Effect of Serrated Structures on Unsteady Flow and Noise Reduction in a Miniature Centrifugal Fan

被引:0
作者
Jiang, Peiran [1 ]
Cheng, Hao [1 ]
Chen, Han [1 ]
Liu, Yu [1 ]
机构
[1] Southern Univ Sci & Technol, Dept Mech & Aerosp Engn, Shenzhen 518055, Guangdong, Peoples R China
来源
30TH AIAA/CEAS AEROACOUSTICS CONFERENCE 2024 | 2024年
关键词
TONAL NOISE; AEROFOIL INTERACTION;
D O I
暂无
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
This study employs a combined approach of numerical simulation and experimental methods to investigate the flow and noise characteristics of miniature centrifugal fans used in portable electronic devices under free inflow conditions. It compares the effects of serrated structures located at the fan inlet and the blade tips on the flow field and aerodynamic noise. The study utilizes Large Eddy Simulation to capture the flow field within the fan accurately and measures the far-field noise spectrum and directivity. By integrating the pressure fluctuations on the fan blades and upper casing walls in the frequency domain, the research reveals the distribution of dipole sound sources and uses the Q-criterion to visualize the vortex structures inside the fan. The results uncover the flow and noise characteristics of the miniature centrifugal fan and analyze the impact of the serrated structures on these properties. It was found that tonal noise is primarily caused by concentrated intake at the inlet of such miniature centrifugal fans. The contribution of the vortex tongue to noise generation is minimal and predominantly contributes to low-frequency broadband noise. The comparative analysis shows that properly designed serrated structures at the inlet can effectively suppress the generation of BPF tonal noise and that appropriately designed serrated structures at the blade tops can effectively weaken broadband noise and alter the distribution of broadband pressure fluctuations on particular fan casing walls.
引用
收藏
页数:14
相关论文
共 29 条
[1]   Noise reduction mechanisms of sawtooth and combed-sawtooth trailing-edge serrations [J].
Avallone, F. ;
van der Velden, W. C. P. ;
Ragni, D. ;
Casalino, D. .
JOURNAL OF FLUID MECHANICS, 2018, 848 :560-591
[2]   An analytic solution for the noise generated by gust-aerofoil interaction for plates with serrated leading edges [J].
Ayton, Lorna J. ;
Kim, Jae Wook .
JOURNAL OF FLUID MECHANICS, 2018, 853 :515-536
[3]  
Ballesteros-Tajadura R., 2006, NUMERICAL CALCULATIO
[4]   Effect of inlet straighteners on centrifugal fan performance [J].
Bayomi, N. N. ;
Hafiz, A. Abdel ;
Osman, A. M. .
ENERGY CONVERSION AND MANAGEMENT, 2006, 47 (18-19) :3307-3318
[5]  
Biedermann T.M., 24 AIAACEAS AEROACOU, DOI [DOI 10.2514/6.2018-2956, 10.2514/6.2018-2956]
[6]  
Braun K., 2014, 1999 EUR WIND EN C, P180
[7]   Performance and mechanism of sinusoidal leading edge serrations for the reduction of turbulence-aerofoil interaction noise [J].
Chaitanya, P. ;
Joseph, P. ;
Narayanan, S. ;
Vanderwel, C. ;
Turner, J. ;
Kim, J. W. ;
Ganapathisubramani, B. .
JOURNAL OF FLUID MECHANICS, 2017, 818 :435-464
[8]  
Glegg S., 2017, Aeroacoustics of low Mach number flows: fundamentals, analysis, and measurement
[9]   The Measurement of Unsteady Surface Pressure Using a Remote Microphone Probe [J].
Guan, Yaoyi ;
Berntsen, Carl R. ;
Bilka, Michael J. ;
Morris, Scott C. .
JOVE-JOURNAL OF VISUALIZED EXPERIMENTS, 2016, (118)
[10]   Reduction of aerodynamic noise of single-inlet centrifugal fan with inclined volute tongue [J].
Hao, Wenyue ;
Wang, Jiajun ;
He, Ximing ;
Zhu, Zuchao ;
Wang, Zhengdao ;
Yang, Hui ;
Zhang, Wei ;
Wei, Yikun .
MEASUREMENT & CONTROL, 2020, 53 (7-8) :1376-1387