于水望, 杜永乐, 蔡晋生. 矩形喷管出口宽高比对流场与声场的影响[J]. 实验流体力学, 2024, 38(1): 1-12. DOI: 10.11729/syltlx20230063
引用本文: 于水望, 杜永乐, 蔡晋生. 矩形喷管出口宽高比对流场与声场的影响[J]. 实验流体力学, 2024, 38(1): 1-12. DOI: 10.11729/syltlx20230063
YU S W, DU Y L, CAI J S. Effect of rectangular nozzle exit aspect ratioon flow field and acoustic field[J]. Journal of Experiments in Fluid Mechanics, 2024, 38(1): 1-12. DOI: 10.11729/syltlx20230063
Citation: YU S W, DU Y L, CAI J S. Effect of rectangular nozzle exit aspect ratioon flow field and acoustic field[J]. Journal of Experiments in Fluid Mechanics, 2024, 38(1): 1-12. DOI: 10.11729/syltlx20230063

矩形喷管出口宽高比对流场与声场的影响

Effect of rectangular nozzle exit aspect ratioon flow field and acoustic field

  • 摘要: 为探究矩形喷管出口宽高比对喷流流场和声场的影响规律,采用DES/FW–H混合算法对出口宽高比为3和1.5的矩形喷管超声速完全膨胀喷流开展研究,分析出口宽高比对喷流流动与噪声的影响。针对多个流场变量进行对比分析,以验证数值模拟方法的可行性,发现喷管出口宽高比不同,靠近出口内壁面上的压力变化也有所不同:喷管出口宽高比越大,压力变化越快。结合已有噪声实验数据和计算数据,验证了噪声模拟的准确性。对不同出口宽高比下剪切层厚度的变化进行了分析,研究了这种变化对喷流噪声的影响,发现随着宽高比增大,剪切层厚度增大,且剪切层快速扩张位置和高频噪声源位置向上游方向移动。对比了不同宽高比下出口唇线上特定频率噪声的相速度,研究发现:喷管宽高比不同,同样频率的近场噪声有着不同的相速度,这决定了近场噪声向下游传播的最大角度;相速度对应的马赫角越大,近场噪声向下游传播的最大角度越大;宽高比增大,长轴唇线上的相速度显著降低,近场噪声向下游的辐射角度减小。

     

    Abstract: To investigate the influence of the aspect ratio on the flow field and acoustic field of a rectangular nozzle, study has been conducted using DES/FW–H hybrid algorithm on two different aspect ratios of rectangular supersonic fully expanded jet nozzles. The influence of the aspect ratio on flow dynamics and noise of the jet has been analyzed. Firstly, multiple flow field variables were compared and analyzed to verify the feasibility of numerical simulation methods. Differences were observed in the pressure changes on the inner wall surface near the outlet for different aspect ratios, with the larger aspect ratio exhibiting faster pressure changes. Also, it was found that the velocity decreases more rapidly with distance from the outlet on the short axis of the lip, while on the long axis of the lip, the velocity decreases slowly. Next, relating the aspect ratio of the nozzle exit to the jet noise field, and comparing existing noise experimental data with computed data, it was found that in all angles, the maximum difference between the experimental and computed total sound pressure level was 2.6 dB (AR = 3) and 4 dB (AR = 1.5). Increasing the aspect ratio could reduce the total sound pressure level upstream. Furthermore, changes in the shear layer thickness under different aspect ratios were analyzed, and the impact of these changes on the jet noise was studied. The results reveal that increasing the aspect ratio would increase the shear layer thickness and shift the rapid expansion location of the shear layer and high-frequency noise sources upstream. Finally, the phase velocities of specific frequency noise at the lip of the exit were compared for different aspect ratios, revealing a significant reduction in the phase velocity along the long axis of the exit lip with increasing aspect ratio, which affects the angle of the near-field noise radiation.

     

/

返回文章
返回