| 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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| 发表期刊 | Science China-Technological Sciences
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| 2015-03
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| 卷号 | 58期号:3页码:470-475 |
| ISSN | 1674-7321
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| 摘要 | 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. |
| 关键词 | Hypersonic Scramjet Test Tunnel
Nozzle
Aerodynamic Heating
Convective Heat Transfer
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| 学科领域 | Engineering, Multidisciplinary
; Materials Science, Multidisciplinary
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| DOI | 10.1007/s11431-014-5764-1
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| URL | 查看原文
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| 收录类别 | SCI
; EI
; CSCD
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| 语种 | 英语
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| WOS记录号 | WOS:000350336800010
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| 关键词[WOS] | FLUX
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| WOS研究方向 | Engineering
; Materials Science
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| WOS类目 | Engineering, Multidisciplinary
; Materials Science, Multidisciplinary
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| 项目资助者 | National Natural Science Foundation of China [11202218, 11172309]
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| 课题组名称 | LHD高超声速推进技术
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| 论文分区 | 二类/Q2
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| 引用统计 |
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| 文献类型 | 期刊论文
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| 条目标识符 | http://dspace.imech.ac.cn/handle/311007/49917
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| 专题 | 高温气体动力学国家重点实验室
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| 通讯作者 | Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Natl Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China. |
推荐引用方式
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.
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| 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.
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| 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.
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