| Literature DB >> 23526050 |
Abstract
The Lattice Boltzmann Method (LBM) is a well established computational tool for fluid flow simulations. This method has been recently utilized for low Mach number computational aeroacoustics. Robust and nonreflective boundary conditions, similar to those used in Navier-Stokes solvers, are needed for LBM-based aeroacoustics simulations. The goal of the present study was to develop an absorbing boundary condition based on the perfectly matched layer (PML) concept for LBM. The derivation of formulations for both two and three dimensional problems are presented. The macroscopic behavior of the new formulation is discussed. The new formulation was tested using benchmark acoustic problems. The perfectly matched layer concept appears to be very well suited for LBM, and yielded very low acoustic reflection factor.Entities:
Keywords: computational aeroacoustics; lattice Boltzmann method; non-reflective boundary conditions
Year: 2012 PMID: 23526050 PMCID: PMC3601760 DOI: 10.1016/j.compfluid.2012.07.017
Source DB: PubMed Journal: Comput Fluids ISSN: 0045-7930 Impact factor: 3.013