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Numerical Simulation of Aerodynamic Sound by the Finite Difference Lattice Boltzmann Method  

강호근 (경상대학교 기계항공공학부ㆍ해양산업연구소)
김은라 (전북대학교 토목공학과)
Publication Information
Journal of Ocean Engineering and Technology / v.18, no.2, 2004 , pp. 10-17 More about this Journal
Abstract
In this research, a numerical simulation for the acoustic sounds around a two-dimensional circular cylinder in a uniform flaw was developed, using the finite difference lattice Boltzmann model. We examine the boundary condition, which is determined by the distribution function concerning density, velocity, and internal energy at the boundary node. Pressure variation, due to the emission of the acoustic waves, is very small, but we can detect this periodic variation in the region far from the cylinder. Daple-like emission of acoustic waves is seen, and these waves travel with the speed of sound, and are synchronized with the frequency of the lift on the cylinder, due to the Karman vortex street. It is also apparent that the size of the sound pressure is proportional to the central distance to the circular cylinder. The lattice BGK model for compressible fluids is shown to be a powerful tool for the simulation of gas flaws.
Keywords
Aerodnamic Sound; Mach Number; Aeolian Tone; Finite Difference Lattice Boltzmann Method; BGK Model;
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Times Cited By KSCI : 2  (Citation Analysis)
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