中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Numerical analysis on the heat transfer of three types of nozzles for the hypersonic long-run wind tunnel

文献类型:期刊论文

作者Xing YF(邢云绯); Zhong FQ(仲峰泉); Li DX(李东霞); Zhang XY(张新宇)
刊名Science China-Technological Sciences
出版日期2015-03
卷号58期号:3页码:470-475
通讯作者邮箱fzhong@imech.ac.cn
关键词hypersonic scramjet test tunnel nozzle aerodynamic heating convective heat transfer
ISSN号1674-7321
产权排序[Xing YunFei; Zhong FengQuan; Li DongXia; Zhang XinYu] Chinese Acad Sci, Inst Mech, Natl Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China
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.
中文摘要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.
学科主题Engineering, Multidisciplinary; Materials Science, Multidisciplinary
分类号二类/Q2
类目[WOS]Engineering, Multidisciplinary ; Materials Science, Multidisciplinary
研究领域[WOS]Engineering ; Materials Science
关键词[WOS]FLUX
收录类别SCI ; EI ; CSCD
原文出处http://dx.doi.org/10.1007/s11431-014-5764-1
语种英语
WOS记录号WOS:000350336800010
源URL[http://dspace.imech.ac.cn/handle/311007/49917]  
专题力学研究所_高温气体动力学国家重点实验室
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.
APA 邢云绯,仲峰泉,李东霞,&张新宇.(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.

入库方式: OAI收割

来源:力学研究所

浏览0
下载0
收藏0
其他版本

除非特别说明,本系统中所有内容都受版权保护,并保留所有权利。