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2018 AIAA/CEAS Aeroacoustics Conference最新文献

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Correction: On the superior performance of leading edge slits over serrations for the reduction of aerofoil interaction noise 更正:关于优越的性能前缘狭缝超过锯齿,以减少翼型相互作用噪音
Pub Date : 2018-06-25 DOI: 10.2514/6.2018-3121.C1
Chaitanya C. Paruchuri, P. Joseph, Lorna J. Ayton
Aerofoils operating in a turbulent flow are an efficient source of noise radiation by scattering vorticity into sound at the leading edge. Much work has now been undertaken demonstrating the effectiveness by which serrations, or undulations, introduced onto the leading edge, can substantially reduce broadband leading edge interaction noise. However, all of this work is focused on sinusoidal leading edge serration profiles. In this paper, a family of alternative serration profiles are proposed that are capable of providing significantly greater noise reductions than single-wavelength serrations at optimal conditions. This new family of profiles will be shown to reduce interaction noise through a fundamentally different noise reduction mechanism than conventional single-wavelength profiles. Unlike single-wavelength profiles, which produce a single compact dominant source region per serration wavelength, these new profiles are designed to produce two dominant compact sources per serration wavelength of the same source strength, that are separated in the streamwise direction. Since these sources are arranged to be closer together than the turbulence length-scale, they are highly coherent and therefore radiate with a difference in phase. A frequency therefore exists at which the sources are exactly 180° out of phase leading to very high levels of noise reduction in the far field.
在湍流中工作的翼型是一种有效的噪声辐射源,通过在前缘将涡度散射成声音。现在已经进行了大量的工作,证明了在前缘引入锯齿或波动的有效性,可以大大降低宽带前缘相互作用噪声。然而,所有这些工作都集中在正弦前缘锯齿剖面上。在本文中,一个家族的替代锯齿轮廓提出,能够提供显著更大的降噪比单波长锯齿在最佳条件下。与传统的单波长谱相比,这种新的谱将通过一种根本不同的降噪机制来减少相互作用的噪声。与单波长剖面不同,单波长剖面在每个锯齿波长产生一个紧凑的主要源区域,这些新的剖面设计为在每个锯齿波长产生两个相同强度的主要紧凑源,它们在流方向上分开。由于这些源被安排得比湍流长度尺度更靠近,它们是高度相干的,因此以相位差异辐射。因此,存在一个频率,在这个频率上,源的相位正好是180°,导致远场的噪声降低水平非常高。
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引用次数: 7
Correction: Unsteady coherent surface-pressure fluctuations from time-averaged flow data with given two-point statistics 修正:从给定两点统计的时间平均流量数据得出的非定常相干表面压力波动
Pub Date : 2018-06-25 DOI: 10.2514/6.2018-4097.C1
F. Avallone, D. Casalino, D. Ragni
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引用次数: 0
Correction: Effects of Free Stream Disturbance on the Development of the Compressible Flow around a Square Cylinder at Subsonic Mach Numbers 修正:自由流扰动对亚音速马赫数下绕方圆柱可压缩流动发展的影响
Pub Date : 2018-06-25 DOI: 10.2514/6.2018-4105.C1
Yohei Inoue, Tsuyoshi Kanuma, Yuma Tasai, H. Maekawa
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引用次数: 0
Withdrawal: Progress in aeroacoustic experimental investigation of high-lift device and landing gear model at D5 wind tunnel 结论:D5风洞大升力装置及起落架模型气动声学实验研究进展
Pub Date : 2018-06-25 DOI: 10.2514/6.2018-3469.C1
Peiqing Liu, Yu-ming Xing, Ling Li, Hao Guo
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引用次数: 0
Correction: Towards Direct Computation of Aeroacoustic Noise with the High-Order FR/CPR Method 修正:用高阶FR/CPR方法直接计算航空声学噪声
Pub Date : 2018-06-25 DOI: 10.2514/6.2018-4095.C1
Jingchang Shi, H. Yan, Z. Wang
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引用次数: 0
Withdrawal: Experimental Investigation of Acoustical Coupling between Cavity Flow and Cross Cylinder Wake 摘要:空腔流与横柱尾流声学耦合的实验研究
Pub Date : 2018-06-25 DOI: 10.2514/6.2018-3471.C1
Xuan Liang, G. Hao, T. Hu, Peiqing Liu
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引用次数: 0
Correction: Acoustic emission from one-dimensional vibrating porous panels in a single-sided flow 修正:单面流中一维振动多孔板的声发射
Pub Date : 2018-06-25 DOI: 10.2514/6.2018-2962.C1
Rozhin Hajian, J. Jaworski, S. Grace
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引用次数: 0
Correction: Deconvolution of the wave number - frequency spectra of wall pressure fluctuations 修正:壁面压力波动的波数-频率谱的反褶积
Pub Date : 2018-06-25 DOI: 10.2514/6.2018-3291.C1
S. Prigent, R. Engelman, E. Salze, C. Bailly
{"title":"Correction: Deconvolution of the wave number - frequency spectra of wall pressure fluctuations","authors":"S. Prigent, R. Engelman, E. Salze, C. Bailly","doi":"10.2514/6.2018-3291.C1","DOIUrl":"https://doi.org/10.2514/6.2018-3291.C1","url":null,"abstract":"","PeriodicalId":429337,"journal":{"name":"2018 AIAA/CEAS Aeroacoustics Conference","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-06-25","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"128897381","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Withdrawal: Experimental investigation of the effect of slat deflection angle variation on aerodynamic noise characteristic 结论:板条偏转角度变化对气动噪声特性影响的实验研究
Pub Date : 2018-06-25 DOI: 10.2514/6.2018-3798.C1
XinXin Geng, Hao Guo, T. Hu, Ling Li, Peiqing Liu
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引用次数: 0
Withdrawal: Experimental Investigation on Circular Cylinders with Metal Foam for Noise Reduction 结论:金属泡沫圆柱的降噪实验研究
Pub Date : 2018-06-25 DOI: 10.2514/6.2018-4107.C1
Fanglin Liu, Hao Guo, T. Hu, Peiqing Liu
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引用次数: 0
期刊
2018 AIAA/CEAS Aeroacoustics Conference
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