Groupe d'Acoustique de l'Université de Sherbrooke, Université de Sherbrooke, Sherbrooke J1K 2R1, Canada.
J Acoust Soc Am. 2012 Feb;131(2):1226-39. doi: 10.1121/1.3675942.
This article discusses an open-loop wave field synthesis (WFS) approach for the reproduction of spatially correlated sound fields. The main application concerns laboratory reproduction of turbulent boundary layer wall pressure on aircraft fuselages and measurement of their sound transmission loss. The problem configuration involves reconstruction of random sound pressure distributions on a planar reproduction surface using a planar array of reproduction monopoles parallel to the reproduction plane. In this paper, the WFS formulation is extended to sound fields with imposed time and spatial correlation properties (or equivalently imposed cross-spectral density in the frequency and wave number domains). Numerical examples are presented for the reproduction of a propagating plane wave, diffuse acoustic field and wall pressure in subsonic or supersonic turbulent boundary layers. The reproduction accuracy is examined in terms of the size of the source plane and reproduction plane, their separation, and the number of reproduction sources required per acoustic wavelength. While the reproduction approach cannot reconstruct sub-wavelength correlation scales of subsonic turbulent boundary layers, it effectively reconstructs correlation scales larger than the acoustic wavelength, making it appropriate for diffuse acoustic field and supersonic turbulent layers.
本文讨论了一种用于再现空间相关声场的开环波场合成(WFS)方法。主要应用涉及在实验室中再现飞机机身的湍流边界层壁压,并测量它们的隔声量。问题配置涉及使用与再现平面平行的再现单极子平面阵列在再现平面上再现随机声压分布。在本文中,WFS 公式被扩展到具有时间和空间相关特性的声场(或者等效地在频率和波数域中具有规定的互谱密度)。给出了用于再现传播平面波、扩散声场和亚声速或超声速湍流边界层壁压的数值示例。再现精度是根据声源平面和再现平面的大小、它们的分离以及每个声波长所需的再现源的数量来检查的。虽然再现方法不能重建亚声速湍流边界层的亚波长相关尺度,但它有效地重建了大于声波波长的相关尺度,因此适用于扩散声场和超声速湍流层。