Parallel Direct Simulation Monte Carlo (DSMC) Methods for Modeling Hypersonic Flow over a Fore-body with Shallow Cavity | |
---|---|
學年 | 104 |
學期 | 1 |
發表日期 | 2015-12-05 |
作品名稱 | Parallel Direct Simulation Monte Carlo (DSMC) Methods for Modeling Hypersonic Flow over a Fore-body with Shallow Cavity |
作品名稱(其他語言) | |
著者 | Lo, M. C; Su, Y. W; Tzeng, P. Y; Hung, C. C. |
作品所屬單位 | |
出版者 | |
會議名稱 | 2015 AASRC Conference |
會議地點 | Yunlin, Taiwan |
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. |
關鍵字 | Direct Simulation Monte Carlo (DSMC);hypersonic flow;rarefied;fore-body;shallow cavity |
語言 | en_US |
收錄於 | |
會議性質 | 國內 |
校內研討會地點 | 無 |
研討會時間 | 20151205~20151205 |
通訊作者 | |
國別 | TWN |
公開徵稿 | |
出版型式 | |
出處 | 02-13 |
相關連結 |
機構典藏連結 ( http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/114935 ) |