Experimental and numerical analysis on tonal noise of single-stage axial compressor

被引:0
|
作者
Chen C. [1 ]
Wang Y. [2 ]
Shu W. [1 ]
Du L. [2 ]
Sun X. [1 ,2 ]
机构
[1] School of Energy and Power Engineering, Beihang University, Beijing
[2] Research Institute of Aero-Engine, Beihang University, Beijing
来源
关键词
compressor; noise prediction; rotor-stator interaction; tonal noise; unsteady pressure fluctuation;
D O I
10.13224/j.cnki.jasp.20220903
中图分类号
学科分类号
摘要
To investigate the correlation between the tonal noise generated by rotor/stator interaction and the incoming upwash velocity of the stator, the tonal noise of a single-stage, low-speed axial compressor test rig (TA36) in a throttling process was studied by a well-developed inhouse hybrid noise prediction method. In order to accurately capture the source of the tonal noise, i.e., unsteady pressure fluctuation on the surface of the stator blade,the effects of the simulation grid and time-step size on the prediction of the unsteady pressure fluctuation were discussed firstly. Then, the variations of upwash velocity and tonal noise in the throttling process were compared. The result showed that at the third blade passing frequency (BPF) of the design speed,the amplitude variation of the incoming upwash velocity on the 70%,80%,and 90% span of the stator was consistent with the sound pressure level predicted by the hybrid method, and kept good consistency with the experimental measurements. In addition, the sound radiation in the far field demonstrated significant directivity while the directivity did not change significantly with the mass flow rate. © 2023 BUAA Press. All rights reserved.
引用
收藏
页码:1239 / 1249
页数:10
相关论文
共 28 条
  • [21] LI Zhibin, WANG Xiaoyu, SUN Xiaofeng, Et al., Experimental research on noise of single-stage low-speed axial compressor, Journal of Propulsion Technology, 39, 6, pp. 1275-1282, (2018)
  • [22] WANG Liangfeng, XIANG Kangshen, MAO Luqin, Et al., Numerical simulation of the effect of the tip clearance flow on rotor-stator interaction tone noise in axial-flow fan, Proceedings of the ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition, pp. 1-10, (2020)
  • [23] LU Huabing, XIAO Youhong, LIU Zhigang, Et al., Simulation and experimental research on aerodynamic noise of gas turbine 1.5-stage axial compressor, Applied Acoustics, 192, (2022)
  • [24] GOLDSTEIN M E., Aeroacoustics, (1976)
  • [25] YANG Bing, WANG T Q., Investigation of the influence of liner hard-splices on duct radiation/propagation and mode scattering, Journal of Sound and Vibration, 315, 4-5, pp. 1016-1034, (2008)
  • [26] DUNN M H., TBIEM3D: a computer program for predicting ducted fan engine noise, (1997)
  • [27] ZHANG Weiguang, WANG Xiaoyu, JING Xiaodong, Et al., Three-dimensional analysis of vane sweep effects on fan interaction noise [J], Journal of Sound and Vibration, 391, pp. 73-94, (2017)
  • [28] CFX-solver modeling guide release 15.0, (2013)