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Noise Reduction of a Model-Scale Landing Gear Measuredin the Virginia Tech Aeroacoustic Wind Tunnel

机译:模型级落地齿轮的降噪测量弗吉尼亚科技出发风隧道

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The effectiveness of various fairings for landing gear noise reduction was measured in the Virginia Tech (VT) Stability Wind Tunnel. This wind tunnel was recently upgraded to an aeroacoustic facility, which allowed acoustic measurements to be carried out in the far-field, out of the flow, and in a low reverberant environment. The model was a very faithful replica of the full-scale landing gear, designed to address the issues associated with low-fidelity models. A 63-element microphone phased array was used to locate the noise source components of the landing gear in its baseline and streamlined configurations, and to measure the noise reduction potential of the fairings. Measurements were carried out from two far-field positions on the flyover path of the landing gear. Through a comparison between the noise levels of the landing gear with and without fairing, the noise reduction potential of each fairing could be estimated. The results from these experiments also showed that if phased-array measurements of the landing gear noise are carried out in the near-field, the noise reduction potential of the fairings could be largely overestimated.
机译:弗吉尼亚科技(VT)稳定风隧道测量了各种公平的落地齿轮噪声减少的有效性。该风洞最近升级到航空声设施,其允许在远场中进行声学测量,流出流动,并在低音混响环境中进行。该模型是全规模着陆装备的一个非常忠实的复制品,旨在解决与低保真模型相关的问题。使用63元件麦克风相控阵列将着陆齿轮的噪声源组件以其基线和流线型配置定位,并测量整个公平的降噪电位。从起落架的天桥路径上的两个远场位置进行测量。通过与且没有整流罩的着陆齿轮的噪声水平之间的比较,可以估计每个整流罩的降噪电位。这些实验的结果也表明,如果在近场进行着陆齿轮噪声的分阶段阵列测量,则公平的降噪电位可能在很大程度上高估。

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