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Vortex shedding noise from a beveled trailing edge

机译:斜面后缘的涡流脱落噪声

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Coherent vortex shedding from blunt and beveled trailing edges generates tonal noise, which is usually undesired. To obtain a better understanding of the noise generation under such conditions, the flow field around a beveled trailing edge was characterized for Reynolds numbers based on the bluntness ranging from 2.5x10(4) to 5.1x10(4). Flow field statistics were obtained by means of planar high-speed two-component and stereoscopic particle image velocimetry measurements. The development of the shear layers and vortex roll-up is described in the present study. Related length scales, the vortex formation length, and wake thickness parameter were derived from the measurements. Noise emission due to vortex shedding was predicted from an analytic solution, derived from diffraction theory and the reversed Sears' problem, and compared to acoustic phased array measurements. This approach has previously been shown to provide accurate results for sharply truncated edges, but questions with regard to the applicability with different trailing edge geometries remained open. The prediction required the auto-spectral density, correlation length, and convective velocity of the upwash velocity component in the vortex formation region. Direct application with data obtained from particle image velocimetry measurements showed an overestimation of about 20dB when compared to the acoustic measurements. The results thus showed that the prediction of vortex shedding noise based on the simplified wake model and diffraction theory is not generally applicable.
机译:钝角和斜角后缘产生的相干涡流会产生音调噪声,通常是不希望的。为了更好地了解这种情况下的噪声,基于2.5x10(4)至5.1x10(4)的钝度,针对雷诺数对斜面后缘周围的流场进行了表征。流场统计数据是通过平面高速两分量和立体粒子图像测速仪测量获得的。在本研究中描述了剪切层的发展和涡旋卷起。相关的长度尺度,涡旋形成长度和尾流厚度参数是从测量得出的。由解析理论预测了由涡旋脱落引起的噪声发射,该分析解决方案源自衍射理论和反向的西尔斯问题,并将其与声相控阵测量结果进行了比较。先前已证明此方法可为锐利的截断边缘提供准确的结果,但是有关使用不同后边缘几何形状的适用性的问题仍然存在。该预测需要涡旋形成区域中上冲速度分量的自谱密度,相关长度和对流速度。与声波测量相比,直接应用从粒子图像测速测量获得的数据显示出高估了约20dB。因此结果表明,基于简化的尾波模型和衍射理论的涡旋脱落噪声的预测通常不适用。

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