An Adaptive Mesh Refinement-Rotated Lattice Boltzmann Flux Solver for Numerical Simulation of Two and Three-Dimensional Compressible Flows with Complex Shock Structures

被引:1
|
作者
Huang, Xiaoyingjie [1 ]
Chen, Jiabao [1 ,2 ]
Zhang, Jun [3 ]
Wang, Long [1 ,4 ]
Wang, Yan [1 ,2 ,4 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Coll Aerosp Engn, 29 Yudao St, Nanjing 210016, Peoples R China
[2] Nanjing Univ Aeronaut & Astronaut, State Key Lab Mech & Control Mech Struct, Yudao St 29, Nanjing 210016, Peoples R China
[3] Chengdu Fluid Dynam Innovat Ctr, 75 West Second Ring Rd, Chengdu 610072, Peoples R China
[4] Nanjing Univ Aeronaut & Astronaut, Jiangsu Key Lab Hitech Res Wind Turbine Design, Yudao St 29, Nanjing 210016, Peoples R China
来源
SYMMETRY-BASEL | 2023年 / 15卷 / 10期
基金
中国国家自然科学基金;
关键词
lattice Boltzmann flux solver; adaptive mesh refinement; compressible flow; shock instability; 2-DIMENSIONAL RIEMANN PROBLEMS; GAS-DYNAMICS; WAVE-PROPAGATION; CARBUNCLE-FREE; MODEL; SCHEME;
D O I
10.3390/sym15101909
中图分类号
O [数理科学和化学]; P [天文学、地球科学]; Q [生物科学]; N [自然科学总论];
学科分类号
07 ; 0710 ; 09 ;
摘要
An adaptive mesh refinement-rotated lattice Boltzmann flux solver (AMR-RLBFS) is presented to simulate two and three-dimensional compressible flows with complex shock structures. In the method, the RLBFS, which has a strong shock-capturing capability and can effectively eliminate the shock instability phenomenon, is applied to solve the flow filed by reconstructing the fluxes at each cell interface adaptively with the mesoscopic lattice Boltzmann model. To locally and dynamically improve the resolution of intricate shock structures and optimize the required computational resources, a block-structured adaptive mesh refinement (AMR) technique is introduced. The validity and effectiveness of the proposed method are confirmed through a range of two and three-dimensional numerical cases, including the shock tube problem, the four-wave Riemann problem, explosion within a rectangular box, and the vorticity induced by a shock. The results obtained using the AMR-RLBFS exhibit excellent agreement with published data and demonstrate high accuracy in capturing complex shock structures. The computational efficiency of the AMR-RLBFS can be also improved significantly compared to the RLBFS on uniform grids. Furthermore, the numerical outcomes underscore the capability of the AMR-RLBFS to eliminate shock instability effects while efficiently capturing a broader spectrum of small-scale vertical structures. These findings highlight the ability of AMR-RLBFS to improve the computational efficiency and capture intricate shock structures effectively, making it a valuable tool for studying a wide range of compressible flows from aerodynamics to astrophysics.
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