A Hybrid Lattice Boltzmann Flux Solver for Simulation of Viscous Compressible Flows

被引:47
作者
Yang, L. M. [1 ,2 ]
Shu, C. [3 ]
Wu, J. [2 ]
机构
[1] China Aerodynam Res & Dev Ctr, State Key Lab Aerodynam, Mianyang 621000, Peoples R China
[2] Nanjing Univ Aeronaut & Astronaut, Dept Aerodynam, Coll Aerosp Engn, Yudao St, Nanjing 210016, Jiangsu, Peoples R China
[3] Natl Univ Singapore, Dept Mech Engn, 10 Kent Ridge Crescent, Singapore 119260, Singapore
关键词
Lattice Boltzmann flux solver; hybrid; 1D lattice Boltzmann model; switch function; NAVIER-STOKES EQUATIONS; KINETIC BGK SCHEME; UNSTRUCTURED GRIDS; MACH NUMBER; EULER; COMPUTATIONS; MESH;
D O I
10.4208/aamm.2015.m1172
中图分类号
O29 [应用数学];
学科分类号
070104 ;
摘要
In this paper, a hybrid lattice Boltzmann flux solver (LBFS) is proposed for simulation of viscous compressible flows. In the solver, the finite volume method is applied to solve the Navier-Stokes equations. Different from conventional Navier-Stokes solvers, in this work, the inviscid flux across the cell interface is evaluated by local reconstruction of solution using one-dimensional lattice Boltzmann model, while the viscous flux is still approximated by conventional smooth function approximation. The present work overcomes the two major drawbacks of existing LBFS [28-31], which is used for simulation of inviscid flows. The first one is its ability to simulate viscous flows by including evaluation of viscous flux. The second one is its ability to effectively capture both strong shock waves and thin boundary layers through introduction of a switch function for evaluation of inviscid flux, which takes a value close to zero in the boundary layer and one around the strong shock wave. Numerical experiments demonstrate that the present solver can accurately and effectively simulate hypersonic viscous flows.
引用
收藏
页码:887 / 910
页数:24
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