中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Numerical analysis of supersonic jet flow and dust transport induced by air ingress in a fusion reactor

文献类型:期刊论文

作者Wang, Bu-Er1,2; Zhang, Shi-Chao2; Wang, Zhen2; Jia, Jiang-Tao2; Chen, Zhi-Bin2
刊名NUCLEAR SCIENCE AND TECHNIQUES
出版日期2021-07-01
卷号32
关键词Supersonic jet Radioactive dust Loss of vacuum accident Mach disk Friction velocity
ISSN号1001-8042
DOI10.1007/s41365-021-00912-z
通讯作者Zhang, Shi-Chao(shichao.zhang@inest.cas.cn) ; Wang, Zhen(zhen.wang@inest.cas.cn)
英文摘要During a loss of vacuum accident (LOVA), the air ingress into a vacuum vessel (VV) may lead to radioactive dust resuspension, migration, and even explosion, thereby posing a great threat to the safe operation of future fusion reactors; thus, it is crucial to understand the flow characteristics and radioactive dust transport behavior induced by LOVA. However, only a few studies have identified the characteristics of the highly under-expanded jet flow at a scale of milliseconds during LOVA. Particularly, the occurrence and behavior of a Mach disk is yet to be captured in existing studies. In this study, we used a more advanced model with a finer mesh and adaptive mesh strategies to capture the Mach disk in a VV during LOVA. In detail, a computational fluid dynamics-discrete phase model one-way coupled multiphase approach was established using the computational fluid dynamics code ANSYS FLUENT and applied to the analysis during the first seconds of LOVA. The results showed that air ingress into the VV behaved like a highly free under-expanded jet at the initial stage and Mach disk was formed at similar to 6 ms. Moreover, the flow field dramatically changed at the position of the Mach disk. The jet core before the Mach disk had a maximum velocity of similar to 8 Mach with the corresponding lowest static pressure (similar to 100 Pa) and temperature (few tens of K). The friction velocities in the lower part of the VV, which is an area of concern due to dust deposition, were generally larger than 15 m/s near the inlet region. Lastly, the crude prediction of the particle trajectories demonstrated the spiral trajectories of the dust following the air motion. Therefore, this study provided a basis for further safety analysis and accident prevention related to dust transport and explosion in future fusion reactors.
WOS关键词VACUUM ACCIDENT ; RESUSPENSION ; DEVICES ; FIELD ; LOVA
资助项目National Natural Science Foundation of China[51906249] ; National Key R&D Program of China[2019YFE0191600] ; President Foundation of Hefei Institute of Physical Science, Chinese Academy of Sciences[YZJJ2019QN21]
WOS研究方向Nuclear Science & Technology ; Physics
语种英语
WOS记录号WOS:000673983000001
出版者SPRINGER SINGAPORE PTE LTD
资助机构National Natural Science Foundation of China ; National Key R&D Program of China ; President Foundation of Hefei Institute of Physical Science, Chinese Academy of Sciences
源URL[http://ir.hfcas.ac.cn:8080/handle/334002/123275]  
专题中国科学院合肥物质科学研究院
通讯作者Zhang, Shi-Chao; Wang, Zhen
作者单位1.Univ Sci & Technol China, Hefei 230026, Peoples R China
2.Chinese Acad Sci, Hefei Inst Phys Sci, Inst Nucl Energy Safety Technol, Hefei 230031, Peoples R China
推荐引用方式
GB/T 7714
Wang, Bu-Er,Zhang, Shi-Chao,Wang, Zhen,et al. Numerical analysis of supersonic jet flow and dust transport induced by air ingress in a fusion reactor[J]. NUCLEAR SCIENCE AND TECHNIQUES,2021,32.
APA Wang, Bu-Er,Zhang, Shi-Chao,Wang, Zhen,Jia, Jiang-Tao,&Chen, Zhi-Bin.(2021).Numerical analysis of supersonic jet flow and dust transport induced by air ingress in a fusion reactor.NUCLEAR SCIENCE AND TECHNIQUES,32.
MLA Wang, Bu-Er,et al."Numerical analysis of supersonic jet flow and dust transport induced by air ingress in a fusion reactor".NUCLEAR SCIENCE AND TECHNIQUES 32(2021).

入库方式: OAI收割

来源:合肥物质科学研究院

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