Numerical Simulation of Two-Dimensional Bluff Body Aerodynamic Noise Using Lattice Boltzmann Method

Article Preview

Abstract:

Aerodynamic noise generated by air-moving devices is a common problem. In this paper, the aerodynamic noise around two-dimensional bluff body flow was simulated by Lattice Boltzmann Method. Utilizing blend radius can reduce the aerodynamic noise around the bluff body notably, and the greater the blend radius, the better the noise reduction effect will be. When the basic shape model is simulated and post-processed, the speed nephogram and the streamline chart of the flow field were obtained. Then Sound Pressure Level (SPL) of some key points was tested. Changing the shape of the bluff body’s vertices to blend radius, the results were compared with those of the basic shape, and the aerodynamic noise was reduced.

You might also be interested in these eBooks

Info:

Periodical:

Advanced Materials Research (Volumes 610-613)

Pages:

2535-2538

Citation:

Online since:

December 2012

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2013 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] Hucho W-H, Sovran G. Aerodynamics of road vehicles[J]. Annual Review of Fluid Mechanics, 1993, 25: 485-485.

DOI: 10.1146/annurev.fl.25.010193.002413

Google Scholar

[2] Yang S. Z, Y Z Z, and A C. Simulation of the flow past two dimensional bluff bodies using deterministic vortex method[J]. Acta Aerodynamica Sinica 2008, 26(04): 526-531.

Google Scholar

[3] F. X Y, T. H Y, C. T Y, et al. Aerodynamic Noise and Modal Analysis of Round Jet Based on the Finite Element Method[J]. Journal of Engineering Thermophysics, 2011, 32(12): 2052-2055.

Google Scholar

[4] He Y, Li Q, Wang Y, et al. Lattice Boltzmann method and its applications in engineering thermophysics[J]. Chinese Science Bulletin, 2009, 54(22): 4117-4134.

DOI: 10.1007/s11434-009-0681-6

Google Scholar

[5] Marié S, Ricot D, and Sagaut P. Comparison between lattice Boltzmann method and Navier–Stokes high order schemes for computational aeroacoustics[J]. Journal of Computational Physics, 2009, 228(4): 1056-1070.

DOI: 10.1016/j.jcp.2008.10.021

Google Scholar

[6] Hiraishi M, Tsutahara M, and Leung R C K. Numerical simulation of sound generation in a mixing layer by the finite difference lattice Boltzmann method[J]. Computers & Mathematics with Applications, 2010, 59(7): 2403-2410.

DOI: 10.1016/j.camwa.2009.08.073

Google Scholar

[7] Hasert M, Bernsdorf J, and Roller S. Towards aeroacoustic sound generation by flow through porous media[J]. Philosophical Transactions of the Royal Society a-Mathematical Physical and Engineering Sciences, 2011, 369(1945): 2467-2475.

DOI: 10.1098/rsta.2011.0089

Google Scholar