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    题名: 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.
    关键词: Direct Simulation Monte Carlo (DSMC);hypersonic flow;rarefied;fore-body;shallow cavity
    日期: 2015-12-05
    上传时间: 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
    显示于类别:[航空太空工程學系暨研究所] 會議論文

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