Please wait a minute...
J4  2013, Vol. 47 Issue (1): 131-138    DOI: 10.3785/j.issn.1008-973X.2013.01.019
    
Numerical simulation of cavity flow field and aeroacoustic
HAO Zong-rui1, WANG Le-qin2, ZHOU Zhong-hai1, WU Da-zhuan2
1. Institute of Oceanographic Instrument, Shandong Academy of Science, Qingdao 266001, China; 2. Institute of
Chemical Machinery and Process Equipment, Zhejiang University, Hangzhou 310027, China
Download:   PDF(0KB) HTML
Export: BibTeX | EndNote (RIS)      

Abstract  

 Linear Euler equations with source terms were adopted to correct the unsteady flow of cavity. The sound radiation and signals in the farfield were solved by Ffowcs WilliamsHawkings equation. The characteristics of acoustic field were obtained and so were the effects of the damping coefficient of truncated region and the position of integral control surface on sound signals. Results show that the sound generated by the formation and collapse of vortex pair in cavity is revealed to be of a rotating quadrupole. A truncated region was developed at upstream of the outflow in order to effectively control the "spurious waves" produced by vortical structures. The order of damping coefficient was set to be 104 in order to ensure good computational convergence rate. The sources should be surrounded by the control surfaces in order to ensure the integrity and accuracy of the obtained sound signals in the far field.



Published: 01 January 2013
CLC:  O 354  
Cite this article:

HAO Zong-rui, WANG Le-qin, ZHOU Zhong-hai, WU Da-zhuan. Numerical simulation of cavity flow field and aeroacoustic. J4, 2013, 47(1): 131-138.

URL:

http://www.zjujournals.com/eng/10.3785/j.issn.1008-973X.2013.01.019     OR     http://www.zjujournals.com/eng/Y2013/V47/I1/131


空腔流场及气动噪声数值模拟

采用带有源项的线性欧拉方程修正空腔流动的非定常流场,利用Ffowcs Williams-Hawkings方程对声源流场的声辐射及远场声信号进行求解,研究空腔辐射声场特性及阻尼截断区域中阻尼系数、控制面位置等参数对噪声信号的影响.计算结果表明,空腔内旋涡的形成和溃灭过程会引起声辐射,且具有四极子特性;在计算区域的边界处设置阻尼截断区域可以有效地控制旋涡撞击边界所产生的“假波”,为了保证较好的收敛速度,阻尼强度系数的量级为104;控制面应包围声源流场区域,以确保求解得到的远场声信号的完整性和准确性.

[1] LIGHTHILL M J. On sound generated aero-dynamically. I. general theory [J]. Proceedings of the Royal Society of London, 1952, 211(1107): 564-587.
[2] CURLE N. The influence of solid boundaries on aerodynamic sound [J]. Proceedings of the Royal Society of London, 1955, 213 (187): 505-514.
[3] FFCOWS W J E, HAWKINGS D L. Sound generation by turbulence and surface in arbitrary motion [J]. Philosophical Transactions of the Royal Society, 1969, 264(1151): 321-342.
[4] GOLDSTEIN M E. Unified approach to aerodynamic sound generation in the presence of sound boundaries [J]. Journal of the Acoustical Society of America, 1974, 56(1): 497-509.
[5] TERRACOL M, MANOHA E, HERRERO C, et al. Hybrid methods for airframe noise numerical prediction [J]. Theoretical and Computational Fluid Dynamics, 2005, 19(3): 197-227.
[6] BAILLYA C, BOGEYA C, GLOERFELTB X. Some useful hybrid approaches for predicting aerodynamic noise [J]. Computes Renders Technique, 2005, 333(9): 666-675.
[7] EWERT R, SCHRODERB W. On the simulation of trailing edge noise with a hybrid LES/APE method [J]. Journal of Sound and Vibration, 2004, 270(3): 509-524.
[8] BECHARA W, BAILLY C, LAFON P. Stochastic approach to noise modeling for free turbulent flows [J]. Journal of the Acoustical Society of America, 1994, 97(6): 3518-3531.
[9] MCMULLAN W A, POKORA C D, PAGE G J, et al. Large eddy simulation of a high Reynolds number subsonic turbulent jet for acoustic source capture [C]∥14th Aeroacoustics Conference. Vancouver: [s. n.], 2008.
[10] GLOERFELT X, BAILLY C, JUVE D. Direct computation of the noise radiated by a subsonic cavity flow and application of integral methods [J]. Journal of Sound and Vibration, 2003, 266(1): 119-146.
[11] LIOW Y S K, THOMPSON M C, HOURIGAN K. Sound generated by a pair of axisymmetric coaxial vortex rings [J]. AIAA Journal, 2005, 43(2): 326-336.
[12] WANG Z K, JAMBAZOV G D, LAI C H. Numerical simulation of flow-induced cavity noise in self-sustained oscillations [J]. Computing and Visualization in Science, 2007, 10(3): 123-134.
[13] ZHANG N, SHEN H, YAO H Z. Numerical simulation of cavity flow induced noise by LES and FWH acoustic analogy [J]. Journal of Hydrodynamics, 2010, 22(5): 242-247.
[14] HAIGERMOSER C. Application of an acoustic analogy to PIV data from rectangular cavity flows [J]. Experiments in Fluids, 2009, 47(1): 145-157.
[15] HOWE M S. Contributions to the theory of aerodynamic sound with application to excess jet noise and the theory of the flute [J]. Journal of Fluid Mechanics, 1975, 71(4): 625-673.
[16] KARAMCHETI K. Acoustic radiation from twodimensional rectangular cutouts in aerodynamic surfaces [R]. Washington D.C.: NACA, 1955: 133.

No related articles found!