IMECH-IR  > 高温气体动力学国家重点实验室
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.
Source PublicationScience China-Technological Sciences
2015-03
Volume58Issue:3Pages:470-475
ISSN1674-7321
AbstractThe 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.
KeywordHypersonic Scramjet Test Tunnel Nozzle Aerodynamic Heating Convective Heat Transfer
Subject AreaEngineering, Multidisciplinary ; Materials Science, Multidisciplinary
DOI10.1007/s11431-014-5764-1
URL查看原文
Indexed BySCI ; EI ; CSCD
Language英语
WOS IDWOS:000350336800010
WOS KeywordFLUX
WOS Research AreaEngineering ; Materials Science
WOS SubjectEngineering, Multidisciplinary ; Materials Science, Multidisciplinary
Funding OrganizationNational Natural Science Foundation of China [11202218, 11172309]
DepartmentLHD高超声速推进技术
Classification二类/Q2
Citation statistics
Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/49917
Collection高温气体动力学国家重点实验室
Corresponding AuthorZhong, 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.
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