeroacoustics; Wind tunnel; Measurement techniques;

    机译:广义逆波束成形;航空声学;风洞测量技术;

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