| Numerical analysis on the heat transfer of three types of nozzles for the hypersonic long-run wind tunnel | |
Xing YF(邢云绯) ; Zhong FQ(仲峰泉); Li DX(李东霞); Zhang XY(张新宇); Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Natl Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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| Source Publication | Science China-Technological Sciences
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| 2015-03 | |
| Volume | 58Issue:3Pages:470-475 |
| ISSN | 1674-7321 |
| Abstract | The hypersonic long-run scramjet test tunnel is one of the key ground facilities for the studies of ramjet/scramjet and hypersonic thermal management. Due to the significantly large heat loading, the nozzle of the tunnel facility demands effective cooling protection. In this work, the two-dimensional, three-dimensional and axisymmetric Mach 6.5 nozzles at an inlet total temperature of 1840 K and a total pressure of 6.4 MPa were studied with main focuses on the properties of aerodynamic heating of nozzles. The present work aims to provide insights into the design of an effective cooling system for the nozzle and other components of the hypersonic long-run wind tunnel. |
| Keyword | Hypersonic Scramjet Test Tunnel Nozzle Aerodynamic Heating Convective Heat Transfer |
| Subject Area | Engineering, Multidisciplinary ; Materials Science, Multidisciplinary |
| DOI | 10.1007/s11431-014-5764-1 |
| URL | 查看原文 |
| Indexed By | SCI ; EI ; CSCD |
| Language | 英语 |
| WOS ID | WOS:000350336800010 |
| WOS Keyword | FLUX |
| WOS Research Area | Engineering ; Materials Science |
| WOS Subject | Engineering, Multidisciplinary ; Materials Science, Multidisciplinary |
| Funding Organization | National Natural Science Foundation of China [11202218, 11172309] |
| Department | LHD高超声速推进技术 |
| Classification | 二类/Q2 |
| Citation statistics | |
| Document Type | 期刊论文 |
| Identifier | http://dspace.imech.ac.cn/handle/311007/49917 |
| Collection | 高温气体动力学国家重点实验室 |
| Corresponding Author | Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Natl Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China. |
| Recommended Citation GB/T 7714 | Xing YF,Zhong FQ,Li DX,et al. Numerical analysis on the heat transfer of three types of nozzles for the hypersonic long-run wind tunnel[J]. Science China-Technological Sciences,2015,58(3):470-475. |
| APA | 邢云绯,仲峰泉,李东霞,张新宇,&Zhong, FQ .(2015).Numerical analysis on the heat transfer of three types of nozzles for the hypersonic long-run wind tunnel.Science China-Technological Sciences,58(3),470-475. |
| MLA | 邢云绯,et al."Numerical analysis on the heat transfer of three types of nozzles for the hypersonic long-run wind tunnel".Science China-Technological Sciences 58.3(2015):470-475. |
| Files in This Item: | ||||||
| File Name/Size | DocType | Version | Access | License | ||
| IMCAS-J2015-071.pdf（860KB） | 开放获取 | CC BY-NC | View Application Full Text | |||
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