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Study of sound generated by large-scale structures in low speed coaxial jets

机译:研究低速同轴射流中大型结构产生的声音

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Sound generation by low speed circular and elliptic coaxial jets is investigated computationally. The secondary to primary jet velocity ratio is limited up to 0.4 and the elliptic jet profile has a 2:1 aspect ratio. Large Eddy Simulations are coupled with the Lighthill's acoustic analogy. Flow incompressibility is assumed limiting the study to the compact quadrupole structures generated during the jet mixing process. As expected, adding a secondary stream is found to extend the mixing region, while changing the jet geometry from circular to elliptic leads to vice versa. Good qualitative agreement in the flow behaviour is achieved with known results. Lighthill's longitudinal streamwise quadrupole is found to dominate the sound generation leading to a mildly high streamwise emission. Increasing the velocity ratio of the secondary stream to the primary stream increases the dominance of the streamwise sound emission. Good qualitative agreement with a previously suggested sound directivity pattern is achieved. Adding a secondary stream to the jet is found to have a mixed effect on the emitted acoustic power. A plausible explanation based on a large scale instability wave model is presented.
机译:通过计算研究了低速圆形和椭圆形同轴射流产生的声音。次级与初级射流速度之比最大限制为0.4,椭圆形射流轮廓的纵横比为2:1。大型涡流模拟与Lighthill的声学比拟相结合。假定流动不可压缩,将研究限制在喷射混合过程中产生的紧凑的四极结构上。如预期的那样,发现添加二次流可扩展混合区域,同时将射流的几何形状从圆形变为椭圆形,反之亦然。在流动性能方面取得了良好的定性一致性,并获得了已知的结果。发现Lighthill的纵向流向四极杆主导了声音的产生,导致了适度的高流向辐射。增加次要流与主要流的速度比会增加流向声音发射的优势。实现了与先前建议的声音指向性模式的良好定性一致性。发现向喷射流中添加二次流对发射的声功率产生混合影响。提出了基于大规模不稳定性波动模型的合理解释。

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