In this study, the lattice Boltzmann method, pseudospectral method, and artificial compressibility method were implemented on both CPU and GPU machines. Homogeneous isotropic turbulent flows were calculated using these three methods with the C language and CUDA library. The computational results show that the flow field obtained by the lattice Boltzmann method was almost the same as that obtained by the pseudospectral method. Among these three methods, the computational time of the lattice Boltzmann method on a GPU was the shortest of all calculations. Thus, the lattice Boltzmann method was well accelerated by CPUs. These results proved that the lattice Boltzmann method on a GPU has advantages of accuracy and computational speed. (C) 2012 Elsevier Ltd. All rights reserved.
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Tsukuba University of Technology, Amakubo, Tsukuba 305-8520, JapanTsukuba University of Technology, Amakubo, Tsukuba 305-8520, Japan
Tanno, I.
Hashimoto, T.
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Kinki University, Kowakae 3-4-1, Higashiosaka, Osaka 577-8502, JapanTsukuba University of Technology, Amakubo, Tsukuba 305-8520, Japan
Hashimoto, T.
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Yasuda, T.
Tanaka, Y.
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Toyo Tire and Rubber Co. Ltd., Fujinoki 2-2-13, Itami, Hyogo 644-0847, JapanTsukuba University of Technology, Amakubo, Tsukuba 305-8520, Japan
Tanaka, Y.
Morinishi, K.
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Kyoto Institute of Technology, Goshokaidocho Matsugasaki Sakyo-ku, Kyoto 606-8525, JapanTsukuba University of Technology, Amakubo, Tsukuba 305-8520, Japan
Morinishi, K.
Satofuka, N.
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Kyoto Institute of Technology, Goshokaidocho Matsugasaki Sakyo-ku, Kyoto 606-8525, JapanTsukuba University of Technology, Amakubo, Tsukuba 305-8520, Japan
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
Jiang, Lan
Gu, Xiangyu
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China Acad Launch Vehicle Technol, Nandahongmen St 1, Beijing 100076, Peoples R ChinaNanjing Univ Aeronaut & Astronaut, State Key Lab Mech & Control Mech Struct, Yudao St 29, Nanjing 210016, Jiangsu, Peoples R China
Gu, Xiangyu
Wu, Jie
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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 China
Nanjing Univ Aeronaut & Astronaut, Minist Ind & Informat Technol, Key Lab Unsteady Aerodynam & Flow Control, 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