The DSMC (Direct Simulation Monto-Carlo) computer code of a small nozzle vacuum plume was reformed.The computation showed that parallel computing could greatly accelerate computation
shorten computing time and enlarge computing scale.The parallel computation results accorded well with the sequential computation results.An example of DSMC parallel computation was also completed successfully for a vacuum plume and the computation results agreed well with theoretical analysis.The sequential computation won't be able to cope with this task.
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Related Author
CAO Si
LIU Bao-jie
HAN Shao-bing
ZHONG Jing-jun
YAN Hong-ming
REN Jun-xue
LIU Yu
LIAO Yun-fei
Related Institution
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics,School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
School of Energy Science and Engineering, Harbin Institute of Technology
Marine Engineering College, Dalian Maritime University
School of Astronautics, Beijing University of Aeronautics and Astronautics
Graduate University of Chinese Academy of Sciences