We present a new application of the nodal discontinuous Galerkin method in solving the lattice Boltzmann equation. By splitting the collision and the streaming operators of the lattice Boltzmann equation, the nodal discontinuous Galerkin method is implemented to solve the resulting advection equation. Space discretization is performed using unstructured grids with triangular elements, while time marching is carried out by applying the low-storage fourth-order, five-stage Runge-Kutta method. To validate the results, two well-known benchmark problems are simulated. The lid-driven square cavity at Reynolds numbers of 1000 and 5000 and Mach number of 0.1 and the impulsively started cylinder at Reynolds numbers of 550 and 9500 with Mach numbers of 0.1 and 0.05, respectively. The results show excellent agreement between the present study and the existing results in the literature. The method is then used to simulate flow in a porous medium. It is shown that the present method requires significantly lower number of grid points compared to the standard lattice Boltzmann method for the simulation of the porous medium flow. (C) 2014 Elsevier Ltd. All rights reserved.
机构:
Nanjing Univ Aeronaut & Astronaut, State Key Lab Mech & Control Mech Struct, Yudao St 29, Nanjing 210016, Jiangsu, Peoples R China
Nanjing Univ Aeronaut & Astronaut, Dept Aerodynam, Yudao St 29, Nanjing 210016, Jiangsu, Peoples R ChinaNanjing Univ Aeronaut & Astronaut, State Key Lab Mech & Control Mech Struct, Yudao St 29, Nanjing 210016, Jiangsu, Peoples R China
Wu, Jie
Shen, Meng
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Nanjing Univ Aeronaut & Astronaut, Dept Aerodynam, Yudao St 29, Nanjing 210016, Jiangsu, Peoples R ChinaNanjing Univ Aeronaut & Astronaut, State Key Lab Mech & Control Mech Struct, Yudao St 29, Nanjing 210016, Jiangsu, Peoples R China
Shen, Meng
Liu, Chen
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Nanjing Univ Aeronaut & Astronaut, Dept Aerodynam, Yudao St 29, Nanjing 210016, Jiangsu, Peoples R ChinaNanjing Univ Aeronaut & Astronaut, State Key Lab Mech & Control Mech Struct, Yudao St 29, Nanjing 210016, Jiangsu, Peoples R China
机构:
Xi An Jiao Tong Univ, Inst Turbomachinery, Xian 710049, Peoples R ChinaXi An Jiao Tong Univ, Inst Turbomachinery, Xian 710049, Peoples R China
Xia, Boyang
Li, Jun
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Xi An Jiao Tong Univ, Inst Turbomachinery, Xian 710049, Peoples R China
Collaborat Innovat Ctr Adv Aeroengine, Beijing 100191, Peoples R ChinaXi An Jiao Tong Univ, Inst Turbomachinery, Xian 710049, Peoples R China
机构:Zhejiang Univ, State Key Lab Fluid Power Transmiss & Control, Dept Mech, Hangzhou 310027, Peoples R China
Shi, X
Lin, JZ
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Zhejiang Univ, State Key Lab Fluid Power Transmiss & Control, Dept Mech, Hangzhou 310027, Peoples R ChinaZhejiang Univ, State Key Lab Fluid Power Transmiss & Control, Dept Mech, Hangzhou 310027, Peoples R China
Lin, JZ
Yu, ZS
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机构:Zhejiang Univ, State Key Lab Fluid Power Transmiss & Control, Dept Mech, Hangzhou 310027, Peoples R China
机构:
Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China
Chinese Acad Sci, Inst Mech, Ctr Interdisciplinary Res Fluids, Beijing 100190, Peoples R China
Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R ChinaKarlsruhe Inst Technol, Sci Comp Ctr, D-76344 Eggenstein Leopoldshafen, Germany