Influence Due to the Blade Number on the Stator Tonal and Broadband Noise

被引:0
作者
Xingyu Wu
Yingsan Wei
Shuanbao Jin
Dong Wang
Hao Zhu
Pengfei Hu
Fangxu Sun
机构
[1] Naval University of Engineering,National Key Laboratory of Science and Technology on Vessel Integrated Power System, Research Institute of Special Electrical Science and Technology
来源
Acoustics Australia | 2021年 / 49卷
关键词
Turbulence; Rotor wake; Broadband noise; Tonal noise; Sound power level;
D O I
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中图分类号
学科分类号
摘要
The cascade’s response function can be used to effectively deal with the unsteady response of the interaction between the harmonic turbulence and the cascades. Based on this function, this paper presents the formulas for the stator broadband and tonal noises, whose inflow models are different from each other. The broadband noise comes from the impact of the random turbulence wave in the rotor wake on the stator, while the tonal noise comes from the interaction between the periodic rotor wake and the stator. According to the formulas for predicating the two kinds of noise, their inflow models are different from each other. Comparing with the test models of subsonic fan, the prediction models of the broadband and tonal noise prove to be correct. Meanwhile, the influence of the blade number on stator tonal and broadband noise is carried out through the prediction models, and the results are summarized that (1) the greater the number of blades, the higher the broadband sound power level of the stator in the high frequency. (2) An increase in the number of blades can “cut off” the tonal noise of the stator at BPF. So, reasonable arrangement of the number of stator and rotor blades is significant to the passive suppression of stator noise.
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页码:345 / 353
页数:8
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共 33 条
  • [1] Farassat F(2012)Broadband noise prediction when turbulence simulation is available—derivation of formulation 2b and its statistical analysis J. Sound Vib. 331 2203-2208
  • [2] Casper J(2015)Predictions of fan broadband noise using lifting surface method AIAA J. 53 2845-2855
  • [3] Zhang W(1970)Lifting surface theory for the problem of an arbitrarily yawed sinusoidal gust incident on a thin aerofoil in incompressible flow Aeronaut. Q. 21 182-198
  • [4] Wang X(2010)Turbulent wind flow over a low hill Q. J. R. Meteorol. Soc. 101 929-955
  • [5] Sun X(1974)Sound radiation from a subsonic rotor subjected to turbulence Fluid Mech. Acoust. Des. Turbomach. 1 493-512
  • [6] Graham JMR(1977)Three-dimensional analysis of blade force and sound generation for an annular cascade in distorted flows J. Sound Vib. 50 479-508
  • [7] Jackson PS(1998)Experimental validation of lifting surface theory for rotor-stator interaction noise generation AIAA J. 36 900-906
  • [8] Hunt JCR(2000)Experiments on radiated noise and vibration from a lifting surface at high reynolds numbers J. Acoust. Soc.Am. 107 2825-11
  • [9] Sevik M(2015)Predictions of fan broadband noise using lifting surface method AIAA J. 53 1-83
  • [10] Namba M(1970)Sound transmission through blade rows J. Sound Vib. 12 59-64