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Jet Noise Source Location by Acoustic Beamforming and Nearfield Sound Contours - A Comparison

机译:通过声束成形和近场声波轮廓定位喷气噪声源-比较

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The knowledge of the distribution of sources of noise for various frequencies in a jet are often needed to understand the jet noise mechanisms and to predict and control jet noise. This knowledge can also be very helpful for extrapolating nearfield noise to the farfield and vice versa. Many techniques have been developed over the years to measure jet noise source locations; however, most of them are extremely time consuming and rather cumbersome. The more recently developed acoustic beamforming technique is quite rapid, but its performance against older techniques has never been examined. This study attempts to do precisely that by acquiring source location data for the same jet, first by the beamforming methodology and then via the well-established nearfield contour method. Both methods are employed to obtain source locations of a small one-inch exit diameter conical jet for subsonic conditions, and it is shown that both methods provide similar results. Additional confirmation is obtained on jets with unmodified and tabbed exit conditions.
机译:通常需要了解喷气机中各种频率的噪声源的分布,以了解喷气机的噪声机理以及预测和控制喷气机的噪声。该知识对于将近场噪声外推到远场,反之亦然也非常有帮助。多年来,已经开发出许多技术来测量喷射噪声源的位置。然而,它们中的大多数非常耗时并且相当麻烦。较新开发的声束成形技术相当快,但是从未检验过它相对于较旧技术的性能。这项研究试图通过获取相同射流的源位置数据来精确地做到这一点,首先是通过波束成形方法,然后是通过公认的近场轮廓法。两种方法都用于获得亚音速条件下小的一英寸出口直径圆锥形射流的震源位置,并且表明两种方法都提供了相似的结果。对于未经修改的选项卡式出口条件的喷气机,可获得更多确认。

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