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Comparison of Computational and Experimental Microphone Array Results for an 18-Scale Aircraft Model

机译:18%比例飞机模型的计算和实验麦克风阵列结果的比较

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摘要

An 18%-scale, semispan model is used as a platform for examining the efficacy of microphone array processing using synthetic data from numerical simulations. Two hybrid RANS/LES codes coupled with Ffowcs Williams-Hawkings solvers are used to calculate 97 microphone signals at the locations of an array employed in the NASA LaRC 14×22 tunnel. Conventional, DAMAS, and CLEAN-SC array processing is applied in an identical fashion to the experimental and computational results for three different configurations involving deploying and retracting the main landing gear and a part-span flap. Despite the short time records of the numerical signals, the beamform maps are able to isolate the noise sources, and the appearance of the DAMAS synthetic array maps is generally better than those from the experimental data. The experimental CLEAN-SC maps are similar in quality to those from the simulations indicating that CLEAN-SC may have less sensitivity to background noise. The spectrum obtained from DAMAS processing of synthetic array data is nearly identical to the spectrum of the center microphone of the array, indicating that for this problem array processing of synthetic data does not improve spectral comparisons with experiment. However, the beamform maps do provide an additional means of comparison that can reveal differences that cannot be ascertained from spectra alone.
机译:18%比例的半跨度模型用作使用数值模拟的合成数据检查麦克风阵列处理效果的平台。与Ffowcs Williams-Hawkings求解器结合使用的两个混合RANS / LES代码用于在NASA LaRC 14×22隧道中采用的阵列位置计算97个麦克风信号。常规,DAMAS和CLEAN-SC阵列处理以相同的方式应用于三种不同配置的实验和计算结果,包括展开和缩回主起落架和部分跨度襟翼。尽管数字信号的记录时间很短,但波束图仍能够隔离噪声源,并且DAMAS合成阵列图的外观通常比实验数据更好。实验性CLEAN-SC图的质量与模拟结果相似,表明CLEAN-SC对背景噪声的敏感性较低。从合成阵列数据的DAMAS处理获得的频谱几乎与阵列中央麦克风的频谱相同,这表明针对此问题,合成数据的阵列处理无法改善与实验的频谱比较。但是,波束图确实提供了一种额外的比较方式,可以揭示仅凭光谱无法确定的差异。

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