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Acoustic characteristics of jets emanating from curved triangular topologies

机译:弯曲三角形拓扑结构产生的射流的声学特性

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Noise generated from two geometrically contrasting jet flow topologies - concave and convex triangular jets are considered in the present work. Jets are generated from disk-nozzles made by cutting out the requisite concave/convex geometries on thin plates. The areas as well as the radii of curvature of concave and convex jets are maintained the same. Acoustic characteristics of the curved jets are measured and compared with those of a regular equilateral triangular jet. Experiments are conducted for underexpanded conditions for pressure ratios ranging from 2 to 7, corresponding to fully expanded jet Mach numbers of 1.04 ≤ M_j ≤ 1.92. Acoustic characterization has been carried out in terms of overall sound pressure levels, spectra, and directivity. The results show that mid-edge planes are noisier than vertex planes. The initial jet perimeter is found to be a key parameter influencing the noise emission of curved jets. Along the mid-edge planes, the concave jet is the noisiest, followed by regular equilateral triangular jet and then by the convex triangular jet. Curvature brings about a reduction in the shock-cell length - the equilateral triangular jet has the highest shock cell length followed by the convex and concave triangular jets.
机译:在当前的工作中,考虑了由两种几何形状不同的射流拓扑产生的噪声-凹形和凸形三角形射流。通过在薄板上切出必要的凹凸几何形状制成的圆盘喷嘴产生喷射流。凹射流和凸射流的面积以及曲率半径保持相同。测量弯曲射流的声学特性,并将其与规则的等边三角形射流的声学特性进行比较。在压力比为2到7的不足膨胀条件下进行实验,对应于1.04≤M_j≤1.92的完全膨胀射流马赫数。已经根据整体声压级,频谱和方向性进行了声学表征。结果表明,中边缘平面比顶点平面噪声更大。发现初始射流周长是影响弯曲射流噪声排放的关键参数。沿着中边缘平面,凹射流是最嘈杂的,其次是规则的等边三角形射流,然后是凸三角形射流。曲率使激波单元长度减小-等边三角形射流具有最高的激波单元长度,其后是凸和凹三角形射流。

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