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Investigation of multi-lobed fighter jet noise sources using acoustical holography and partial field decomposition methods

机译:利用声全息和局部场分解方法研究多瓣战斗机噪声源

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Full-scale tactical aircraft noise exhibits multiple radiation lobes not seen in laboratory-scale jets. These lobes have different radiation directions yet appear to have similar, overlapping source regions. Near-field acoustical holography (NAH) source reconstructions, in conjunction with partial field decomposition (PFD) methods that produce physically meaningful partial fields, are used in the current work to investigate the nature of these radiation patterns. First, it is shown that the two main radiation lobes are highly incoherent, suggesting independent partial sources. Second, these lobes are isolated as mutually orthogonal partial fields. In this representation, the lobes seem to be generated by independent yet spatially coincident extended partial sources. Source comparisons are made between non-afterburner and afterburner engine powers to investigate whether afterburner combustion produces any sources that are fundamentally different from those of non-afterburner operations. The current results show no qualitative changes occur due to the addition of the afterburner thrust aside from minor variations in source distribution, level, and the nature of the overlap between the multiple lobes.
机译:全尺寸战术飞机噪声显示出实验室规模喷​​气机中看不到的多个辐射波瓣。这些波瓣具有不同的辐射方向,但似乎具有相似的重叠源区域。在当前工作中,近场声全息(NAH)源重构与产生物理上有意义的分场的分场分解(PFD)方法结合在一起,用于研究这些辐射方向图的性质。首先,表明两个主要辐射波瓣高度不相干,表明存在独立的部分辐射源。第二,将这些波瓣隔离为相互正交的子场。在此表示中,波瓣似乎是由独立但空间上重合的扩展部分源生成的。在非加力燃烧器和加力燃烧器发动机功率之间进行了源比较,以调查加力燃烧器燃烧是否产生与非加力燃烧操作根本不同的任何来源。目前的结果表明,除了源分布,水平和多个波瓣之间重叠部分的微小变化外,由于增加了加力推力,没有发生质的变化。

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