Generalized form of interpolation-supplemented lattice Boltzmann method for computational aeroacoustics

被引:0
|
作者
Liu W.-H. [1 ]
Chen R.-Q. [1 ,2 ]
Qiu R.-F. [1 ]
Lin W. [1 ]
You Y.-C. [1 ]
机构
[1] School of Aerospace Engineering, Xiamen University, Xiamen
[2] Key Laboratory of Aerodynamic Noise Control, China Aerodynamics Research and Development Center, Mianyang
关键词
Aeroacoustics; Cylinder noise; Generalized form of interpolation-supplemented lattice Boltzmann method; Lattice Boltzmann method; Non-uniform mesh;
D O I
10.3785/j.issn.1008-973X.2020.08.024
中图分类号
学科分类号
摘要
The generalized form of interpolation-supplemented lattice Boltzmann method (GILBM) was proposed for aeroacoustics simulation on non-uniform meshes. The correctness of GILBM code was validated by simulating the lid-driven cavity flow and the low Reynolds number cylinder flow. On this basis, this method was applied to simulate the Gaussian pulse propagation, acoustic periodic point sources and aerodynamic noise of two-dimensional cylinder flow. Results show that the propagation process of Gaussian pulse and acoustic periodic point sources can be well simulated on non-uniform meshes by GILBM, and the simulation results are in good agreement with the analytical solution. Also, the generation and propagation of the aerodynamic noise produced by the vortex shedding generated by a cylinder can be simulated on non-uniform body-fitted mesh by GILBM, and the sound pressure propagation in the near field and the far field can be well captured. The aerodynamic noise characteristics of flow around a cylinder show a dipole pattern. Results present a good agreement with the references, which confirms the correctness and the feasibility of GILBM in simulating sound propagation problems and aerodynamic noise on non-uniform meshes. Copyright ©2018 Journal of Zhejiang University (Engineering Science). All rights reserved.
引用
收藏
页码:1637 / 1644
页数:7
相关论文
共 21 条
  • [1] MARIE S, RICOT D, SAGAUT P., Comparison between lattice Boltzmann method and Navier-Stokes high order schemes for computational aeroacoustics, Journal of Computational Physics, 228, 4, pp. 1056-1070, (2009)
  • [2] KAM E W S, LEUNG R C K, SO R M C, Et al., A lattice Boltzmann method for computation of aeroacoustic interaction, International Journal of Modern Physics C, 18, 4, pp. 463-472, (2007)
  • [3] VIGGEN E M., The lattice Boltzmann methods with applications in acoustics, (2009)
  • [4] VIGGEN E M., Acoustic multipole sources for the lattice Boltzmann method, Physical Review E, 87, 2, (2013)
  • [5] WANG Yong, HE Ya-ling, LIU Ying-wen, Et al., Simulation on attenuation of sound waves with lattice-Boltzmann method, Journal of Xi'an Jiaotong University, 41, 1, pp. 5-8, (2007)
  • [6] SI Hai-qing, SHI Yan, WANG Bing, Et al., Computational aeroacoustics based on lattice Boltzmann method, Journal of Nanjing University of Aeronautics and Astronautics, 45, 5, pp. 616-620, (2013)
  • [7] SI H Q, WANG B, SHI Y, Et al., Aero-acoustics computations of square cylinder using the latticeBoltzmann method, Applied Mechanics and Materials, 444-445, pp. 400-405, (2014)
  • [8] SHAO Wei-dong, LI Jun, Study on the Galerkin Boltzmann method for computational aeroacoustics, Journal of Xi'an Jiaotong University, 50, 3, pp. 134-140, (2016)
  • [9] LI Kai, Study on the compressible lattice Boltzmann method, (2016)
  • [10] JIANG Mao-qiang, ZHANG Rui, LIU Zhao-hui, Direct forcing immersed boundary-lattice Boltzmann coupling method for solving fluid structure interaction with complex boundary, Journal of Engineering Thermophysics, 39, 12, pp. 139-144, (2018)