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    請使用永久網址來引用或連結此文件: http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/114935

    題名: Parallel Direct Simulation Monte Carlo (DSMC) Methods for Modeling Hypersonic Flow over a Fore-body with Shallow Cavity
    作者: Lo, M. C;Su, Y. W;Tzeng, P. Y;Hung, C. C.
    關鍵詞: Direct Simulation Monte Carlo (DSMC);hypersonic flow;rarefied;fore-body;shallow cavity
    日期: 2015-12-05
    上傳時間: 2018-09-18 12:11:38 (UTC+8)
    摘要: In this study, the improved parallel Direct Simulation Monte Carlo (DSMC) method is adopted to implement the three dimensional computations of the shallow cavity flow field with hypersonic and rarefied conditions. In order to effectively accelerate the overall computational efficiency, a parallel direct simulation Monte Carlo code based on the C++ language, named PDSC++, using object-oriented programming is employed.
    關聯: 02-13
    顯示於類別:[航空太空工程學系暨研究所] 會議論文


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