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Aeroacoustic Simulations Using Compressible Lattice Boltzmann Method

Part of: Optics, electromagnetic theory - General

Published online by Cambridge University Press:  08 July 2016

Kai Li  and
Chengwen Zhong
Kai Li*
Affiliation:
National Key Laboratory of Science and Technology on Aerodynamic Design and Research, Northwestern Polytechnical University, Xi'an 710072, China
Chengwen Zhong*
Affiliation:
National Key Laboratory of Science and Technology on Aerodynamic Design and Research, Northwestern Polytechnical University, Xi'an 710072, China
*
*Corresponding author. Email:[email protected] (K. Li), [email protected] (C.W. Zhong)
*Corresponding author. Email:[email protected] (K. Li), [email protected] (C.W. Zhong)
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Abstract

This paper presents a lattice Boltzmann (LB) method based study aimed at numerical simulation of aeroacoustic phenomenon in flows around a symmetric obstacle. To simulate the compressible flow accurately, a potential energy double-distribution-function (DDF) lattice Boltzmann method is used over the entire computational domain from the near to far fields. The buffer zone and absorbing boundary condition is employed to eliminate the non-physical reflecting. Through the direct numerical simulation, the flow around a circular cylinder at Re=150, M=0.2 and the flow around a NACA0012 airfoil at Re=10000, M=0.8, α=0° are investigated. The generation and propagation of the sound produced by the vortex shedding are reappeared clearly. The obtained results increase our understanding of the characteristic features of the aeroacoustic sound.

Keywords

Lattice Boltzmann methodcompressible flowdouble-distribution-functiondirect numerical simulationaeroacoustics

MSC classification

Secondary: 78A48: Composite media; random media
Type
Research Article
Information
Advances in Applied Mathematics and Mechanics , Volume 8 , Issue 5 , October 2016 , pp. 795 - 809
Copyright
Copyright © Global-Science Press 2016 

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