Knowledge Management System of Institue of Mechanics, CAS
| Direct numerical simulation of round supersonic free jet | |
Li XL(李新亮) ; Fu DX(傅德薰); Ma YW(马延文); Li, XL (reprint author), Chinese Acad Sci, LNM, Inst Mech, Beijing 100080, Peoples R China.
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| Source Publication | RECENT ADVANCES IN FLUID MECHANICS |
| 2004 | |
| Conference Name | 4th International Conference on Fluid Mechanics |
| Conference Date | JUL 20-30, 2004 |
| Conference Place | Dalian, PEOPLES R CHINA |
| Abstract | 6th order group-velocity control scheme is constructed and used in direct numerical simulation of the round supersonic free jet. The exit Mach number of the jet is 2.5. The disturbance waves generated by the jet are showed and the reason of the existence up-stream propagated wave is analyzed. |
| WOS ID | WOS:000225709300159 |
| ISBN | 7-302-08817-9 |
| Indexed By | CPCI-S |
| Language | 英语 |
| Citation statistics | |
| Document Type | 会议论文 |
| Identifier | http://dspace.imech.ac.cn/handle/311007/58920 |
| Collection | 力学所知识产出(1956-2008) |
| Corresponding Author | Li, XL (reprint author), Chinese Acad Sci, LNM, Inst Mech, Beijing 100080, Peoples R China. |
| Recommended Citation GB/T 7714 | Li XL,Fu DX,Ma YW,et al. Direct numerical simulation of round supersonic free jet[C]RECENT ADVANCES IN FLUID MECHANICS,2004. |
| Files in This Item: | Download All | |||||
| File Name/Size | DocType | Version | Access | License | ||
| CPCI-B017.pdf（268KB） | 会议论文 | 开放获取 | CC BY-NC-SA | View Download | ||
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