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Initial Assessment of Acoustic Source Visibility with a 24-element Microphone Array in the Arnold Engineering Development Center 80- by 120-Foot Wind Tunnel at NASA Ames Research Center

机译:NASA AMES研究中心的Arnold Engineering开发中心24元麦克风阵列初步评估了24元麦克风阵列的声学源可见度

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Measurements of background noise were recently obtained with a 24-element phased microphone array in the test section of the Arnold Engineering Development Center 80-byl20-Foot Wind Tunnel at speeds of 50 to 100 knots (27.5 to 51.4 m/s). The array was mounted in an aerodynamic fairing positioned with array center 1.2m from the floor and 16 m from the tunnel centerline, The array plate was mounted flush with the fairing surface as well as recessed 1/2 in. (1.27 cm) behind a porous Kevlar screen. Wind-off speaker measurements were also acquired every 15° on a 10 m semicircular arc to assess directional resolution of the array with various processing algorithms, and to estimate minimum detectable source strengths for future wind tunnel aeroacoustic studies. The dominant background noise of the facility is from the six drive fans downstream of the test section and first set of turning vanes. Directional array response and processing methods such as background-noise cross-spectral-matrix subtraction suggest that sources 10-15 dB weaker than the background can be detected.
机译:最近获得的背景噪声的测量,用24元件在阿诺德工程开发中心80 byl20英尺风洞的测试部分的相控麦克风阵列在50至100节(27.5至51.4米/秒)的速度。该阵列被安装在位于与从地板阵列中心1.2米和从隧道中心线16米一个气动整流罩,所述阵列板平齐安装与整流罩表面以及在凹1/2英寸(1.27cm)的后面的多孔芳纶屏幕。开卷扬声器测量还获取每15°上10μm的半圆弧形,以评估与各种处理算法阵列的定向分辨率,并估计最小可检测源强度为未来的风洞空气声学研究。该设施的占主导地位的背景噪声是从测试部分和第一组转向叶片的下游的6个驱动风扇。定向阵列的响应和处理方法,诸如背景噪声交叉频谱矩阵减法表明源10-15分贝弱于背景可被检测。

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