An improved CESE method and its application to steady-state coronal structure simulation
文献类型:期刊论文
作者 | Zhou YuFen; Feng XueShang |
刊名 | SCIENCE CHINA-EARTH SCIENCES
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出版日期 | 2014 |
卷号 | 57期号:1页码:153-166 |
关键词 | improved CESE scheme numerical dissipation steady-state coronal structure |
ISSN号 | 1674-7313 |
通讯作者 | Zhou, YF (reprint author), Chinese Acad Sci, SIGMA Weather Grp, Ctr Space Sci & Appl Res, State Key Lab Space Weather, Beijing 100190, Peoples R China. |
英文摘要 | This paper presents an improved space-time conservation element and solution element (CESE) method by applying a non-staggered space-time mesh system and simply improving the calculation of flow variables and applies it to magnetohydrodynamics (MHD) equations. The improved CESE method can improve the solution quality even with a large disparity in the Courant number (CFL) when using a fixed global marching time. Moreover, for a small CFL (say < 0.1), the method can significantly reduce the numerical dissipation and retain the solution quality, which are verified by two benchmark problems. And meanwhile, comparison with the original CESE scheme shows better resolution of the improved scheme results. Finally, we demonstrate its validation through the application of this method in three-dimensional coronal dynamical structure with dipole magnetic fields and measured solar surface magnetic fields as the initial input. |
学科主题 | 空间物理 |
收录类别 | SCI |
语种 | 英语 |
源URL | [http://ir.cssar.ac.cn/handle/122/1508] ![]() |
专题 | 国家空间科学中心_空间科学部 |
推荐引用方式 GB/T 7714 | Zhou YuFen,Feng XueShang. An improved CESE method and its application to steady-state coronal structure simulation[J]. SCIENCE CHINA-EARTH SCIENCES,2014,57(1):153-166. |
APA | Zhou YuFen,&Feng XueShang.(2014).An improved CESE method and its application to steady-state coronal structure simulation.SCIENCE CHINA-EARTH SCIENCES,57(1),153-166. |
MLA | Zhou YuFen,et al."An improved CESE method and its application to steady-state coronal structure simulation".SCIENCE CHINA-EARTH SCIENCES 57.1(2014):153-166. |
入库方式: OAI收割
来源:国家空间科学中心
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