Numerical investigation of aeroacoustics damping performance of a Helmholtz resonator: Effects of geometry, grazing and bias flow

被引:60
作者
Wu, Gang [1 ,2 ]
Lu, Zhengli [3 ]
Xu, Xiao [3 ]
Pan, Weichen [3 ]
Wu, Weiwei [3 ]
Li, Jun [3 ]
Ci, J. [4 ]
机构
[1] Changsha Univ Sci & Technol, Coll Automot & Mech Engn, Changsha 410114, Hunan, Peoples R China
[2] Changsha Univ Sci & Technol, Key Lab Lightweight & Reliabil Technol Engn Vehic, Changsha 410114, Hunan, Peoples R China
[3] Jiangsu Univ Sci & Technol, Sch Energy & Power Engn, Mengxi Rd 2, Zhenjiang 212003, Jiangsu, Peoples R China
[4] Nanyang Technol Univ, Coll Engn, 50 Nanyang Ave, Singapore 639798, Singapore
基金
新加坡国家研究基金会; 中国国家自然科学基金;
关键词
MICRO-CYLINDRICAL COMBUSTOR; TUNED PASSIVE CONTROL; N-BUTANOL-ETHANOL; SOUND-ABSORPTION; EXCITED RESONANCE; FLUID-DYNAMICS; FUEL CANDIDATE; DEEP CAVITY; FREQUENCY; INSTABILITIES;
D O I
10.1016/j.ast.2019.01.007
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In this work, the effects of the grazing flow and its geometric dimensions on the aeroacoustics damping performance of a Helmholtz resonator are numerically evaluated. The grazing flow tangentially passing through the neck of the resonator is characterized by Mach number. And it is varied from 0 to 0.1. 2D numerical simulations are conducted by solving linearized Navier-Stokes equations in frequency domain via COMSOL 5.3. The numerical model is first validated by comparing with experimental and theoretical data available in literature, as a low Mach number grazing flow is present only. Good agreement is obtained. The model is then used to examine the effect of the grazing flow and the resonator geometric dimensions on transmission loss (TL) performance. Four key parameters are identified, and they include 1) the neck length, 2) neck diameter, 3) cavity volume and 4) the grazing flow Mach number. It is found that as the grazing flow Mach number is greater than 0.07, increasing the neck length leads to a decreased TLmax. Same observation is found for increased cavity volume V-r. Smaller Helmholtz resonator V-r or shorter neck length L-n is found to be involved with a larger TLmax in the presence of the grazing flow. Further study is then conducted, when there is a joint bias-grazing flow. The bias flow could be injected with respect to the grazing flow in 3 different directions, 1) parallel, 2) perpendicular and 3) counter flow. The bias flow injection direction is found to lead to 5 dB transmission loss difference. Parallel or counter injection of the bias flow is showed to be associated with improved n. performance, since there are counter-rotating vortices produced in the cavity. Finally, increasing the Mach number of the grazing flow leads to the noise damping effectiveness being deteriorated in general, even in the presence of a bias flow. The present work shed lights on the aeroacoustics design of Helmholtz resonators in the presence of a grazing and bias flow. (C) 2019 Elsevier Masson SAS. All rights reserved.
引用
收藏
页码:191 / 203
页数:13
相关论文
共 64 条
[1]  
Adobes A., 1990, Journal of Low Frequency Noise & Vibration, V9, P92
[2]   SOUND-ABSORPTION CAUSED BY VORTICITY SHEDDING, DEMONSTRATED WITH A JET FLOW [J].
BECHERT, DW .
JOURNAL OF SOUND AND VIBRATION, 1980, 70 (03) :389-405
[3]  
Bellucci V., 2001, ASME TURBO EXPO 2001
[4]   Scattering and absorption of sound at flow duct expansions [J].
Boij, S ;
Nilsson, B .
JOURNAL OF SOUND AND VIBRATION, 2006, 289 (03) :577-594
[5]   Acoustic performance of different Helmholtz resonator array configurations [J].
Cai, Chenzhi ;
Mak, Cheuk Ming .
APPLIED ACOUSTICS, 2018, 130 :204-209
[6]   Effects of geometry on the resonance frequency of Helmholtz resonators .2. [J].
Chanaud, RC .
JOURNAL OF SOUND AND VIBRATION, 1997, 204 (05) :829-834
[7]   EFFECTS OF GEOMETRY ON THE RESONANCE FREQUENCY OF HELMHOLTZ RESONATORS [J].
CHANAUD, RC .
JOURNAL OF SOUND AND VIBRATION, 1994, 178 (03) :337-348
[8]   Acoustical Treatment of Multi-Tone Broadband Noise with Hybrid Side-Branched Mufflers Using a Simulated Annealing Method [J].
Chiu, Min-Chie .
JOURNAL OF LOW FREQUENCY NOISE VIBRATION AND ACTIVE CONTROL, 2014, 33 (01) :79-111
[9]   ACOUSTIC NONLINEARITIES AND POWER LOSSES AT ORIFICES [J].
CUMMINGS, A .
AIAA JOURNAL, 1984, 22 (06) :786-792
[10]   A simple method for the analysis of deep cavity and long neck acoustic resonators [J].
Doria, A .
JOURNAL OF SOUND AND VIBRATION, 2000, 232 (04) :823-833