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2018 AIAA/CEAS Aeroacoustics Conference最新文献

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Flight-Test Evaluation of Airframe Noise Mitigation Technologies 机身降噪技术的试飞评估
Pub Date : 2018-06-24 DOI: 10.2514/6.2018-2972
M. Khorrami, D. Lockard, W. Humphreys, Patricio A. Ravetta
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引用次数: 20
S1MAWind Tunnel New Aeroacoustic Capability: a Traversing Microphone Array s1ma风洞新型气动声学性能:一种遍历式麦克风阵列
Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3137
F. Nicolas, M. Rey
This paper aims at describing the new measurement device installed in S1MA wind tunnel for aeroacoustics tests. We present here the in-situ qualification of a traversing microphone array which equipped the acoustic closed test section of the wind tunnel. First, we show that it allows us to capture very complex directivity patterns thanks to a very good spatial resolution. Secondly, we demonstrate the ability of continuous scans measurements to perform as well as stabilized acquisitions, leading to a major improvement in wind tunnel productivity. Finally, we also take advantage of the microphone array to denoise acquisition data using beamforming processing.
本文介绍了安装在S1MA风洞中用于气动声学试验的新型测量装置。本文介绍了安装在风洞声学封闭试验段的一种遍历传声器阵列的现场鉴定。首先,我们表明,由于具有非常好的空间分辨率,它允许我们捕获非常复杂的指向性模式。其次,我们展示了连续扫描测量的能力,以及稳定采集的能力,从而大大提高了风洞生产率。最后,我们还利用麦克风阵列对采集数据进行波束成形处理。
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引用次数: 4
Experimental Study of Axisymmetric Cavities in Supersonic Flow 超声速流动轴对称空腔的实验研究
Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3292
B. T. Brooker, Narendra S. Chaganti, S. Olçmen, G. Cheng
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引用次数: 1
Compact beam liners for low frequency noise 用于低频噪声的紧凑型光束衬垫
Pub Date : 2018-06-24 DOI: 10.2514/6.2018-4101
M. Farooqui, Y. Aurégan
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引用次数: 0
Experimental Investigation of Acoustical Coupling between Cavity Flow and Cross Cylinder Wake 空腔流与横柱尾流声学耦合的实验研究
Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3471
Hao Guo, Xuan Liang, T. Hu, Peiqing Liu
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引用次数: 0
Experimental and Numerical Study of Passive Gap Noise 被动间隙噪声的实验与数值研究
Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3595
L. Erbig, Nan Hu, S. Lardeau
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引用次数: 6
Measurement of Flow Separation Noise on a Full-scale Wind Turbine 全尺寸风力机流动分离噪声的测量
Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3462
S. Buck
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引用次数: 3
Opportunities and Challenges for X-plane Acoustic Flight Research x飞机声学飞行研究的机遇与挑战
Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3127
Russell H. Thomas, Yueping Guo
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引用次数: 1
Experimental Characterization of Vortex Generators Induced Noise of Wind Turbines 风力发电机涡发生器诱导噪声的实验表征
Pub Date : 2018-06-24 DOI: 10.2514/6.2018-2800
D. Kolkman, L. D. Santana, A. V. Garrel, C. Venner, Arlos Arce León, M. Sanders
The wind energy industry is progressively aiming towards larger wind turbine size as a means of increasing energy production efficiency. Wind turbine rotor blades are becoming significantly more flexible and have an increased risk of structural failure. Thicker airfoil profiles can be used to increase the structural strength. However, thicker airfoils are more prone to flow separation with adverse effect on power generation. Vortex generators (VGs) are an effective solution to delay flow separation. However, VGs significantly increase radiated noise levels. This presented research experimentally investigates the effect of VGs on blade noise production. Specifically, the influence of the VG geometric shape is evaluated while keeping the dimensions constant. Wind tunnel tests have been carried out on a NACA 0018 that is equipped with triangular vane-type VGs specifically designed for the test conditions. A microphone phased array is used to assess the radiated noise using the beamforming technique. The results show that the VGs significantly contribute to increase the blade noise production with having a predominant role at high-frequencies where the VG acts as a non-compact aeroacoustic source.
风能工业正逐步瞄准更大的风力涡轮机尺寸,作为提高能源生产效率的手段。风力涡轮机的转子叶片变得更加灵活,结构失效的风险也在增加。更厚的翼型轮廓可以用来增加结构强度。然而,较厚的翼型更容易发生流动分离,对发电产生不利影响。涡流发生器是解决延迟流动分离问题的有效方法。然而,VGs显著增加了辐射噪声水平。本文通过实验研究了VGs对叶片噪声产生的影响。具体来说,在保持尺寸不变的情况下,评估了VG几何形状的影响。风洞试验已经在NACA 0018上进行,该飞机配备了专门为试验条件设计的三角叶片型VGs。利用波束形成技术,采用传声器相控阵对辐射噪声进行评估。结果表明,在非紧凑型气动声源作用下,涡扇对叶片噪声产生有显著的促进作用,且在高频段具有主导作用。
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引用次数: 2
Sound Absorption of Sintered Stainless Steel Fiber Blocks 烧结不锈钢纤维块的吸声性能
Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3928
J. A. Tuasikal, Kanta Sato, H. Daiguji, T. Ishii
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引用次数: 2
期刊
2018 AIAA/CEAS Aeroacoustics Conference
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