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Non-intrusive planar velocity-based nearfield acoustic holography in moving fluid medium

机译:运动流体介质中基于非侵入性平面速度的近场声全息

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摘要

Nearfield Acoustic Holography (NAH) is a powerful acoustic imaging method, but its application in aeronautics can be limited by intrusive measurements of acoustic field. In this paper, a moving fluid medium NAH procedure using non-intrusive velocity measurements is proposed. This method is based on convective Kirchhoff-Helmholtz integral formula. Convective equations and convective Green's function are used to derive convective real-space propagators including airflow effects. Discrete Fourier transforms of these propagators allow the assessment of acoustic fields from acoustic pressure or normal acoustic velocity measurements. As the aim is to derive an in-flow velocity-based NAH method, this study is especially focused on real convective velocity-to-pressure propagator. In order to validate this procedure, simulations in the case of monopole sources radiating in various uniform subsonic flows have been performed. NAH provides very favorable results when compared to the simulated fields. A comparison of results obtained by the real propagator and those obtained by the wave number-frequency-domain one developed by Kwon [J. Acoust. Soc. Am. 128(4), 1823-1832 (2010)] shows the interest of using the real-form in the case of pressure backward propagation from velocity measurements. The efficiency of the developed procedure is confirmed by a wind tunnel campaign with a flush-mounted loudspeaker and non-intrusive Laser Doppler Velocimetry velocity measurements.
机译:近场声全息术(NAH)是一种强大的声成像方法,但是其在航空领域的应用可能会受到声场的侵入式测量的限制。在本文中,提出了一种使用非侵入式速度测量的运动流体介质NAH程序。该方法基于对流Kirchhoff-Helmholtz积分公式。对流方程和对流格林函数用于导出对流真实空间传播器,包括气流效应。这些传播器的离散傅立叶变换允许从声压或正常声速测量中评估声场。由于目的是推导基于流速的NAH方法,因此本研究特别关注于实际对流速度-压力传播器。为了验证该程序,已经对单极子源以各种均匀的亚音速流辐射的情况进行了仿真。与模拟场相比,NAH提供了非常有利的结果。实数传播器获得的结果与权氏提出的波数-频域获得的结果的比较[J. co Soc。上午。 128(4),1823-1832(2010)]显示了在从速度测量中向后传播压力的情况下使用实数形式的兴趣。风洞运动采用齐平安装的扬声器和非侵入式激光多普勒测速仪进行速度测量,从而证实了开发程序的效率。

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